WO2018198570A1 - フィルム状焼成材料、及び支持シート付フィルム状焼成材料 - Google Patents
フィルム状焼成材料、及び支持シート付フィルム状焼成材料 Download PDFInfo
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- WO2018198570A1 WO2018198570A1 PCT/JP2018/010222 JP2018010222W WO2018198570A1 WO 2018198570 A1 WO2018198570 A1 WO 2018198570A1 JP 2018010222 W JP2018010222 W JP 2018010222W WO 2018198570 A1 WO2018198570 A1 WO 2018198570A1
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- film
- fired material
- metal particles
- curve
- sinterable metal
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- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/006—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of flat products, e.g. sheets
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Definitions
- the present invention relates to a film-like fired material and a film-like fired material with a support sheet.
- This application includes Japanese Patent Application No. 2017-090714 filed in Japan on April 28, 2017, Japanese Patent Application No. 2017-179797 filed in Japan on September 20, 2017, and October 2, 2017. Claim priority based on Japanese Patent Application No. 2017-192821 filed in Japan, the contents of which are incorporated herein.
- Patent Document 1 discloses paste-like metal fine particles in which specific heat-sinterable metal particles, a specific polymer dispersant, and a specific volatile dispersion medium are mixed. A composition is disclosed. When the composition is sintered, it becomes a solid metal having excellent thermal conductivity.
- an object of the present invention is to provide a film-like fired material that is excellent in thickness stability and thermal conductivity and exhibits excellent shear adhesion after firing. To do. Moreover, it aims at providing the film-like baking material with a support sheet provided with the said film-like baking material.
- thermogravimetric curve TG curve
- DTA curve differential thermal analysis curve
- the present invention includes the following aspects.
- a film-like fired material containing sinterable metal particles and a binder component In the thermogravimetric curve (TG curve) measured from 40 ° C. to 600 ° C. at a rate of temperature increase of 10 ° C./min in the air atmosphere, the time (A1) after the start of temperature increase with the largest negative slope, In a differential thermal analysis curve (DTA curve) measured from 40 ° C. to 600 ° C. at a rate of temperature increase of 10 ° C./min in an air atmosphere using alumina particles as a reference sample, in the time range from 0 seconds to 2160 seconds after the start of temperature increase.
- TG curve thermogravimetric curve
- DTA curve differential thermal analysis curve
- the maximum peak time (B1) of A film-like fired material satisfying the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds and A1 ⁇ 2000 seconds.
- TG curve thermogravimetric curve
- DTA curve differential thermal analysis curve
- the peak time (B1 ′) observed in the shortest time is The film-like fired material according to [1], which satisfies a relationship of B1 ′ ⁇ A1 ′.
- temperature increase starts in a differential thermal analysis curve (DTA curve) measured from 40 ° C. to 600 ° C. at a temperature increase rate of 10 ° C./min in an air atmosphere using alumina particles as a reference sample.
- DTA curve differential thermal analysis curve
- a film-like fired material containing sinterable metal particles and a binder component In the thermogravimetric curve (TG curve) measured at a heating rate of 10 ° C./min in a nitrogen atmosphere, the temperature (A2) having the largest negative slope, The maximum peak temperature (B2) in the temperature range of 25 ° C. to 400 ° C. in a differential thermal analysis curve (DTA curve) measured at a temperature increase rate of 10 ° C./min under a nitrogen atmosphere using alumina particles as a reference sample, A film-like fired material satisfying the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C.
- the negative slope is the largest in the thermogravimetric curve (TG curve) measured at a temperature increase rate of 10 ° C./min in a nitrogen atmosphere.
- Temperature (A2 ′) The sinterable metal particles were observed in a temperature range of 200 ° C. to 400 ° C. in a differential thermal analysis curve (DTA curve) measured with a temperature rise rate of 10 ° C./min under a nitrogen atmosphere using alumina particles as a reference sample.
- the peak temperature (B2 ′) observed at the lowest temperature is The film-like fired material according to [4], which satisfies a relationship of B2 ′ ⁇ A2 ′.
- a film with a support sheet comprising: the film-like fired material according to any one of [1] to [7]; and a support sheet provided on at least one side of the film-like fired material. Firing material.
- the support sheet is provided with a pressure-sensitive adhesive layer on a base film, The film-like fired material with a support sheet according to [8], wherein the film-like fired material is provided on the pressure-sensitive adhesive layer.
- a film-like fired material that is excellent in thickness stability and thermal conductivity and exhibits excellent shear adhesion after firing.
- a film-like fired material with a support sheet which is provided with the film-like fired material and is used for sintered joining of semiconductor elements, can be provided.
- the film-like fired material of the first embodiment is a film-like fired material containing sinterable metal particles and a binder component, and is measured from 40 ° C. to 600 ° C. at a temperature rising rate of 10 ° C./min in an air atmosphere.
- TG curve thermogravimetric curve
- A1 the time (A1) after the start of temperature increase with the largest negative slope
- the maximum peak time (B1) in the time range from 0 second to 2160 seconds after the start of temperature rising in the differential thermal analysis curve (DTA curve) measured up to 1 satisfies the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds, and A1 ⁇ 2000 seconds.
- the film-like fired material of the second embodiment is a film-like fired material containing sinterable metal particles and a binder component, and is a thermogravimetric curve (TG) measured at a heating rate of 10 ° C./min in a nitrogen atmosphere. Curve) at a temperature with the largest negative slope (A2) and a differential thermal analysis curve (DTA curve) measured at a heating rate of 10 ° C./min under a nitrogen atmosphere using alumina particles as a reference sample. The maximum peak temperature (B2) in the temperature range of 400 ° C. satisfies the relationship of A 2 ⁇ B 2 ⁇ A 2 + 60 ° C.
- FIG. 1 is a cross-sectional view schematically showing a film-like fired material according to the first embodiment and the second embodiment.
- the film-like fired material 1 contains sinterable metal particles 10 and a binder component 20.
- the film-like fired material may be composed of one layer (single layer) or may be composed of two or more layers.
- these layers may be the same as or different from each other, and the combination of these layers is not particularly limited as long as the effects of the present invention are not impaired.
- a plurality of layers may be the same or different from each other” means “all layers may be the same or all layers. May be different, and only some of the layers may be the same, ”and“ multiple layers are different from each other ”means“ the constituent materials of each layer, the blending ratio of the constituent materials, and the thickness. At least one of them is different from each other ”.
- the thickness of the film-like fired material before firing is not particularly limited, but is preferably 10 to 200 ⁇ m, preferably 20 to 150 ⁇ m, and more preferably 30 to 90 ⁇ m.
- the “thickness of the film-like fired material” means the thickness of the entire film-like fired material.
- the thickness of the film-like fired material consisting of a plurality of layers means all of the film-like fired material Means the total thickness of the layers.
- thickness can be obtained by using a constant pressure thickness measuring instrument in accordance with JIS K7130 as a value represented by an average of thicknesses measured at five arbitrary locations.
- a film-form baking material can be provided in the state laminated
- the release film may be peeled off and placed on the object to be sintered and bonded to the film-like fired material.
- the release film also has a function as a protective film for preventing damage to the film-like fired material and adhesion of dirt.
- the release film only needs to be provided on at least one side of the film-like fired material, and may be provided on both sides of the film-like fired material.
- release film for example, polyethylene film, polypropylene film, polybutene film, polybutadiene film, polymethylpentene film, polyvinyl chloride film, vinyl chloride copolymer film, polyethylene terephthalate film, polyethylene naphthalate film, polybutylene terephthalate film, Polyurethane film, ethylene vinyl acetate copolymer film, ionomer resin film, ethylene / (meth) acrylic acid copolymer film, ethylene / (meth) acrylic acid ester copolymer film, polystyrene film, polycarbonate film, polyimide film, fluorine A transparent film such as a resin film is used. These crosslinked films are also used.
- these laminated films may be sufficient.
- the film which colored these, an opaque film, etc. can be used.
- the release agent include release agents such as silicone-based, fluorine-based, alkyd-based, olefin-based, and long-chain alkyl group-containing carbamate.
- the thickness of the release film is usually about 10 to 500 ⁇ m, preferably about 15 to 300 ⁇ m, particularly preferably about 20 to 250 ⁇ m.
- the sinterable metal particles are metal particles that can be heated and processed as a fired film-like fired material to melt and bond the particles to form a sintered body. By forming a sintered body, it is possible to sinter-bond the film-like fired material and the article fired in contact therewith.
- the metal species of the sinterable metal particles include silver, gold, copper, iron, nickel, aluminum, silicon, palladium, platinum, titanium, barium titanate, oxides or alloys thereof, and silver and silver oxide. Is preferred. Only one kind of sinterable metal particles may be blended, or two or more kinds may be blended.
- the sinterable metal particles are preferably silver nanoparticles that are nano-sized silver particles.
- the particle diameter of the sinterable metal particles contained in the film-like fired material is not particularly limited as long as it can exhibit the sinterability, but may be 100 nm or less, and 50 nm or less. It may be 30 nm or less.
- the particle diameter of the metal particles contained in the film-like fired material is a projected area equivalent circle diameter of the particle diameter of the metal particles observed with an electron microscope. Metal particles belonging to the above particle diameter range are preferable because of excellent sinterability.
- the particle diameter of the sinterable metal particles contained in the film-like fired material is the number average of the particle diameters obtained for the particles having a projected area equivalent circle diameter of 100 nm or less of the particle diameter of the metal particles observed with an electron microscope. 0.1 to 95 nm, 0.3 to 50 nm, and 0.5 to 30 nm. The number of metal particles to be measured is 100 or more randomly selected per one film-like fired material.
- a high-boiling solvent with a high boiling point such as isobornyl hexanol or decyl alcohol in order to make the aggregate free of aggregates. May be.
- the boiling point of the high boiling point solvent may be 200 to 350 ° C., for example.
- normal temperature means a temperature that is not particularly cooled or heated, that is, a normal temperature, and examples thereof include a temperature of 15 to 25 ° C.
- non-sinterable metal particles having a particle diameter not exceeding 100 nm are further blended. May be.
- the particle diameter of non-sinterable metal particles having a particle diameter exceeding 100 nm is the number of particle diameters obtained for particles having a projected area equivalent circle diameter exceeding 100 nm of the particle diameter of the metal particles observed with an electron microscope.
- the average may be greater than 150 nm and less than or equal to 50000 nm, may be 150 to 10,000 nm, and may be 180 to 5000 nm.
- the metal species of the non-sinterable metal particles having a particle diameter exceeding 100 nm include those exemplified above, and silver, copper, and oxides thereof are preferable.
- the metal particles having a particle diameter of 100 nm or less and the non-sinterable metal particles having a particle diameter exceeding 100 nm may be the same metal species or different metal species.
- the metal particles having a particle diameter of 100 nm or less may be silver particles
- the non-sinterable metal particles having a particle diameter exceeding 100 nm may be silver or silver oxide particles.
- the metal particles having a particle diameter of 100 nm or less may be silver or silver oxide particles
- the non-sinterable metal particles having a particle diameter exceeding 100 nm may be copper or copper oxide particles.
- the content of metal particles having a particle diameter of 100 nm or less with respect to 100 parts by mass of the total mass of all metal particles may be 20 to 100 parts by mass, or 30 to 99 parts by mass. It may be 50 to 95 parts by mass.
- At least one surface of the sinterable metal particles and the non-sinterable metal particles may be coated with an organic substance.
- an organic coating film compatibility with the binder component is improved. Furthermore, aggregation of particles can be prevented and the particles can be uniformly dispersed.
- the organic material is coated on at least one surface of the sinterable metal particles and the non-sinterable metal particles, the mass of the sinterable metal particles and the non-sinterable metal particles is a value including the coating.
- the fired material can be formed into a film shape, and tackiness can be imparted to the film-like fired material before firing.
- the binder component may be thermally decomposable that is thermally decomposed by heat treatment as firing of the film-like fired material.
- a binder component is not specifically limited, Resin is mentioned as a suitable example of a binder component.
- the resin include acrylic resins, polycarbonate resins, polylactic acid, and polymerized cellulose derivatives, and acrylic resins are preferred.
- Acrylic resins include homopolymers of (meth) acrylate compounds, copolymers of two or more (meth) acrylate compounds, and copolymers of (meth) acrylate compounds and other copolymerizable monomers. included.
- the content of the structural unit derived from the (meth) acrylate compound is preferably 50 to 100% by mass, and preferably 80 to 100% by mass with respect to the total amount of the structural unit. More preferably, it is 90 to 100% by mass.
- “derived” means that the monomer has undergone a structural change necessary for polymerization.
- the (meth) acrylate compound examples include methyl (meth) acrylate, ethyl (meth) acrylate, propyl (meth) acrylate, isopropyl (meth) acrylate, butyl (meth) acrylate, isobutyl (meth) acrylate, and t-butyl.
- (Meth) acrylate pentyl (meth) acrylate, amyl (meth) acrylate, isoamyl (meth) acrylate, hexyl (meth) acrylate, heptyl (meth) acrylate, octyl (meth) acrylate, isooctyl (meth) acrylate, 2-ethylhexyl (Meth) acrylate, ethylhexyl (meth) acrylate, nonyl (meth) acrylate, decyl (meth) acrylate, isodecyl (meth) acrylate, undecyl (meth) acrylate Dodecyl (meth) acrylate, alkyl (meth) acrylates such as lauryl (meth) acrylate, stearyl (meth) acrylate, isostearyl (meth) acrylate;
- Examples thereof include benzyl (meth) acrylate and tetrahydrofurfuryl (meth) acrylate.
- Alkyl (meth) acrylates or alkoxyalkyl (meth) acrylates are preferred.
- Particularly preferred (meth) acrylate compounds include butyl (meth) acrylate, ethylhexyl (meth) acrylate, lauryl (meth) acrylate, isodecyl (meth) acrylate, 2- Mention may be made of ethylhexyl (meth) acrylate and 2-ethoxyethyl (meth) acrylate.
- (meth) acrylic acid is a concept including both “acrylic acid” and “methacrylic acid”
- (meth) acrylate” means “acrylate” and “methacrylate”. It is a concept that encompasses both.
- the acrylic resin methacrylate is preferable.
- the binder component contains a structural unit derived from methacrylate
- the time (A1) and the time (B1) have a relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds, and a film-like fired material in which A1 ⁇ 2000 seconds is obtained. Easy to obtain.
- the binder component contains a structural unit derived from methacrylate, a film-like fired material in which the temperature (A2) and the temperature (B2) have a relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C. is easily obtained.
- the content of the structural unit derived from methacrylate is preferably 50 to 100% by mass, more preferably 80 to 100% by mass, based on the total amount of the structural unit, 90 More preferably, it is ⁇ 100% by mass.
- the other copolymerizable monomer is not particularly limited as long as it is a compound copolymerizable with the above (meth) acrylate compound.
- Unsaturated carboxylic acids; vinyl group-containing radical polymerizable compounds such as vinyl benzyl methyl ether, vinyl glycidyl ether, styrene, ⁇ -methyl styrene, butadiene, and isoprene.
- the weight average molecular weight (Mw) of the resin constituting the binder component is preferably 1,000 to 1,000,000, and more preferably 10,000 to 800,000. When the weight average molecular weight of the resin is within the above range, it becomes easy to develop sufficient film strength and impart flexibility as a film.
- weight average molecular weight is a polystyrene equivalent value measured by gel permeation chromatography (GPC) method unless otherwise specified.
- the glass transition temperature (Tg) of the resin constituting the binder component can be obtained by calculation using the following Fox theoretical formula, which is preferably ⁇ 60 to 50 ° C., and preferably ⁇ 30 to 10 ° C. It is more preferable that the temperature is ⁇ 20 or higher and lower than 0 ° C.
- Tg obtained from the Fox equation of the resin is not more than the above upper limit value, the adhesive force before firing between the film-like fired material and the adherend (for example, semiconductor element, chip, substrate, etc.) is improved.
- required from the Fox formula of resin is more than the said lower limit, a film shape can be maintained and the film-like baking material can be pulled apart from a support sheet etc. more easily.
- Tg represents the glass transition temperature of the polymer portion
- Tg1, Tg2,..., Tgm represent the glass transition temperature of each polymerization monomer
- W1, W2,..., Wm represent the weight ratio of each polymerization monomer.
- the binder component may be thermally decomposable that is thermally decomposed by heat treatment as firing of the film-like fired material.
- the thermal decomposition of the binder component can be confirmed by a decrease in the mass of the binder component due to firing.
- blended as a binder component may be substantially thermally decomposed by baking, the total mass of the component mix
- the binder component may have a mass after firing of 10% by mass or less, or 5% by mass or less, and 3% by mass or less with respect to 100% by mass of the binder component before firing. It may be.
- the film-like fired material of the embodiment includes sinterable metal particles, non-sinterable materials within the range not impairing the effects of the present invention.
- Other additives that do not correspond to the sinterable metal particles and the binder component may be contained.
- additives that may be contained in the film-like fired material of the embodiment include a solvent, a dispersant, a plasticizer, a tackifier, a storage stabilizer, an antifoaming agent, a thermal decomposition accelerator, and an antioxidant. Etc. Only 1 type may be contained and 2 or more types of additives may be contained. These additives are not particularly limited, and those commonly used in this field can be appropriately selected.
- the film-like fired material of the embodiment may be composed of sinterable metal particles, a binder component, and other additives, and the sum of these contents (% by mass) is 100% by mass. Good.
- the film-like fired material of the embodiment includes non-sinterable metal particles
- the film-like fired material is made of sinterable metal particles, non-sinterable metal particles, a binder component, and other additives. The sum of these contents (mass%) may be 100 mass%.
- the content of the sinterable metal particles is preferably 10 to 98% by mass with respect to the total content of 100% by mass of all components other than the solvent (hereinafter referred to as “solid content”). 15 to 90% by mass is more preferable, and 20 to 80% by mass is further preferable.
- the film-like fired material contains non-sinterable metal particles
- the total content of the sinterable metal particles and the non-sinterable metal particles with respect to 100% by mass of the total solid content in the film-like fired material is 50 to 98 mass% is preferable, 70 to 95 mass% is more preferable, and 80 to 90 mass% is more preferable.
- the content of the binder component with respect to the total solid content of 100% by mass in the film-like fired material is preferably 2 to 50% by mass, more preferably 5 to 30% by mass, and even more preferably 10 to 20% by mass.
- the mass ratio of the sinterable metal particles to the binder component is preferably 50: 1 to 1: 5, more preferably 20: 1 to 1: 2. 10: 1 to 1: 1 is more preferable.
- the mass ratio of the sinterable metal particles and non-sinterable metal particles to the binder component is preferably 50: 1 to 1: 1, more preferably 20: 1 to 2: 1, and even more preferably 9: 1 to 4: 1.
- the film-like fired material of the first embodiment may contain a high boiling point solvent used when mixing sinterable metal particles, non-sinterable metal particles, a binder component and other additive components. Good.
- the content of the high boiling point solvent is preferably 20% by mass or less, more preferably 15% by mass or less, and still more preferably 10% by mass or less with respect to 100% by mass of the total mass of the film-like fired material of the first embodiment.
- the time (A1) and the time (B1) have a relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds, and A1 ⁇ 2000 seconds.
- a fired material is easily obtained.
- DTA curve differential thermal analysis curve
- ⁇ Time (A1) / Time (B1)> The film-like fired material according to the first embodiment starts the temperature increase with the largest negative slope in the thermogravimetric curve (TG curve) measured from 40 ° C. to 600 ° C. at a temperature increase rate of 10 ° C./min in the air atmosphere. Later time (A1) and 0 in the differential thermal analysis curve (DTA curve) measured from 40 ° C. to 600 ° C. at a temperature rising rate of 10 ° C./min in the air atmosphere using alumina particles as a reference sample.
- the maximum peak time (B1) in the time range from 2 seconds to 2160 seconds satisfies the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds, and A1 ⁇ 2000 seconds.
- the TG curve represents a change in the weight of the film-like fired material in the process of heat-treating the film-like fired material in the air atmosphere.
- the DTA curve represents a change in differential heat of the film-like fired material in the process of heat-treating the film-like fired material in the air atmosphere.
- FIG. 2 shows the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds, A1 ⁇ 2000 seconds, before firing (FIG. 2 (a)), during firing (FIG. 2 (b)), after firing. It is sectional drawing which shows a mode that it estimates about (FIG.2 (c)).
- the binder component 20 contained in the film-like fired material before firing (FIG. 2 (a)) is reduced in weight by heating (FIG. 2 (b) to (c)), and this phenomenon is a TG curve. Appears as a negative slope at.
- the binder component 20 contained in the film-like fired material before firing (FIG. 2A) is thermally decomposed by absorbing heat during heating, and is contained in the film-like fired material before firing (FIG. 2A).
- the sinterable metal particles 10 are melted by absorbing heat during heating (FIG. 2B), and then sintered while generating heat (FIG. 2C). This endothermic process is observed as a DTA curve, but when the sintering process proceeds sufficiently, the calorific value is large and the pyrolysis of the binder component 20 contained in the film-like fired material (FIG. 2 (a)).
- the heat absorption by melting of the sinterable metal particles 10 is greatly exceeded. That is, in the DTA curve obtained by measurement, only positive differential heat due to heat generation is observed and appears as a peak.
- the time (A1) and the time (B1) satisfy the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds, and A1 ⁇ 2000 seconds means that the sinterable metal particles are heated immediately after the decrease of the binder component. This is considered to mean that the melting and sintering of is completed. It is generally known that the firing temperature is related to the size of the metal particles, and the smaller the metal particles, the lower the firing temperature. Therefore, the film-like fired material 1 satisfying the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds and A1 ⁇ 2000 seconds does not show aggregation or fusion between the sinterable metal particles at the start of sintering, and is in the form of fine particles. It is presumed that the sintered metal particles 10m melted as they are sintered.
- FIG. 3 does not satisfy the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds, and the firing material 1c having a B1 time larger than A1 + 200 seconds is before firing (FIG. 3 (a)) and during firing (FIG. 3 (b)). It is sectional drawing which shows typically a mode that it estimates about after baking (FIG.3 (c)).
- the binder component 21 contained in the film-like fired material before firing (FIG. 3A) also decreases in weight due to heating (FIGS. 3B to 3C). Appears as a negative slope at.
- the binder component 21 contained in the film-like fired material before firing (FIG. 3 (a)) is also thermally decomposed by absorbing heat during heating, and then into the film-like fired material before firing (FIG. 3 (a)).
- the contained sinterable metal particles 11 cause melting by heat absorption and sintering by heat generation (FIG. 3C).
- the process of absorbing and generating heat of the sinterable metal particles 11 occurs almost at the same time because the binder component 21 is not present or is small even if it is present, but since the amount of heat generated by sintering is large, the DTA curve In, only a positive peak indicating an exothermic process appears.
- the fact that the time (A1) and the time (B1) do not satisfy the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds means that the firing of the sinterable metal particles is not completed in the heating time immediately following the decrease of the binder component. It is thought that means.
- the firing temperature is related to the size of the metal particles, and the larger the metal particles, the higher the firing temperature. Therefore, for example, in the sintered material 1c that does not satisfy the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds and the time of B1 is longer than A1 + 200 seconds, it is estimated that the size of the sinterable metal particles is large at the stage of sintering.
- the inventors satisfy the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds with time (A1) and time (B1), and the film-like fired material satisfying A1 ⁇ 2000 seconds has excellent shear adhesive strength after firing. I found out.
- the sintered sinterable metal particles are sintered. It is conceivable that many unsintered portions remain, and the material after sintering is poor in adhesive strength (shear adhesive strength). Alternatively, it is conceivable that voids are likely to be generated at the adhesion interface with the adherend, and the adhesion strength is reduced by reducing the adhesion area.
- the film-like fired material satisfying A1 ⁇ 2000 seconds can be applied to a device member due to a decrease in productivity due to a tact time extension and a higher temperature required for firing. An adverse effect is possible.
- the sintered metal particles melted in the form of fine particles are baked in the presence of the binder component. By being bonded, the sinterable metals are uniformly and tightly bonded to each other, and it is considered that the adhesion strength of the sintered material is improved.
- the shear adhesive strength after firing of the film-like fired material can be measured by the method described in Examples.
- the time (A1) and the time (B1) satisfy the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds, for example, satisfy the relationship of A1 ⁇ B1 ⁇ A1 + 100 seconds. It may be a thing, may satisfy
- the maximum peak time (B1) in the time range from 0 seconds to 2160 seconds after the start of temperature increase is a differential measured from 40 ° C. to 600 ° C. at a temperature increase rate of 10 ° C./min in an air atmosphere using alumina particles as a reference sample.
- DTA curve thermal analysis curve
- the film-like fired material of the first embodiment is a heat measured from 40 ° C. to 600 ° C. at a temperature rise rate of 10 ° C./min in an air atmosphere for the component obtained by removing the sinterable metal particles from the film-like fired material.
- DTA curve differential thermal analysis curve measured from 40 ° C. to 600 ° C. at a rate
- the peak time observed in the shortest time among the peaks observed in the time range from 960 seconds to 2160 seconds after the start of temperature increase ( B1 ′) preferably satisfies the relationship B1 ′ ⁇ A1 ′.
- the TG curve represents the change in the weight of the component excluding the sinterable metal particles from the film-like fired material in the process of being heat-treated as fired in the air atmosphere.
- the DTA curve represents the differential heat change of the sinterable metal particles in the process of heat treatment as firing in an air atmosphere.
- the film-like fired material according to the first embodiment includes non-sinterable metal particles
- the film-like fired material according to the first embodiment is obtained from the film-like fired material and the sinterable metal particles and the non-sinterable metal.
- the thermogravimetric curve (TG curve) measured from 40 ° C. to 600 ° C. at a temperature increase rate of 10 ° C./min in the air atmosphere
- the peak time (B1 ′) observed in the shortest time among the peaks observed in the time range from 960 seconds to 2160 seconds after the start of temperature rise has a relationship of B1 ′ ⁇ A1 ′.
- B1 ′ the peak time observed in the shortest time among the peaks observed in the time range from 960 seconds to 2160 seconds after the start of temperature rise.
- B1 ′ the peak time observed in the shortest time among the peaks observed in the time range from 960 seconds to 2160 seconds after the start of temperature rise has a relationship of B1 ′ ⁇ A1 ′.
- the components obtained by removing the sinterable metal particles and non-sinterable metal particles from the film-like fired material containing the binder component contained in the film-like fired material before firing are reduced in weight by heating in the atmosphere. This phenomenon appears as a negative slope in the TG curve.
- the sinterable metal particles contained in the film-like fired material before firing are melted and sintered by heating in the atmosphere, the melting phenomenon is a negative peak in the DTA curve, and the sintering phenomenon is positive in the DTA curve. Appears as a peak.
- time (A1 ′) and time (B1 ′) satisfy the relationship of B1 ′ ⁇ A1 ′ means that the components distributed around the sinterable metal particles of the film-like fired material during the heat treatment process. This is considered to mean that the melting and sintering of the sinterable metal particles are started earlier than the timing of weight reduction. Therefore, the film-like fired material satisfying the relationship of B1 ′ ⁇ A1 ′ is in a state of being isolated by the components distributed around the sinterable metal particles, easily melted in the form of fine particles, and time (A1 ′) At this point, the collision frequency increases rapidly, and the sinterable metal particles melted in the form of fine particles are easily sintered. As a result, in the film-like fired material satisfying the relationship of B1 ' ⁇ A1', the sinterable metals are uniformly and tightly bonded to each other, and it is considered that the strength of the sintered material is improved.
- the time (A1 ′) and the time (B1 ′) are obtained by separating the sinterable metal particles and the components excluding the sinterable metal particles from the film-like fired material before firing. It can be determined from the TG curve and DTA curve for the sample. Separation of the sinterable metal particles from the film-like fired material before firing and the remaining components excluding the sinterable metal particles can be performed, for example, by the following method. First, after mixing a film-like fired material before firing and a sufficient amount of an organic solvent, this is allowed to stand for a sufficient time until the sinterable metal particles settle. The supernatant liquid is extracted with a syringe or the like, and the residue after drying at 120 ° C.
- the film-like fired material of the first embodiment includes non-sinterable metal particles
- the time (A1 ′) and time (B1 ′) are determined from the film-like fired material before firing. Separating the sinterable metal particles and non-sinterable metal particles from the components excluding the sinterable metal particles and non-sinterable metal particles, and a TG curve for each separated sample; It can be determined from the DTA curve. Separation of the sinterable metal particles and non-sinterable metal particles from the film-like fired material before firing and the remaining components excluding the sinterable metal particles and non-sinterable metal particles is, for example, The following method can be used.
- the solvent used here is preferably a solvent that can dissolve the binder component and can be volatilized under the drying conditions at 120 to 250 ° C. for 10 minutes.
- hydrocarbons such as toluene and xylene
- alcohols such as methanol, ethanol, 2-propanol, isobutyl alcohol (2-methylpropan-1-ol) and 1-butanol
- esters such as ethyl acetate
- ketones such as acetone and methyl ethyl ketone Ethers such as tetrahydrofuran
- amides such as dimethylformamide and N-methylpyrrolidone (compounds having an amide bond), and the like.
- the film-like fired material of the first embodiment is a differential thermal analysis curve (measured from 40 ° C. to 600 ° C. at a temperature rise rate of 10 ° C./min in the air atmosphere with the alumina particles as a reference sample. (DTA curve) preferably has no endothermic peak in the time range from 0 seconds to 2160 seconds after the start of temperature increase.
- the DTA curve represents the change in differential heat of the film-like fired material during the process of heating the film-like fired material as firing.
- the film-like fired material contains a component that changes (for example, evaporates) by absorbing heat from the film-like fired material from 0 to 2160 seconds after the start of temperature increase. It is possible. That is, it can be considered that the evaporation of the components has occurred and the heat of vaporization associated therewith is necessary. Or it shows that it contains many components that endotherm by heat absorption and exceeds the amount of heat generated by sintering.
- the film-like fired material of the first embodiment has a small or no content of components having a property of evaporating from the film-like fired material in 0 to 2160 seconds after the start of temperature increase. Moreover, it is preferable that the content of the component which absorbs a large amount of heat in pyrolysis and hinders the heat generation process by sintering is small or not contained.
- the film-like fired material be pretreated such as drying so that moisture absorbed as impurities is not measured. Is done.
- drying treatment condition include 110 ° C. for 4 minutes.
- the film-like fired material of the first embodiment is excellent in thickness stability. Moreover, since the film-form baking material of 1st embodiment contains a sinterable metal particle, it is excellent in thermal conductivity. Furthermore, the film-like fired material of the first embodiment satisfies the relationship of A1 ⁇ B1 ⁇ A1 + 200 seconds, and exhibits an excellent shear adhesive force after firing when A1 ⁇ 2000 seconds.
- the film-like fired material of the second embodiment may contain a high boiling point solvent used when mixing sinterable metal particles, non-sinterable metal particles, a binder component and other additive components. Good.
- the content of the high boiling point solvent is preferably 20% by mass or less, more preferably 15% by mass or less, and further preferably 10% by mass or less with respect to 100% by mass of the total mass of the film-like fired material of the second embodiment.
- the content of the high boiling point solvent is not more than the above upper limit value, a film-like fired material in which the temperature (A2) and the temperature (B2) have a relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C. is easily obtained.
- DTA curve differential thermal analysis curve
- the film-like fired material according to the second embodiment comprises a temperature (A2) having the largest negative slope in the thermogravimetric curve (TG curve) measured at a heating rate of 10 ° C./min in a nitrogen atmosphere, and alumina particles.
- the maximum peak temperature (B2) in the temperature range from 25 ° C. to 400 ° C. in the differential thermal analysis curve (DTA curve) measured at a rate of temperature increase of 10 ° C./min under a nitrogen atmosphere as a reference sample is A2 ⁇ B2 ⁇ A2 + 60 ° C. is satisfied.
- the TG curve represents a change in the weight of the film-like fired material in the process of heat-treating the film-like fired material in a nitrogen atmosphere.
- the DTA curve represents the differential heat change of the film-like fired material in the course of heat treatment of the film-like fired material in a nitrogen atmosphere.
- FIG. 2 shows a film-like fired material 1 satisfying the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C. before firing (FIG. 2 (a)), during firing (FIG. 2 (b)), and after firing (FIG. 2 (c)). It is sectional drawing which shows typically a mode that it estimates about.
- the binder component 20 contained in the film-like fired material before firing (FIG. 2 (a)) is reduced in weight by heating (FIG. 2 (b) to (c)), and this phenomenon is a TG curve. Appears as a negative slope at.
- the binder component 20 contained in the film-like fired material before firing (FIG. 2A) is thermally decomposed by absorbing heat during heating, and is contained in the film-like fired material before firing (FIG. 2A).
- the sinterable metal particles 10 are melted by absorbing heat during heating (FIG. 2B), and then sintered while generating heat (FIG. 2C). This endothermic process is observed as a DTA curve, but when the sintering process proceeds sufficiently, the calorific value is large and the pyrolysis of the binder component 20 contained in the film-like fired material (FIG. 2 (a)).
- the heat absorption by melting of the sinterable metal particles 10 is greatly exceeded. That is, in the DTA curve obtained by measurement, only positive differential heat due to heat generation is observed and appears as a peak.
- the fact that the temperature (A2) and the temperature (B2) satisfy the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C. means that the melting and sintering of the sinterable metal particles are completed at the heating temperature immediately following the decrease of the binder component. It is thought that it means to do. It is generally known that the firing temperature is related to the size of the metal particles, and the smaller the metal particles, the lower the firing temperature. Therefore, the film-like fired material 1 satisfying the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C. is not confirmed to be agglomerated or fused between the sinterable metal particles at the start of sintering, and sinterability melted in the form of fine particles. It is estimated that the metal particles 10m are sintered.
- FIG. 3 does not satisfy the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C., and the firing material 1c in which the temperature of B2 is larger than A2 + 60 ° C. is before firing (FIG. 3 (a)) and during firing (FIG. 3 (b)). It is sectional drawing which shows typically a mode that it estimates about after baking (FIG.3 (c)).
- the binder component 21 contained in the film-like fired material before firing (FIG. 3A) also decreases in weight due to heating (FIGS. 3B to 3C). Appears as a negative slope at.
- the binder component 21 contained in the film-like fired material before firing (FIG. 3 (a)) is also thermally decomposed by absorbing heat during heating, and then into the film-like fired material before firing (FIG. 3 (a)).
- the contained sinterable metal particles 11 cause melting by heat absorption and sintering by heat generation (FIG. 3C).
- the process of absorbing and generating heat of the sinterable metal particles 11 occurs almost at the same time because the binder component 21 is not present or is small even if it is present, but since the amount of heat generated by sintering is large, the DTA curve In, only a positive peak indicating an exothermic process appears.
- the fact that the temperature (A2) and the temperature (B2) do not satisfy the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C. means that the firing of the sinterable metal particles is not completed at the heating temperature immediately following the decrease of the binder component. It is thought that means.
- the firing temperature is related to the size of the metal particles, and the larger the metal particles, the higher the firing temperature. Therefore, for example, in the sintered material 1c that does not satisfy the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C. and the temperature of B2 is higher than A2 + 60 ° C., it is estimated that the size of the sinterable metal particles is large at the stage of sintering.
- the inventors have also found that a film-like fired material in which the temperature (A2) and the temperature (B2) satisfy the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C. is excellent in shear adhesive strength after firing.
- the sintered sinterable metal particles are sintered. It is conceivable that many unsintered portions remain, and the material after sintering is poor in adhesive strength (shear adhesive strength). Alternatively, it is conceivable that voids are likely to be generated at the adhesion interface with the adherend, and the adhesion strength is reduced by reducing the adhesion area.
- the sintered metal particles that are melted in the form of fine particles are sintered, so that the sinterable metals are uniformly and densely metallized. It is considered that the bonding strength of the material after sintering is improved.
- the shear adhesive strength after firing of the film-like fired material can be measured by the method described in Examples.
- the temperature (A2) and the temperature (B2) satisfy the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C., for example, satisfy the relationship of A2 ⁇ B2 ⁇ A2 + 50 ° C. May satisfy
- the maximum peak temperature (B2) in the temperature range of 25 ° C. to 400 ° C. is 200 in a differential thermal analysis curve (DTA curve) measured at a temperature rising rate of 10 ° C./min in a nitrogen atmosphere using alumina particles as a reference sample.
- the maximum peak temperature is preferably at ⁇ 400 ° C., more preferably the maximum peak temperature at 220-390 ° C., and further preferably the maximum peak temperature at 250-380 ° C.
- the film-like fired material of the second embodiment is a thermogravimetric curve (TG curve) measured at a heating rate of 10 ° C./min in a nitrogen atmosphere with respect to the component obtained by removing the sinterable metal particles from the film-like fired material.
- TG curve thermogravimetric curve
- DTA differential thermal analysis curve
- the peak temperature (B2 ′) observed at the lowest temperature among the peaks observed in the temperature range of 200 ° C. to 400 ° C. in the curve) preferably satisfies the relationship B2 ′ ⁇ A2 ′.
- the TG curve represents the change in the weight of the component excluding the sinterable metal particles from the film-like fired material in the process of being heat-treated as fired in a nitrogen atmosphere.
- the DTA curve represents the temperature change of the differential heat of the sinterable metal particles in the process of heat treatment as firing in a nitrogen atmosphere.
- the film-like fired material according to the second embodiment includes non-sinterable metal particles
- the film-like fired material according to the second embodiment is obtained from the film-like fired material and the sinterable metal particles and the non-sinterable metal.
- the temperature (A2 ′) having the largest negative slope in the thermogravimetric curve (TG curve) measured at a heating rate of 10 ° C./min in a nitrogen atmosphere and the sinterable metal particles And non-sinterable metal particles in a temperature range of 200 ° C. to 400 ° C. in a differential thermal analysis curve (DTA curve) measured at a heating rate of 10 ° C./min under a nitrogen atmosphere using alumina particles as a reference sample.
- DTA curve differential thermal analysis curve
- the peak temperature (B2 ′) observed at the lowest temperature preferably satisfies the relationship of B2 ′ ⁇ A2 ′.
- Components obtained by removing the sinterable metal particles and non-sinterable metal particles from the film-like fired material containing the binder component contained in the film-like fired material before firing are reduced in weight by heating in a nitrogen atmosphere. This phenomenon appears as a negative slope in the TG curve.
- the fact that the temperature (A2 ′) and the temperature (B2 ′) satisfy the relationship of B2 ′ ⁇ A2 ′ means that the components distributed around the sinterable metal particles of the film-like fired material during the heat treatment process. This is considered to mean that the melting and sintering of the sinterable metal particles are started earlier than the timing of weight reduction. Therefore, the film-like fired material satisfying the relationship of B2 ′ ⁇ A2 ′ is in a state where each is isolated by components distributed around the sinterable metal particles, and is easily melted in the form of fine particles at a temperature (A2 ′). At this point, the collision frequency increases rapidly, and the sinterable metal particles melted in the form of fine particles are easily sintered. As a result, in the film-like fired material satisfying the relationship of B2 ' ⁇ A2', the sinterable metals are uniformly and tightly bonded to each other, and it is considered that the strength of the sintered material is improved.
- the temperature (A2 ′) and the temperature (B2 ′) are obtained by separating the sinterable metal particles and the components excluding the sinterable metal particles from the film-like fired material before firing. It can be determined from the TG curve and DTA curve for the sample. Separation of the sinterable metal particles from the film-like fired material before firing and the remaining components excluding the sinterable metal particles can be performed, for example, by the following method. First, after mixing a film-like fired material before firing and a sufficient amount of an organic solvent, this is allowed to stand for a sufficient time until the sinterable metal particles settle. The supernatant liquid is extracted with a syringe or the like, and the residue after drying at 120 ° C.
- the remaining liquid was dried at 120 ° C. for 10 minutes, and the residue was collected to collect the sinterable metal particles. Is possible.
- the film-like fired material of the second embodiment contains non-sinterable metal particles
- the temperature (A2 ′) and temperature (B2 ′) are determined from the film-like fired material before firing. Separating the sinterable metal particles and non-sinterable metal particles from the components excluding the sinterable metal particles and non-sinterable metal particles, and a TG curve for each separated sample; It can be determined from the DTA curve. Separation of the sinterable metal particles and non-sinterable metal particles from the film-like fired material before firing and the remaining components excluding the sinterable metal particles and non-sinterable metal particles is, for example, The following method can be used.
- the solvent used here is preferably a solvent that can dissolve the binder component and can be volatilized under the drying conditions at 120 to 250 ° C. for 10 minutes.
- hydrocarbons such as toluene and xylene
- alcohols such as methanol, ethanol, 2-propanol, isobutyl alcohol (2-methylpropan-1-ol) and 1-butanol
- esters such as ethyl acetate
- ketones such as acetone and methyl ethyl ketone Ethers such as tetrahydrofuran
- amides such as dimethylformamide and N-methylpyrrolidone (compounds having an amide bond), and the like.
- the film-like fired material of the second embodiment is a differential thermal analysis curve (DTA curve) measured for the film-like fired material using alumina particles as a reference sample at a heating rate of 10 ° C./min in a nitrogen atmosphere. It is preferable that there is no endothermic peak in the temperature range of from °C to 400 °C.
- DTA curve differential thermal analysis curve
- the above DTA curve represents the temperature change of the differential heat of the film-like fired material during the process in which the film-like fired material is heat-treated as fired.
- the film-like fired material contains a component having a property of changing (for example, evaporating) by absorbing heat from the film-like fired material at 25 ° C. to 400 ° C. . That is, it can be considered that the evaporation of the components has occurred and the heat of vaporization associated therewith is necessary. Or it shows that it contains many components that endotherm by heat absorption and exceeds the amount of heat generated by sintering. Therefore, it is preferable that the film-like fired material of the second embodiment has little or no content of a component having a property of evaporating from the film-like fired material at 25 ° C. to 400 ° C. Moreover, it is preferable that the content of the component which absorbs a large amount of heat in pyrolysis and hinders the heat generation process by sintering is small or not contained.
- the film-like fired material be pretreated such as drying so that moisture absorbed as impurities is not measured. Is done.
- drying treatment condition include 110 ° C. for 4 minutes.
- the film-like fired material of the second embodiment is excellent in thickness stability. Moreover, since the film-form baking material of 2nd embodiment contains a sinterable metal particle, it is excellent in thermal conductivity. Furthermore, the film-like fired material of the second embodiment exhibits an excellent shear adhesive force after firing by satisfying the relationship of A2 ⁇ B2 ⁇ A2 + 60 ° C.
- the film-like fired material can be formed using a fired material composition containing the constituent materials.
- a fired material composition containing each component and a solvent for constituting the film-like fired material by applying a fired material composition containing each component and a solvent for constituting the film-like fired material, and drying the solvent as needed to volatilize the solvent, A film-like adhesive can be formed at the target site.
- the solvent preferably has a boiling point of less than 250 ° C, more preferably a boiling point of less than 200 ° C, such as n-hexane (boiling point: 68 ° C), ethyl acetate (boiling point: 77 ° C), 2-butanone (boiling point).
- n-heptane (boiling point: 98 ° C), methylcyclohexane (boiling point: 101 ° C), toluene (boiling point: 111 ° C), acetylacetone (boiling point: 138 ° C), n-xylene (boiling point: 139 ° C), Examples thereof include dimethylformamide (boiling point: 153 ° C.) and butyl carbitol (boiling point: 230 ° C.). These may be used alone or in combination.
- the surface to be formed of the film-like fired material includes the surface of a release film.
- the firing material composition may be applied by a known method, for example, an air knife coater, a blade coater, a bar coater, a gravure coater, a comma (registered trademark) coater, a roll coater, a roll knife coater, a curtain coater, or a die coater. And a method using various coaters such as a coater, a knife coater, a screen coater, a Meyer bar coater, and a kiss coater.
- a known method for example, an air knife coater, a blade coater, a bar coater, a gravure coater, a comma (registered trademark) coater, a roll coater, a roll knife coater, a curtain coater, or a die coater.
- various coaters such as a coater, a knife coater, a screen coater, a Meyer bar coater, and a kiss coater.
- the drying conditions of the fired material composition are not particularly limited, but when the fired material composition contains a solvent, it is preferably heated and dried. In this case, for example, 70 to 250 ° C., for example, 80 to 180 ° C., It is preferable to dry under conditions of 10 seconds to 10 minutes.
- the film-like fired material with a support sheet of the embodiment includes the film-like fired material and a support sheet provided on at least one side of the film-like fired material.
- the support sheet is provided with a pressure-sensitive adhesive layer on the entire surface or on the outer periphery of the base film, and the film-like fired material is preferably provided on the pressure-sensitive adhesive layer.
- the film-like fired material may be provided in direct contact with the pressure-sensitive adhesive layer, or may be provided in direct contact with the base film. By taking this form, it can be used as a dicing sheet used when a semiconductor wafer is separated into elements. In addition, by using a blade or the like to separate into pieces together with the wafer, it can be processed as a film-like fired material having the same shape as the element, and a semiconductor element with a film-like fired material can be manufactured.
- FIG. 4 and 5 are schematic cross-sectional views of the film-like fired material with a support sheet of the present embodiment.
- the film-like fired material 100 a, 100 b of the present embodiment can peel the film-like fired material 1 on the inner peripheral part of the support sheet 2 having an adhesive part on the outer peripheral part. It is temporarily attached to.
- the support sheet 2 is a pressure-sensitive adhesive sheet having a pressure-sensitive adhesive layer 4 on the upper surface of the base film 3, and the inner peripheral surface of the pressure-sensitive adhesive layer 4 is covered with a film-like baking material, It becomes the structure which the adhesion part exposed to the outer peripheral part.
- the support sheet 2 may have a configuration having a ring-shaped pressure-sensitive adhesive layer 4 on the outer peripheral portion of the base film 3.
- the film-like fired material 1 is formed on the inner peripheral part of the support sheet 2 in substantially the same shape as the work (semiconductor wafer or the like) to be stuck.
- the support sheet 2 has an adhesive portion on the outer peripheral portion.
- the film-like fired material 1 having a smaller diameter than the support sheet 2 is concentrically laminated on the circular support sheet 2.
- the adhesive portion on the outer peripheral portion is used for fixing the ring frame 5 as illustrated.
- the base film 3 is not particularly limited.
- low density polyethylene LDPE
- linear low density polyethylene LLDPE
- ethylene / propylene copolymer polypropylene, polybutene, polybutadiene, polymethylpentene, ethylene / vinyl acetate.
- Copolymer ethylene / (meth) acrylic acid copolymer, ethylene / (meth) methyl acrylate copolymer, ethylene / (meth) ethyl acrylate copolymer, polyvinyl chloride, vinyl chloride / vinyl acetate copolymer
- a film made of coalescence, polyurethane film, ionomer or the like is used.
- “(meth) acryl” is used to mean both acrylic and methacrylic.
- the base film 3 includes polyester films such as polyethylene terephthalate, polybutylene terephthalate, and polyethylene naphthalate, and polyolefin films such as polypropylene and polymethylpentene. Can be mentioned. In addition, these cross-linked films and modified films by radiation and discharge can also be used.
- the base film may be a laminate of the above films.
- these films can be used by laminating or combining two or more kinds. Furthermore, the thing which colored these films, or what gave printing etc. can be used.
- the film may be a sheet formed by extrusion molding of a thermoplastic resin, or may be a stretched film. A film obtained by thinning and curing a curable resin by a predetermined means is used. It may be broken.
- the thickness of the base film is not particularly limited, and is preferably 30 to 300 ⁇ m, more preferably 50 to 200 ⁇ m. By making the thickness of the base film within the above range, the base film is hardly broken even if cutting is performed by dicing. In addition, since sufficient flexibility is imparted to the film-like fired material with a support sheet, good sticking property to a workpiece (for example, a semiconductor wafer) is exhibited.
- the base film can also be obtained by applying a release agent on the surface and performing a release treatment.
- a release agent used for the release treatment, alkyd, silicone, fluorine, unsaturated polyester, polyolefin, wax, and the like are used.
- alkyd, silicone, and fluorine release agents are heat resistant. This is preferable.
- the release agent is used without a solvent, or diluted or emulsified with a solvent, and a gravure coater, a Mayer bar coater, an air knife coater, a roll coater, etc.
- the substrate film on which the release agent is applied is applied at room temperature or under heating, or cured by electron beam, wet lamination, dry lamination, hot melt lamination, melt extrusion lamination, coextrusion processing, etc.
- the laminate may be formed with
- the support sheet 2 has an adhesive portion at least on the outer periphery thereof.
- the adhesive portion has a function of temporarily fixing the ring frame 5 at the outer peripheral portions of the film-like fired materials 100a and 100b with a support sheet, and it is preferable that the ring frame 5 can be peeled off after a required process.
- the pressure-sensitive adhesive layer 4 may be weakly adhesive, or may be energy-ray curable, whose adhesive strength is reduced by irradiation with energy rays.
- the re-peelable pressure-sensitive adhesive layer is made of various conventionally known pressure-sensitive adhesives (for example, rubber-based, acrylic-based, silicone-based, urethane-based, vinyl ether-based general-purpose pressure-sensitive adhesives, pressure-sensitive adhesives, energy ray curable type) Adhesive, thermal expansion component-containing adhesive, etc.).
- pressure-sensitive adhesives for example, rubber-based, acrylic-based, silicone-based, urethane-based, vinyl ether-based general-purpose pressure-sensitive adhesives, pressure-sensitive adhesives, energy ray curable type Adhesive, thermal expansion component-containing adhesive, etc.
- the support sheet 2 is a pressure-sensitive adhesive sheet having a normal structure having a pressure-sensitive adhesive layer 4 on the entire upper surface of the base film 3, and the inner peripheral surface of the pressure-sensitive adhesive layer 4 is a film-like fired material. It may be the structure which was covered with and the adhesion part was exposed to the outer peripheral part. In this case, the outer peripheral portion of the pressure-sensitive adhesive layer 4 is used for fixing the ring frame 5 described above, and a film-like fired material is laminated on the inner peripheral portion in a peelable manner.
- a weakly-adhesive layer may be used as described above, or an energy ray-curable pressure-sensitive adhesive may be used.
- the ring-shaped adhesive layer 4 is formed in the outer peripheral part of the base film 3, and it is set as an adhesion part.
- the pressure-sensitive adhesive layer 4 may be a single-layer pressure-sensitive adhesive layer made of the above-mentioned pressure-sensitive adhesive, or may be one obtained by circularly cutting a double-sided pressure-sensitive adhesive tape including a pressure-sensitive adhesive layer made of the above-mentioned pressure-sensitive adhesive.
- the adhesive strength of the adhesive layer 4 to the SUS plate at 23 ° C. is preferably 30 to 120 mN / 25 mm, and preferably 50 to 100 mN / 25 mm. Is more preferable, and 60 to 90 mN / 25 mm is more preferable. If the adhesive strength is too low, the adhesiveness between the film-like fired material 1 and the pressure-sensitive adhesive layer 4 becomes insufficient, and the film-like fired material and the pressure-sensitive adhesive layer are peeled off during the dicing process, or the ring frame falls off. There are things to do. On the other hand, if the adhesive strength is too high, the film-like fired material and the pressure-sensitive adhesive layer are excessively adhered to each other, which causes a pickup failure.
- the region where the film-like fired material is laminated may be irradiated with energy rays in advance to reduce the adhesiveness. Good.
- the other regions may not be irradiated with energy rays, and may be maintained with a high adhesive force for the purpose of adhesion to the ring frame 5, for example.
- an energy ray shielding layer is provided by printing or the like in regions corresponding to other regions of the substrate film, and energy rays are irradiated from the substrate film side. Just do it.
- the surface in which the adhesive layer 4 of the base film 3 is provided may be sandblasted, if desired.
- Irregularizing treatment such as solvent treatment, or corona discharge treatment, electron beam irradiation, plasma treatment, ozone / ultraviolet irradiation treatment, flame treatment, chromic acid treatment, hot air treatment, or other oxidation treatment can be performed.
- primer treatment can also be performed.
- the thickness of the pressure-sensitive adhesive layer 4 is not particularly limited, but is preferably 1 to 100 ⁇ m, more preferably 2 to 80 ⁇ m, and particularly preferably 3 to 50 ⁇ m.
- the film-like fired material with a support sheet is formed by temporarily attaching the film-like fired material to the inner periphery of a support sheet having an adhesive part on the outer periphery.
- the film-like fired material 100a with a support sheet is laminated so that the film-like fired material 1 can be peeled on the inner peripheral portion of the support sheet 2 composed of the base film 3 and the pressure-sensitive adhesive layer 4.
- the pressure-sensitive adhesive layer 4 is exposed on the outer periphery of the support sheet 2.
- it is preferable that the film-like fired material 1 having a smaller diameter than the support sheet 2 is laminated on the pressure-sensitive adhesive layer 4 of the support sheet 2 so as to be peeled in a concentric manner.
- the film-shaped baking material 100a with a support sheet having the above-described configuration is attached to the ring frame 5 in the pressure-sensitive adhesive layer 4 exposed on the outer periphery of the support sheet 2.
- annular double-sided tape or an adhesive layer may be separately provided on the margin for the ring frame (exposed adhesive layer on the outer periphery of the adhesive sheet).
- the double-sided tape has a configuration of pressure-sensitive adhesive layer / core material / pressure-sensitive adhesive layer, and the pressure-sensitive adhesive layer in the double-sided tape is not particularly limited. For example, rubber-based, acrylic-based, silicone-based, polyvinyl ether, or the like is used. .
- the adhesive layer is affixed to the ring frame at the outer periphery when an element described later is manufactured.
- a polyester film for example, a polyester film, a polypropylene film, a polycarbonate film, a polyimide film, a fluororesin film, a liquid crystal polymer film and the like are preferably used.
- a ring-shaped adhesive layer 4 is formed on the outer peripheral portion of the base film 3 to form an adhesive portion.
- the pressure-sensitive adhesive layer 4 may be a single-layer pressure-sensitive adhesive layer made of the above-mentioned pressure-sensitive adhesive, or may be one obtained by circularly cutting a double-sided pressure-sensitive adhesive tape including a pressure-sensitive adhesive layer made of the above-mentioned pressure-sensitive adhesive.
- the film-like fired material 1 is detachably laminated on the inner peripheral part of the base film 3 surrounded by the adhesive part. In this configuration example, it is preferable that the film-shaped fired material 1 having a smaller diameter than the support sheet 2 is laminated on the base film 3 of the support sheet 2 so as to be concentrically peelable.
- the film-like fired material with a support sheet is a release film for the purpose of protecting the surface of either the film-like fired material and / or the adhesive part, or both, until they are used. May be provided.
- a surface protective film As a surface protective film (release film), it can also be obtained by applying a release agent to the surface of a base film such as polyethylene, polyethylene terephthalate, polybutylene terephthalate, polyethylene naphthalate and polypropylene mentioned above and applying a release treatment. it can.
- a release agent used for the release treatment alkyd, silicone, fluorine, unsaturated polyester, polyolefin, wax, and the like are used.
- alkyd, silicone, and fluorine release agents are heat resistant. This is preferable.
- the release agent is used without a solvent, or diluted or emulsified with a solvent, and a gravure coater, a Mayer bar coater, an air knife coater, a roll coater, etc.
- the substrate film on which the release agent is applied is applied at room temperature or under heating, or cured by electron beam, wet lamination, dry lamination, hot melt lamination, melt extrusion lamination, coextrusion processing, etc.
- the laminate may be formed with
- the thickness of the film-like fired material with a support sheet is preferably 1 to 500 ⁇ m, more preferably 5 to 300 ⁇ m, and even more preferably 10 to 150 ⁇ m.
- the film-like fired material with a support sheet can be produced by sequentially laminating the above-described layers so as to have a corresponding positional relationship. For example, when laminating a pressure-sensitive adhesive layer or a film-like fired material on a base film, a pressure-sensitive adhesive composition or a fired material composition containing a component and a solvent for constituting the film is applied onto the release film.
- the pressure-sensitive adhesive layer or film-like fired material is formed in advance on the release film by drying and volatilizing the solvent as necessary to form a film, and this formed pressure-sensitive adhesive layer or film What is necessary is just to bond the exposed surface on the opposite side to the side which is contacting the said peeling film of a baking material with the surface of a base film.
- the pressure-sensitive adhesive composition or the baking material composition is preferably applied to the release-treated surface of the release film.
- the release film may be removed as necessary after forming the laminated structure.
- a film-like fired material with a support sheet in which a pressure-sensitive adhesive layer is laminated on a base film, and a film-like fired material is laminated on the pressure-sensitive adhesive layer (the support sheet is a laminate of the base film and the pressure-sensitive adhesive layer)
- the adhesive layer is laminated on the base film by the above-described method, and the components for constituting this separately on the release film and A film-shaped fired material is formed on a release film by applying a fired material composition containing a solvent, drying as necessary, and volatilizing the solvent to form a film.
- a film-like fired material with a support sheet is obtained by laminating the exposed surface of the film with the exposed surface of the pressure-sensitive adhesive layer laminated on the substrate and laminating the film-like fired material on the pressure-sensitive adhesive layer. Even when the film-like fired material is formed on the release film, the fired material composition is preferably applied to the release-treated surface of the release film, and the release film can be removed as necessary after forming the laminated structure. Good.
- all layers other than the base material constituting the film-like fired material with a support sheet can be laminated by a method in which the layers are formed in advance on the release film and bonded to the surface of the target layer. Accordingly, a layer employing such a process may be appropriately selected to produce a film-like fired material with a support sheet.
- the film-like fired material with a support sheet may be stored in a state in which a release film is bonded to the surface of the outermost layer opposite to the support sheet.
- a method for producing a semiconductor element using a film-like fired material with a support sheet comprises a semiconductor wafer (workpiece) having a circuit formed on the surface by peeling off the release film of the film-like fired material with a support sheet.
- the film-like fired material with a support sheet is affixed to the back surface of (), and the following steps (1) to (2) may be carried out in the order of (1) and (2).
- (4) may be performed in the order of (1), (2), (3), and (4).
- Step (1) a step of dicing the semiconductor wafer (work) and the film-like fired material of the laminate in which the support sheet, the film-like fired material, and the semiconductor wafer (work) are laminated in this order
- Step (2) A step of peeling the film-like fired material and the support sheet to obtain an element with the film-like fired material
- Step (3) A step of attaching an element with a film-like fired material to the surface of the adherend
- the semiconductor wafer may be a silicon wafer and a silicon carbide wafer, or may be a compound semiconductor wafer such as gallium / arsenic. Formation of a circuit on the wafer surface can be performed by various methods including conventionally used methods such as an etching method and a lift-off method. Next, the opposite surface (back surface) of the circuit surface of the semiconductor wafer is ground.
- the grinding method is not particularly limited, and grinding may be performed by a known means using a grinder or the like. At the time of back surface grinding, an adhesive sheet called a surface protection sheet is attached to the circuit surface in order to protect the circuit on the surface.
- the circuit surface side (that is, the surface protection sheet side) of the wafer is fixed by a chuck table or the like, and the back surface side on which no circuit is formed is ground by a grinder.
- the thickness of the wafer after grinding is not particularly limited, but is usually about 20 to 500 ⁇ m.
- the crushed layer generated during back grinding is removed.
- the crushed layer is removed by chemical etching, plasma etching, or the like.
- steps (1) to (4) are performed in the order of (1), (2), (3), and (4).
- the semiconductor wafer / film-like fired material / support sheet laminate is diced for each circuit formed on the wafer surface to obtain a semiconductor element / film-like fired material / support sheet laminate.
- Dicing is performed so as to cut both the wafer and the film-like fired material.
- the film-like fired material with a support sheet of this embodiment since the adhesive force is exhibited between the film-like fired material and the support sheet during dicing, chipping and element jumping can be prevented, and dicing suitability can be achieved. Excellent.
- the dicing is not particularly limited. For example, after dicing the wafer, the periphery of the support sheet (the outer periphery of the support) is fixed by a ring frame, and then a known method such as using a rotating round blade such as a dicing blade is used. For example, a method for dividing a wafer into individual pieces may be used.
- the cutting depth into the support sheet by dicing may be obtained by completely cutting the film-like fired material, and is preferably 0 to 30 ⁇ m from the interface between the film-like fired material and the support sheet.
- the support sheet may be expanded.
- the support sheet has excellent expandability.
- the film-like fired material and the support sheet are peeled off by picking up the diced semiconductor element with the film-like fired material by a general-purpose means such as a collet. As a result, a semiconductor element having a film-like fired material on the back surface (semiconductor element with a film-like fired material) is obtained.
- an element with a film-like fired material is attached to the surface of an adherend such as a substrate, a lead frame, or a heat sink.
- an adherend such as a substrate, a lead frame, or a heat sink.
- the film-like fired material is fired, and a substrate, a lead frame, an adherend such as a heat sink, and the element are sintered and joined.
- the exposed surface of the film-like fired material of the semiconductor element with the film-like fired material is attached to an adherend such as a substrate, a lead frame, or a heat sink, the semiconductor wafer (work) and The adherend can be sintered and joined.
- the heating temperature for firing the film-like fired material may be appropriately determined in consideration of the type of the film-like fired material, etc., but is preferably 100 to 600 ° C, more preferably 150 to 550 ° C, and further preferably 250 to 500 ° C. preferable.
- the heating time may be appropriately determined in consideration of the type of the film-like fired material, etc., preferably 10 seconds to 60 minutes, more preferably 10 seconds to 30 minutes, and further preferably 10 seconds to 10 minutes.
- the firing of the film-like fired material may be performed by pressure firing in which the film-like fired material is fired under pressure.
- the pressurizing condition may be about 1 to 50 MPa.
- a film-like fired material with high uniformity in thickness can be easily formed on the back surface of the device, and cracks after the dicing process and packaging are less likely to occur.
- a semiconductor element with a film-like fired material can be obtained without individually attaching the film-like fired material to the individualized semiconductor element back surface. Simplification can be achieved. Then, the semiconductor element with the film-like fired material is placed on a desired adherend such as a device substrate and fired to sinter-bond the semiconductor element and the adherend via the film-like fired material.
- a semiconductor device can be manufactured.
- a semiconductor element with a film-like fired material comprising a semiconductor element and the film-like fired material is obtained.
- the semiconductor element with a film-like fired material can be manufactured by the above-described element manufacturing method.
- the sintering joining object of a film-like baking material is not limited to what was illustrated above, Sinter bonding is possible for various articles sintered in contact with the film-like fired material.
- ⁇ Manufacture of firing material composition The components used for the production of the fired material composition are shown below.
- metal particles having a particle diameter of 100 nm or less are expressed as “sinterable metal particles”, and metal particles having a particle diameter exceeding 100 nm are expressed as “non-sinterable metal particles”.
- Arconano silver paste ANP-1 Organic coated composite silver nanopaste, Applied Nanoparticles Laboratory Co., Ltd .: Alcohol derivative-coated silver particles, metal content 70 wt% or more, average particle diameter 100 nm or less silver particles 60 wt% or more
- Arconano silver paste ANP-4 Organic coated composite silver nanopaste, Applied Nanoparticles Laboratory Co., Ltd .: Alcohol derivative-coated silver particles, metal content of 80 wt% or more, average particle size of 100 nm or less of silver particles of 25 wt% or more
- Acrylic polymer 1 (2-ethylhexyl methacrylate polymer, weight average molecular weight 280,000, L-0818, manufactured by Nippon Synthetic Chemical Co., Ltd., MEK diluted product, solid content 54.5% by mass, Tg: ⁇ 10 ° C.
- each component was mixed in the composition shown in Table 1 below to obtain fired material compositions corresponding to Examples 1-2 and Comparative Examples 1-2.
- the value of each component in Table 1 represents parts by mass. Since the sinterable metal particle-containing paste material is sold containing a high boiling point solvent and remains in the film-like firing material after coating or drying, the components of the sinterable metal particle-containing paste material Includes these. Considering that the solvent in the binder component volatilizes during drying, it represents the mass part of solid content excluding the solvent component.
- the fired material composition obtained above is applied to one side of a release film (thickness 38 ⁇ m, SP-PET 381031, manufactured by Lintec Corporation) and dried at 110 ° C. for 4 minutes to have the thicknesses shown in Table 1. A film-like fired material was obtained.
- Table 1 shows the time (A1) after the start of temperature increase with the largest negative slope in the TG curve and the maximum peak time (B1) in the time range from 0 seconds to 2160 seconds after the start of temperature increase in the DTA curve. Shown in In addition, with respect to the component obtained by removing the sinterable metal particles and non-sinterable metal particles from the film-like fired material by the separation method, the time (A1) after the start of temperature increase with the largest negative slope in the TG curve Table 1 shows ') and the peak time (B1') observed in the shortest time among the peaks observed in the time range from 960 seconds to 2160 seconds after the start of temperature increase in the DTA curve.
- the temperature (A2 ′) having the largest negative slope in the TG curve, and DTA Table 1 shows the peak temperature (B2 ′) observed at the lowest temperature among the peaks observed in the temperature range of 200 ° C. to 400 ° C. in the curve.
- the shear adhesive strength after firing of the film-like fired material was measured by the following method.
- the film-like fired material obtained above was cut into 10 mm ⁇ 10 mm, and this was pasted on the top surface of a cylindrical copper adherend having a height of 5 mm having a cross section of 10 mm in diameter, and a 5 mm diameter on it.
- a cylindrical copper adherend with a height of 2 mm with a cross-section is placed on it and fired under pressure in the air or nitrogen atmosphere under the following conditions (1) to (3) for bonding adhesive strength measurement A specimen was obtained.
- the film-like fired materials of Examples 1 and 2 had higher shear adhesion than the fired materials of Comparative Examples 1 and 2.
- a film-like fired material that is excellent in thickness stability and thermal conductivity and exhibits excellent shear adhesion after firing.
- a film-like fired material with a support sheet which is provided with the film-like fired material and is used for sintered joining of semiconductor elements, can be provided.
- SYMBOLS 1 Film-like baking material, 1c ... Baking material, 10, 11 ... Sinterable metal particle, 20, 21 ... Binder component, 100 ... Film-like baking material with a support sheet, 2 ... Support sheet, 3 ... Base film, 4 ... Adhesive layer, 5 ... Ring frame
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Abstract
Description
本願は、2017年4月28日に日本に出願された特願2017-090714号、2017年9月20日に日本に出願された特願2017-179797号、及び、2017年10月2日に日本に出願された特願2017-192821号に基づき優先権を主張し、その内容をここに援用する。
従来、半導体素子から発生した熱の放熱のため、半導体素子の周りにヒートシンクが取り付けられる場合もある。しかし、ヒートシンクと半導体素子との間の接合部での熱伝導性が良好でなければ、効率的な放熱が妨げられてしまう。
本発明は、上記のような実状に鑑みてなされたものであり、厚さ安定性及び熱伝導性に優れ、焼成後に優れたせん断接着力を発揮するフィルム状焼成材料を提供することを目的とする。また、前記フィルム状焼成材料を備えた支持シート付フィルム状焼成材料を提供することを目的とする。
[1] 焼結性金属粒子及びバインダー成分を含有するフィルム状焼成材料であって、
大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい昇温開始後の時間(A1)と、
アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)における、昇温開始後0秒から2160秒の時間範囲での最大ピーク時間(B1)とが、
A1<B1<A1+200秒の関係を満たし、且つ、A1<2000秒である、フィルム状焼成材料。
[2] フィルム状焼成材料から前記焼結性金属粒子を除いた成分について、大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい昇温開始後の時間(A1’)と、
前記焼結性金属粒子について、アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)における、昇温開始後960秒から2160秒の時間範囲で観測されるピークの内、最短時間で観測されるピーク時間(B1’)とが、
B1’<A1’の関係を満たす、前記[1]に記載のフィルム状焼成材料。
[3] 前記フィルム状焼成材料について、アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)において、昇温開始後0秒から2160秒の時間範囲での吸熱ピークを有さない、前記[1]又は[2]に記載のフィルム状焼成材料。
窒素雰囲気下10℃/分の昇温速度で測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい温度(A2)と、
アルミナ粒子を参照試料として窒素雰囲気下10℃/分の昇温速度で測定された示差熱分析曲線(DTA曲線)における、25℃から400℃の温度範囲での最大ピーク温度(B2)とが、
A2<B2<A2+60℃の関係を満たす、フィルム状焼成材料。
[5] フィルム状焼成材料から前記焼結性金属粒子を除いた成分について、窒素雰囲気下10℃/分の昇温速度で測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい温度(A2’)と、
前記焼結性金属粒子について、アルミナ粒子を参照試料として窒素雰囲気下10℃/分の昇温速度で測定された示差熱分析曲線(DTA曲線)における、200℃から400℃の温度範囲で観測されるピークの内、最も低温で観測されるピーク温度(B2’)とが、
B2’<A2’の関係を満たす、前記[4]に記載のフィルム状焼成材料。
[6] 前記フィルム状焼成材料について、アルミナ粒子を参照試料として窒素雰囲気下10℃/分の昇温速度で測定された示差熱分析曲線(DTA曲線)において、25℃から400℃の温度範囲での吸熱ピークを有さない、前記[4]又は[5]に記載のフィルム状焼成材料。
[8] 前記[1]~[7]のいずれか一つに記載のフィルム状焼成材料と、前記フィルム状焼成材料の少なくとも一方の側に設けられた支持シートと、を備えた支持シート付フィルム状焼成材料。
[9] 前記支持シートが、基材フィルム上に粘着剤層が設けられたものであり、
前記粘着剤層上に、前記フィルム状焼成材料が設けられている、前記[8]に記載の支持シート付フィルム状焼成材料。
なお、以下の説明で用いる図は、本発明の特徴を分かり易くするために、便宜上、要部となる部分を拡大して示している場合があり、各構成要素の寸法比率等が実際と同じであるとは限らない。
第一実施形態のフィルム状焼成材料は、焼結性金属粒子及びバインダー成分を含有するフィルム状焼成材料であって、大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい昇温開始後の時間(A1)と、アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)における、昇温開始後0秒から2160秒の時間範囲での最大ピーク時間(B1)とがA1<B1<A1+200秒の関係を満たし、且つ、A1<2000秒であるものである。
図1は、第一実施形態及び第二実施形態のフィルム状焼成材料を模式的に示す断面図である。フィルム状焼成材料1は、焼結性金属粒子10及びバインダー成分20を含有している。
なお、本明細書においては、フィルム状焼成材料の場合に限らず、「複数層が互いに同一でも異なっていてもよい」とは、「すべての層が同一であってもよいし、すべての層が異なっていてもよく、一部の層のみが同一であってもよい」ことを意味し、さらに「複数層が互いに異なる」とは、「各層の構成材料、構成材料の配合比、及び厚さの少なくとも一つが互いに異なる」ことを意味する。
ここで、「フィルム状焼成材料の厚さ」とは、フィルム状焼成材料全体の厚さを意味し、例えば、複数層からなるフィルム状焼成材料の厚さとは、フィルム状焼成材料を構成するすべての層の合計の厚さを意味する。
フィルム状焼成材料は、剥離フィルム上に積層された状態で提供することができる。使用する際には、剥離フィルムを剥がし、フィルム状焼成材料を焼結接合させる対象物上に配置すればよい。剥離フィルムはフィルム状焼成材料の損傷や汚れ付着を防ぐための保護フィルムとしての機能も有する。剥離フィルムは、フィルム状焼成材料の少なくとも一方の側に設けられていればよく、フィルム状焼成材料の両方の側に設けられてよい。
焼結性金属粒子は、フィルム状焼成材料の焼成として加熱処理されることで粒子同士が溶融・結合して焼結体を形成可能な金属粒子である。焼結体を形成することで、フィルム状焼成材料とそれに接して焼成された物品とを焼結接合させることが可能である。
上記粒子径の範囲に属する金属粒子は、焼結性に優れるため好ましい。
フィルム状焼成材料が含む焼結性金属粒子の粒子径は、電子顕微鏡で観察された金属粒子の粒子径の、投影面積円相当径が100nm以下の粒子に対して求めた粒子径の数平均が、0.1~95nmであってよく、0.3~50nmであってよく、0.5~30nmであってよい。なお、測定対象の金属粒子は、1つのフィルム状焼成材料あたり無作為に選ばれた100個以上とする。
分散法としてはニーダ、三本ロール、ビーズミルおよび超音波などが挙げられる。
なお、本明細書において、「常温」とは、特に冷やしたり、熱したりしない温度、すなわち平常の温度を意味し、例えば、15~25℃の温度等が挙げられる。
粒子径100nm以下の金属粒子と、粒子径が100nmを超える非焼結性の金属粒子とは、互いに同一の金属種であってもよく、互いに異なる金属種であってもよい。例えば、粒子径100nm以下の金属粒子が銀粒子であり、粒子径が100nmを超える非焼結性の金属粒子が銀又は酸化銀粒子であってもよい。例えば、粒子径100nm以下の金属粒子が銀又は酸化銀粒子であり、粒子径が100nmを超える非焼結性の金属粒子が銅又は酸化銅粒子であってもよい。
焼結性金属粒子及び非焼結性の金属粒子の少なくとも一方の表面に有機物が被覆されている場合、焼結性金属粒子及び非焼結性の金属粒子の質量は、被覆物を含んだ値とする。
バインダー成分が配合されることで、焼成材料をフィルム状に成形でき、焼成前のフィルム状焼成材料に粘着性を付与することができる。バインダー成分は、フィルム状焼成材料の焼成として加熱処理されることで熱分解される熱分解性であってよい。
バインダー成分は特に限定されるものではないが、バインダー成分の好適な一例として、樹脂が挙げられる。樹脂としては、アクリル系樹脂、ポリカーボネート樹脂、ポリ乳酸、セルロース誘導体の重合物等が挙げられ、アクリル系樹脂が好ましい。アクリル系樹脂には、(メタ)アクリレート化合物の単独重合体、(メタ)アクリレート化合物の2種以上の共重合体、(メタ)アクリレート化合物と他の共重合性単量体との共重合体が含まれる。
ここでいう「由来」とは、前記モノマーが重合するのに必要な構造の変化を受けたことを意味する。
アクリル樹脂としては、メタクリレートが好ましい。バインダー成分がメタクリレート由来の構成単位を含有することで、前記時間(A1)と前記時間(B1)とがA1<B1<A1+200秒の関係を有し、A1<2000秒となるフィルム状焼成材料が得られやすい。また、バインダー成分がメタクリレート由来の構成単位を含有することで、前記温度(A2)と前記温度(B2)とがA2<B2<A2+60℃の関係を有するフィルム状焼成材料が得られやすい。
1/Tg=(W1/Tg1)+(W2/Tg2)+…+(Wm/Tgm)
W1+W2+…+Wm=1
の関係を示す。式中、Tgは重合体部分のガラス転移温度を表わし、Tg1,Tg2,…,Tgmは各重合単量体のガラス転移温度を表わす。また、W1,W2,…,Wmは各重合単量体の重量比率を表わす。
前記実施形態のフィルム状焼成材料は、焼結性金属粒子、バインダー成分、及びその他の添加剤からなるものであってもよく、これらの含有量(質量%)の和は100質量%となってよい。
前記実施形態のフィルム状焼成材料が非焼結性の金属粒子を含む場合には、フィルム状焼成材料は、焼結性金属粒子、非焼結性の金属粒子、バインダー成分、及びその他の添加剤からなるものであってもよく、これらの含有量(質量%)の和は100質量%となってよい。
フィルム状焼成材料が非焼結性の金属粒子を含む場合、フィルム状焼成材料における固形分の総含有量100質量%に対する、焼結性金属粒子及び非焼結性の金属粒子の総含有量は、50~98質量%が好ましく、70~95質量%がより好ましく、80~90質量%がさらに好ましい。
第一実施形態のフィルム状焼成材料が上記に示す組成を有することにより、前記時間(A1)と前記時間(B1)とがA1<B1<A1+200秒の関係を有し、A1<2000秒となるフィルム状焼成材料が得られやすい。
第一実施形態のフィルム状焼成材料は、大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい昇温開始後の時間(A1)と、アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)における、昇温開始後0秒から2160秒の時間範囲での最大ピーク時間(B1)とが、A1<B1<A1+200秒の関係を満たし、A1<2000秒であるものである。
上記DTA曲線は、大気雰囲気下、フィルム状焼成材料が加熱処理される過程での、フィルム状焼成材料の示差熱変化を表したものである。
焼成前のフィルム状焼成材料(図2(a))に含まれているバインダー成分20は、加熱により重量が減少していき(図2(b)~(c))、この現象は、TG曲線における負の傾きとして表れる。
A1<B1<A1+200秒の関係を満たさず、B1の時間がA1+200秒よりも大きい焼成材料では、塊状になった焼結性金属粒子が焼結されることで、焼結が十分でない場合や、焼結していない箇所が多く残ることとなり、焼結後の材料は接着強度(せん断接着力の強度)に乏しいものになることが考えられる。または、被着体との接着界面において空隙が発生し易くなり、接着面積が小さくなってしまうことで接着強度が低下することが考えられる。
対して、A1<B1<A1+200秒の関係を満たし、且つA1<2000秒であるフィルム状焼成材料では、バインダー成分が存在している状態で、微粒子状のまま融解した焼結性金属粒子が焼結されることで、焼結性金属同士が一様に密に金属結合することとなり、焼結後の材料の接着強度の向上が生じると考えられる。
第一実施形態のフィルム状焼成材料は、フィルム状焼成材料から前記焼結性金属粒子を除いた成分について、大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい昇温開始後の時間(A1’)と、前記焼結性金属粒子について、アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)における、昇温開始後960秒から2160秒の時間範囲で観測されるピークの内、最短時間で観測されるピーク時間(B1’)とが、B1’<A1’の関係を満たすことが好ましい。
上記DTA曲線は、大気雰囲気下、焼成として加熱処理される過程での、焼結性金属粒子の示差熱変化を表したものである。
焼成前のフィルム状焼成材料に含まれていた焼結性金属粒子は、大気雰囲気下、加熱により融解と焼結が生じ、融解現象はDTA曲線における負のピーク、焼結現象はDTA曲線における正のピークとして表れる。
焼成前のフィルム状焼成材料からの焼結性金属粒子と、前記焼結性金属粒子を除いた残りの成分との分離は、例えば、以下の方法により行うことができる。
まず、焼成前のフィルム状焼成材料と、十分量の有機溶媒とを混合した後にこれを焼結性金属粒子が沈降するまで十分な時間、静置する。この上澄み液をシリンジ等で抜き取り、120℃10分で乾燥した後の残留物を回収することで、フィルム状焼成材料から前記焼結性金属粒子を除いた成分を分取できる。また上記シリンジ等で上澄み液を抜き取った後の焼結性金属粒子が含まれる液に対して、再び十分量の有機溶媒を混合した後にこれを焼結性金属粒子が沈降するまで十分な時間、静置し、上澄み液をシリンジ等で抜き取る。
この有機溶媒の混合と静置および上澄み液の抜き取りを5回以上繰り返した後、残った液を120℃10分で乾燥した後の残留物を回収することで、焼結性金属粒子を分取することが可能である。
焼成前のフィルム状焼成材料からの焼結性金属粒子及び非焼結性の金属粒子と、前記焼結性金属粒子及び非焼結性の金属粒子を除いた残りの成分との分離は、例えば、以下の方法により行うことができる。
第一実施形態のフィルム状焼成材料は、前記フィルム状焼成材料について、アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)において、昇温開始後0秒から2160秒の時間範囲での吸熱ピークを有さないことが好ましい。
第二実施形態のフィルム状焼成材料が上記に示す組成を有することにより、前記温度(A2)と前記温度(B2)とがA2<B2<A2+60℃の関係を有するフィルム状焼成材料が得られやすい。
第二実施形態のフィルム状焼成材料は、窒素雰囲気下10℃/分の昇温速度で測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい温度(A2)と、アルミナ粒子を参照試料として窒素雰囲気下10℃/分の昇温速度で測定された示差熱分析曲線(DTA曲線)における、25℃から400℃の温度範囲での最大ピーク温度(B2)とが、A2<B2<A2+60℃の関係を満たすものである。
上記DTA曲線は、窒素雰囲気下、フィルム状焼成材料が加熱処理される過程での、フィルム状焼成材料の示差熱変化を表したものである。
焼成前のフィルム状焼成材料(図2(a))に含まれているバインダー成分20は、加熱により重量が減少していき(図2(b)~(c))、この現象は、TG曲線における負の傾きとして表れる。
第二実施形態のフィルム状焼成材料は、フィルム状焼成材料から前記焼結性金属粒子を除いた成分について、窒素雰囲気下10℃/分の昇温速度で測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい温度(A2’)と、前記焼結性金属粒子について、アルミナ粒子を参照試料として窒素雰囲気下10℃/分の昇温速度で測定された示差熱分析曲線(DTA曲線)における、200℃から400℃の温度範囲で観測されるピークの内、最も低温で観測されるピーク温度(B2’)とが、B2’<A2’の関係を満たすことが好ましい。
上記DTA曲線は、窒素雰囲気下、焼成として加熱処理される過程での、焼結性金属粒子の示差熱の温度変化を表したものである。
焼成前のフィルム状焼成材料からの焼結性金属粒子と、前記焼結性金属粒子を除いた残りの成分との分離は、例えば、以下の方法により行うことができる。
まず、焼成前のフィルム状焼成材料と、十分量の有機溶媒とを混合した後にこれを焼結性金属粒子が沈降するまで十分な時間、静置する。この上澄み液をシリンジ等で抜き取り、120℃10分で乾燥した後の残留物を回収することで、フィルム状焼成材料から前記焼結性金属粒子を除いた成分を分取できる。また上記シリンジ等で上澄み液を抜き取った後の焼結性金属粒子が含まれる液に対して、再び十分量の有機溶媒を混合した後にこれを焼結性金属粒子が沈降するまで十分な時間、静置し、上澄み液をシリンジ等で抜き取る。
焼成前のフィルム状焼成材料からの焼結性金属粒子及び非焼結性の金属粒子と、前記焼結性金属粒子及び非焼結性の金属粒子を除いた残りの成分との分離は、例えば、以下の方法により行うことができる。
第二実施形態のフィルム状焼成材料は、前記フィルム状焼成材料について、アルミナ粒子を参照試料として窒素雰囲気下10℃/分の昇温速度で測定された示差熱分析曲線(DTA曲線)において、25℃から400℃の温度範囲での吸熱ピークを有さないことが好ましい。
したがって、第二実施形態のフィルム状焼成材料には、25℃から400℃でフィルム状焼成材料から蒸発する性質を有する成分の含有量が少ない又は含まれていないことが好ましい。また熱分解に多くの熱量を吸収し、焼結による発熱過程を妨げる成分の含有量が少ない又は含まれていないことが好ましい。
フィルム状焼成材料は、その構成材料を含有する焼成材料組成物を用いて形成できる。
例えば、フィルム状焼成材料の形成対象面に、フィルム状焼成材料を構成するための各成分及び溶媒を含む焼成材料組成物を塗工し、必要に応じて乾燥させて溶媒を揮発させることで、目的とする部位にフィルム状接着剤を形成できる。
溶媒としては、沸点が250℃未満のものが好ましく、沸点が200℃未満のものがより好ましく、たとえばn-ヘキサン(沸点:68℃)、酢酸エチル(沸点:77℃)、2-ブタノン(沸点:80℃)、n-ヘプタン(沸点:98℃)、メチルシクロヘキサン(沸点:101℃)、トルエン(沸点:111℃)、アセチルアセトン(沸点:138℃)、n-キシレン(沸点:139℃)、ジメチルホルムアミド(沸点:153℃)およびブチルカルビトール(沸点:230℃)などが挙げられる。これらは単独で使用してもよく、また組み合わせて使用してもよい。
実施形態の支持シート付フィルム状焼成材料は、前記フィルム状焼成材料と、前記フィルム状焼成材料の少なくとも一方の側に設けられた支持シートと、を備える。前記支持シートは、基材フィルム上の全面もしくは外周部に粘着剤層が設けられたものであり、前記粘着剤層上に、前記フィルム状焼成材料が設けられていることが好ましい。前記フィルム状焼成材料は、粘着剤層に直接接触して設けられてもよく、基材フィルムに直接接触して設けられてもよい。本形態をとることで、半導体ウエハを素子に個片化する際に使用するダイシングシートとして使用することが出来る。且つブレード等を用いてウエハと一緒に個片化することで素子と同形のフィルム状焼成材料として加工することが出来、且つフィルム状焼成材料付半導体素子を製造することが出来る。
基材フィルム3としては、特に限定されず、例えば低密度ポリエチレン(LDPE)、直鎖低密度ポリエチレン(LLDPE),エチレン・プロピレン共重合体、ポリプロピレン、ポリブテン、ポリブタジエン、ポリメチルペンテン、エチレン・酢酸ビニル共重合体、エチレン・(メタ)アクリル酸共重合体、エチレン・(メタ)アクリル酸メチル共重合体、エチレン・(メタ)アクリル酸エチル共重合体、ポリ塩化ビニル、塩化ビニル・酢酸ビニル共重合体、ポリウレタンフィルム、アイオノマー等からなるフィルムなどが用いられる。なお、本明細書において「(メタ)アクリル」は、アクリルおよびメタクリルの両者を含む意味で用いる。
支持シート2は、少なくともその外周部に粘着部を有する。粘着部は、支持シート付フィルム状焼成材料100a,100bの外周部において、リングフレーム5を一時的に固定する機能を有し、所要の工程後にはリングフレーム5が剥離可能であることが好ましい。したがって、粘着剤層4には、弱粘着性のものを使用してもよいし、エネルギー線照射により粘着力が低下するエネルギー線硬化性のものを使用してもよい。再剥離性粘着剤層は、従来より公知の種々の粘着剤(例えば、ゴム系、アクリル系、シリコーン系、ウレタン系、ビニルエーテル系などの汎用粘着剤、表面凹凸のある粘着剤、エネルギー線硬化型粘着剤、熱膨張成分含有粘着剤等)により形成できる。
支持シート付フィルム状焼成材料は、外周部に粘着部を有する支持シートの内周部にフィルム状焼成材料が剥離可能に仮着されてなる。図4で示した構成例では、支持シート付フィルム状焼成材料100aは、基材フィルム3と粘着剤層4とからなる支持シート2の内周部にフィルム状焼成材料1が剥離可能に積層され、支持シート2の外周部に粘着剤層4が露出している。この構成例では、支持シート2よりも小径のフィルム状焼成材料1が、支持シート2の粘着剤層4上に同心円状に剥離可能に積層されていることが好ましい。
前記支持シート付フィルム状焼成材料は、上述の各層を対応する位置関係となるように順次積層することで製造できる。
例えば、基材フィルム上に粘着剤層又はフィルム状焼成材料を積層する場合には、剥離フィルム上に、これを構成するための成分及び溶媒を含有する粘着剤組成物又は焼成材料組成物を塗工し、必要に応じて乾燥させ溶媒を揮発させてフィルム状とすることで、剥離フィルム上に粘着剤層又はフィルム状焼成材料をあらかじめ形成しておき、この形成済みの粘着剤層又はフィルム状焼成材料の前記剥離フィルムと接触している側とは反対側の露出面を、基材フィルムの表面と貼り合わせればよい。このとき、粘着剤組成物又は焼成材料組成物は、剥離フィルムの剥離処理面に塗工することが好ましい。剥離フィルムは、積層構造の形成後、必要に応じて取り除けばよい。
次に本発明に係る支持シート付フィルム状焼成材料の利用方法について、前記焼成材料を素子(例えば半導体素子)の製造に適用した場合を例にとって説明する。
工程(2):フィルム状焼成材料と、支持シートとを剥離し、フィルム状焼成材料付素子を得る工程、
工程(3):被着体の表面に、フィルム状焼成材料付素子を貼付する工程、
工程(4):フィルム状焼成材料を焼成し、半導体素子と被着体とを接合する工程。
半導体ウエハはシリコンウエハおよびシリコンカーバイドウエハであってもよく、またガリウム・砒素などの化合物半導体ウエハであってもよい。ウエハ表面への回路の形成はエッチング法、リフトオフ法などの従来汎用されている方法を含む様々な方法により行うことができる。次いで、半導体ウエハの回路面の反対面(裏面)を研削する。研削法は特に限定はされず、グラインダーなどを用いた公知の手段で研削してもよい。裏面研削時には、表面の回路を保護するために回路面に、表面保護シートと呼ばれる粘着シートを貼付する。裏面研削は、ウエハの回路面側(すなわち表面保護シート側)をチャックテーブル等により固定し、回路が形成されていない裏面側をグラインダーにより研削する。ウエハの研削後の厚さは特に限定はされないが、通常は20~500μm程度である。その後、必要に応じ、裏面研削時に生じた破砕層を除去する。破砕層の除去は、ケミカルエッチングや、プラズマエッチングなどにより行われる。
次いでフィルム状焼成材料を焼成し、基板やリードフレームおよびヒートシンク等の被着体と素子とを焼結接合する。このとき、フィルム状焼成材料付半導体素子のフィルム状焼成材料の露出面を、基板やリードフレームおよびヒートシンク等の被着体に貼付けておけば、フィルム状焼成材料を介して半導体ウエハ(ワーク)と前記被着体とを焼結接合できる。
焼成材料組成物の製造に用いた成分を以下に示す。ここでは、粒子径100nm以下の金属粒子について「焼結性金属粒子」と表記し、粒子径100nmを超える金属粒子について「非焼結性の金属粒子」と表記している。
・アルコナノ銀ペーストANP-1(有機被覆複合銀ナノペースト、株式会社応用ナノ粒子研究所:アルコール誘導体被覆銀粒子、金属含有量70wt%以上、平均粒径100nm以下の銀粒子60wt%以上)
・アルコナノ銀ペーストANP-4(有機被覆複合銀ナノペースト、株式会社応用ナノ粒子研究所:アルコール誘導体被覆銀粒子、金属含有量80wt%以上、平均粒径100nm以下の銀粒子25wt%以上)
・アクリル重合体1(2-エチルヘキシルメタクリレート重合体、重量平均分子量280,000、L-0818、日本合成化学社製、MEK希釈品、固形分54.5質量%、Tg:-10℃(Foxの理論式を用いた計算値))
・アクリル重合体2(メチルアクリレート/2-ヒドロキエチルアクリレート共重合体、共重合重量比率85/15、重量平均分子量370,000、N-4617、日本合成化学社製、酢酸エチル/トルエン=1/1混合溶媒希釈品、固形分35.7質量%、Tg:4℃(Foxの理論式を用いた計算値))
剥離フィルム(厚さ38μm、SP-PET381031、リンテック社製)の片面に、上記で得られた焼成材料組成物を塗工し、110℃4分間乾燥させることで、表1に示す厚さを有するフィルム状焼成材料を得た。
焼成前のフィルム状焼成材料と、重量で約10倍量の有機溶媒とを混合した後にこれを焼結性金属粒子および非焼結性の金属粒子が沈降するまで、約30分間、静置した。この上澄み液をシリンジで抜き取り、120℃10分で乾燥した後の残留物を回収することで、フィルム状焼成材料から焼結性金属粒子および非焼結性の金属粒子を除いた成分を分取した。また上記シリンジで上澄み液を抜き取った後の焼結性金属粒子および非焼結性の金属粒子が含まれる液に対して、再び、フィルム状焼成材料の約10倍量の有機溶媒を混合した後にこれを焼結性金属粒子及び非焼結性の金属粒子が沈降するまで、約30分間、静置し、上澄み液をシリンジで抜き取った。この有機溶媒の混合と静置および上澄み液の抜き取りを5回繰り返した後、残った液を120℃10分で乾燥した後、残留物を回収することで、焼結性金属粒子および非焼結性の金属粒子を分取した。
上記で得られたフィルム状焼成材料について、下記項目を評価した。
上記で得られたフィルム状焼成材料について、熱分析測定装置(熱分析計TG/DTA同時測定装置 DTG-60、株式会社島津製作所製)を用い、測定試料とほぼ同量のアルミナ粒子を参照試料として大気雰囲気下、昇温速度10℃/分で40℃から600℃まで測定し、TG曲線及びDTA曲線を求めた。実施例1の結果を図7に、実施例2の結果を図8に、比較例1の結果を図9に、比較例2の結果を図10に示す。また、TG曲線における、負の傾きが最も大きい昇温開始後の時間(A1)と、DTA曲線における昇温開始後0秒から2160秒の時間範囲での最大ピーク時間(B1)とを表1に示す。
また、前記分離方法により、フィルム状焼成材料から前記焼結性金属粒子および非焼結性の金属粒子を除いた成分について、TG曲線における、負の傾きが最も大きい昇温開始後の時間(A1’)と、DTA曲線における昇温開始後960秒から2160秒の時間範囲で観測されるピークの内、最短時間で観測されるピーク時間(B1’)とを表1に示す。
上記で得られたフィルム状焼成材料について、熱分析測定装置(熱分析計TG/DTA同時測定装置 DTG-60、株式会社島津製作所製)を用い、測定試料とほぼ同量のアルミナ粒子を参照試料として窒素雰囲気下、昇温速度10℃/分で測定し、TG曲線及びDTA曲線を求めた。実施例1の結果を図11に、実施例2の結果を図12に、比較例1の結果を図13に、比較例2の結果を図14に示す。また、TG曲線における、負の傾きが最も大きい温度(A2)と、DTA曲線における25℃から400℃の温度範囲での最大ピーク温度(B2)とを表1に示す。
フィルム状焼成材料の焼成後のせん断接着力は、以下の方法により測定した。
上記で得られたフィルム状焼成材料を10mm×10mmにカットし、これを直径10mmの断面を持つ高さ5mmの、円柱体形状の銅被着体の上面に貼付し、その上に直径5mmの断面を持つ高さ2mmの、円柱体形状の銅被着体を載せて、大気雰囲気下または窒素雰囲気下で下記(1)~(3)の条件にて加圧焼成し、接合接着力測定用試験片を得た。常温で、この試験片の接着面に対して6mm/分の速度でせん断方向から力を加え、接着状態が破壊するときの強度を測定し、下記加圧焼成条件で得た試験片の測定結果の内、最も高い接合接着強度を示した条件の値の平均値をもって、せん断接着力とした。結果を表1に示す。
(1)300℃3分、30MPa、
(2)350℃3分、10MPa、
(3)400℃3分、10MPa
JIS K7130に準じて、定圧厚さ測定器(テクロック社製、製品名「PG-02」)を用いて測定した。
Claims (9)
- 焼結性金属粒子及びバインダー成分を含有するフィルム状焼成材料であって、
大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい昇温開始後の時間(A1)と、
アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)における、昇温開始後0秒から2160秒の時間範囲での最大ピーク時間(B1)とが、
A1<B1<A1+200秒の関係を満たし、且つ、A1<2000秒である、フィルム状焼成材料。 - フィルム状焼成材料から前記焼結性金属粒子を除いた成分について、大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい昇温開始後の時間(A1’)と、
前記焼結性金属粒子について、アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)における、昇温開始後960秒から2160秒の時間範囲で観測されるピークの内、最短時間で観測されるピーク時間(B1’)とが、
B1’<A1’の関係を満たす、請求項1に記載のフィルム状焼成材料。 - 前記フィルム状焼成材料について、アルミナ粒子を参照試料として大気雰囲気下10℃/分の昇温速度で40℃から600℃まで測定された示差熱分析曲線(DTA曲線)において、昇温開始後0秒から2160秒の時間範囲での吸熱ピークを有さない、請求項1又は2に記載のフィルム状焼成材料。
- 焼結性金属粒子及びバインダー成分を含有するフィルム状焼成材料であって、
窒素雰囲気下10℃/分の昇温速度で測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい温度(A2)と、
アルミナ粒子を参照試料として窒素雰囲気下10℃/分の昇温速度で測定された示差熱分析曲線(DTA曲線)における、25℃から400℃の温度範囲での最大ピーク温度(B2)とが、
A2<B2<A2+60℃の関係を満たす、フィルム状焼成材料。 - フィルム状焼成材料から前記焼結性金属粒子を除いた成分について、窒素雰囲気下10℃/分の昇温速度で測定された熱重量曲線(TG曲線)における、負の傾きが最も大きい温度(A2’)と、
前記焼結性金属粒子について、アルミナ粒子を参照試料として窒素雰囲気下10℃/分の昇温速度で測定された示差熱分析曲線(DTA曲線)における、200℃から400℃の温度範囲で観測されるピークの内、最も低温で観測されるピーク温度(B2’)とが、
B2’<A2’の関係を満たす、請求項4に記載のフィルム状焼成材料。 - 前記フィルム状焼成材料について、アルミナ粒子を参照試料として窒素雰囲気下10℃/分の昇温速度で測定された示差熱分析曲線(DTA曲線)において、25℃から400℃の温度範囲での吸熱ピークを有さない、請求項4又は5に記載のフィルム状焼成材料。
- 前記焼結性金属粒子が銀ナノ粒子である、請求項1~6のいずれか一項に記載のフィルム状焼成材料。
- 請求項1~7のいずれか一項に記載のフィルム状焼成材料と、前記フィルム状焼成材料の少なくとも一方の側に設けられた支持シートと、を備えた支持シート付フィルム状焼成材料。
- 前記支持シートが、基材フィルム上に粘着剤層が設けられたものであり、
前記粘着剤層上に、前記フィルム状焼成材料が設けられている、請求項8に記載の支持シート付フィルム状焼成材料。
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| KR1020197031385A KR102087022B1 (ko) | 2017-04-28 | 2018-03-15 | 필름상 소성재료, 및 지지 시트를 가지는 필름상 소성재료 |
| US16/608,288 US11285536B2 (en) | 2017-04-28 | 2018-03-15 | Film-shaped fired material, and film-shaped fired material with support sheet |
| EP18790028.7A EP3618108B1 (en) | 2017-04-28 | 2018-03-15 | Film-shaped fired material, and film-shaped fired material with support sheet |
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| JP2017192821A JP6555695B2 (ja) | 2017-10-02 | 2017-10-02 | フィルム状焼成材料、及び支持シート付フィルム状焼成材料 |
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| EP3979300A4 (en) * | 2019-05-24 | 2023-11-29 | Lintec Corporation | FILM-LIKE CURNING MATERIAL WITH CARRIER FILM, ROLL BODY, MULTI-LAYER BODY AND METHOD FOR PRODUCING A DEVICE |
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| KR102290466B1 (ko) * | 2017-09-15 | 2021-08-17 | 린텍 가부시키가이샤 | 필름상 소성 재료, 및 지지 시트를 가지는 필름상 소성 재료 |
| KR20210141490A (ko) * | 2019-03-15 | 2021-11-23 | 린텍 가부시키가이샤 | 지지 시트 부착 필름상 소성 재료, 롤체, 적층체, 및 장치의 제조 방법 |
| JP7611164B2 (ja) * | 2019-11-22 | 2025-01-09 | リンテック株式会社 | フィルム状焼成材料、支持シート付フィルム状焼成材料、積層体、及び装置の製造方法 |
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| EP3618108A4 (en) | 2021-01-06 |
| US20200376549A1 (en) | 2020-12-03 |
| EP3618108A1 (en) | 2020-03-04 |
| EP3618108B1 (en) | 2022-07-06 |
| US11285536B2 (en) | 2022-03-29 |
| TW201843744A (zh) | 2018-12-16 |
| TWI753145B (zh) | 2022-01-21 |
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