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NL2034783B1 - Method for manufacturing a rare earth doped optical waveguide, and a rare earth doped optical waveguide - Google Patents

Method for manufacturing a rare earth doped optical waveguide, and a rare earth doped optical waveguide Download PDF

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Publication number
NL2034783B1
NL2034783B1 NL2034783A NL2034783A NL2034783B1 NL 2034783 B1 NL2034783 B1 NL 2034783B1 NL 2034783 A NL2034783 A NL 2034783A NL 2034783 A NL2034783 A NL 2034783A NL 2034783 B1 NL2034783 B1 NL 2034783B1
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Prior art keywords
waveguide core
waveguide
substrate
cladding layer
aluminium oxide
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NL2034783A
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Dutch (nl)
Inventor
Benson Bonneville Dawson
María García Blanco Sonia
Arnoldus Petrus Marinus Hendriks Ward
Eduardo Osornio Martínez Carlos
Wang Kai
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Univ Twente
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Priority to NL2034783A priority Critical patent/NL2034783B1/en
Priority to PCT/NL2024/050181 priority patent/WO2024232752A1/en
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Publication of NL2034783B1 publication Critical patent/NL2034783B1/en

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/05Construction or shape of optical resonators; Accommodation of active medium therein; Shape of active medium
    • H01S3/06Construction or shape of active medium
    • H01S3/063Waveguide lasers, i.e. whereby the dimensions of the waveguide are of the order of the light wavelength
    • H01S3/0632Thin film lasers in which light propagates in the plane of the thin film
    • H01S3/0637Integrated lateral waveguide, e.g. the active waveguide is integrated on a substrate made by Si on insulator technology (Si/SiO2)
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/0021Reactive sputtering or evaporation
    • C23C14/0036Reactive sputtering
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/08Oxides
    • C23C14/081Oxides of aluminium, magnesium or beryllium
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/10Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type
    • G02B6/12Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type of the integrated circuit kind
    • G02B6/13Integrated optical circuits characterised by the manufacturing method
    • G02B6/132Integrated optical circuits characterised by the manufacturing method by deposition of thin films
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/05Construction or shape of optical resonators; Accommodation of active medium therein; Shape of active medium
    • H01S3/06Construction or shape of active medium
    • H01S3/063Waveguide lasers, i.e. whereby the dimensions of the waveguide are of the order of the light wavelength
    • H01S3/0632Thin film lasers in which light propagates in the plane of the thin film
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/14Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range characterised by the material used as the active medium
    • H01S3/16Solid materials
    • H01S3/1601Solid materials characterised by an active (lasing) ion
    • H01S3/1603Solid materials characterised by an active (lasing) ion rare earth
    • H01S3/1608Solid materials characterised by an active (lasing) ion rare earth erbium
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/14Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range characterised by the material used as the active medium
    • H01S3/16Solid materials
    • H01S3/17Solid materials amorphous, e.g. glass

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  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Optics & Photonics (AREA)
  • Electromagnetism (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • General Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Optical Integrated Circuits (AREA)

Abstract

The present application concerns a method for manufacturing an aluminium oxide optical waveguide doped with rare earth ions. The present application further concerns an aluminium oxide optical waveguide doped with rare earth ions that are preferably manufactured by said method. According to the present invention, the method comprises providing a substrate, depositing an aluminium oxide waveguide core layer doped with ions of a rare earth metal onto the substrate, and arranging a cladding layer on the deposited waveguide core, said arranging comprising at least one processing step during which the deposited waveguide core is subjected to a given maximum temperature. The method is characterized in that depositing the waveguide core comprises forming nano-crystallites in the waveguide core. A lowest temperature at which a quenching percentage of the deposited waveguide core significantly increases, exceeds the given maximum temperature, wherein the given maximum temperature is about 400 degrees Celsius or higher.

Description

METHOD FOR MANUFACTURING A RARE EARTH DOPED OPTICAL WAVEGUIDE,
AND A RARE EARTH DOPED OPTICAL WAVEGUIDE
The present application concerns a method for manufacturing an alominium oxide optical waveguide doped with rare earth ions. The present application further concerns an aluminium oxide optical waveguide doped with rare earth ions that are preferably manufactured by said method.
Integrated photonics has become ubiquitous as its development opens opportunities for improved capabilities in applications over well-developed microelectronic technologies.
Especially, as ultra-low loss waveguides are realized, a myriad of applications for photonics integrated circuits can be explored, among others, quantum computing, microwave photonics, biosensing, and non-linear sources. Rare earth doped media in particular is emerging as a competitive light source platform for a wide variety of applications, ranging from telecommunications, light detection and ranging, LIDAR, and environmental and biological sensing.
Known from the art is that an optical waveguide may be manufactured by providing a substrate, depositing an aluminium oxide waveguide core doped with ions of a rare earth metal on the substrate, and arranging a cladding layer on the deposited aluminium oxide waveguide core.
Here, it is noted that arranging the cladding layer comprises at least one processing step during which the deposited aluminium oxide waveguide core is subjected to a given maximum temperature. Such optical waveguides may, for example, be used as parts of optical amplifiers.
An optical signal comprises anywhere between one, a few, or a continuous stream of signal photons of a particular wavelength. Optical amplifiers can amplify such a signal by providing an environment in which these signal photons can cause stimulated emission, stimulated emission being the process in which a signal photon interacts with an excited ion causing said ion to emit an identical photon and to return to a relaxed state. Specifically, such an environment may be provided by doping a medium such as a fibre or a waveguide with rare earth ions, i.e. ions of rare earth metals, and introducing pump energy into the medium to excite the rare earth ions. This pump energy can be provided with a pump laser, but alternatives are also known.
The skilled person is aware that the desired process of stimulated emission has less than desirable counterparts in energy migration and energy transfer up conversion. In energy migration, a signal photon, being either an original photon or a photon resulting from stimulated emission, is absorbed by a ‘relaxed!’ rare earth ion, thereby exciting it. In energy transfer up conversion, a signal photon, being either an original photon or a photon resulting from stimulated emission, is absorbed by an already excited rare earth ion, exciting it even further. These processes are together sometimes referred to as quenching. How much quenching occurs can be expressed using any one of a number of characteristics, including the quenching percentage, the quenching factor, or the quenching rate.
In the present application, reference will be made to the quenching percentage.
Known from the art are optical waveguides with rare earth doped waveguide cores. Of the materials investigated for integrated photonics, aluminium oxide, A1203, has emerged as a promising platform material due to its large transparency window, low propagation losses, and high rare-earth solubility. Specifically, known in the art are optical waveguides that comprise a waveguide core made of amorphous aluminium oxide. These tend to show high optical performance and/or low losses in themselves. However, if, after deposition, the doped waveguide core is exposed to high temperatures, the quenching percentage significantly increases, making them less than ideal candidates for use in optical amplifiers.
The skilled person will be aware that optical losses in an optical waveguide are determined, not just by losses in the waveguide core, but also by losses in the cladding layer.
Optical losses in cladding layers may vary between different materials. For example, tetraethyl orthosilicate, TEOS, is known to display relatively low optical losses. However, for the manufacturing of a TEOS cladding layer, a high temperature annealing step is typically required.
When combining the TEOS cladding layer with an amorphous alominium oxide waveguide core doped with ions of a rare earth metal, a problem therefore arises in that the benefit of the optical quality of the TEOS cladding layer is mitigated by the significant increase of the quenching percentage of the amorphous aluminium oxide waveguide core due to the high temperatures involved when using a TEOS cladding layer on the amorphous aluminium oxide waveguide core.
There may also be other types of cladding layers that, to be arranged on the deposited aluminium oxide waveguide core, require processing steps during which said aluminium oxide waveguide core is subjected to high temperatures, resulting in the aforementioned increase in quenching percentage of the aluminium oxide waveguide cores. Hereinafter, cladding layers that require a high-temperature step performed at 400 degrees Celsius or higher during or after deposition are referred to as high-temperature cladding layers.
Accordingly, a problem exists when combining a known aluminium oxide waveguide core doped with ions of a rare earth metal with a high-temperature cladding layer. This problem prevents further reductions in optical losses for aluminium oxide waveguide cores. Consequently, high-temperature cladding layers cannot be combined with known amorphous aluminium oxide waveguide cores doped with ions of a rare earth metal, even though both components by themselves show high optical performance and/or low losses, and thus seem to be advantageous to use in combination.
This problem, for example, occurs in the paper “Characteristics of Er-doped A1203 thin films deposited by reactive co-sputtering” by MUSA, S., et al, IEEE journal of quantum electronics, 2000, 36.9: 1089-1097. This paper discusses Er-doped A1203 thin films that have been deposited by reactive co-sputtering onto thermally oxidized Si-waters. The thin films are deposited at a substrate temperature of 400 °C to ensure that they are amorphous and the waveguides have not been annealed. A relatively broad luminescence band, having an FWHM of 55 nm around the 1533 nm wavelength, has been measured. From gain versus pumping power curves, an up- conversion coefficient lower than 20x 10% m?/s has been derived.
The authors indicate that high temperature annealing results in clustering in ion implanted materials, leading to higher energy migration in the centre of the waveguide core. Consequently, the authors limit themselves to low-temperature reactive co-sputtering to produce Er: A203 thin- films to avoid clustering of Er-ions.
Also known in the art are optical waveguides comprising a waveguide core that is manufactored as a single crystal. These show lower quenching percentages but are significantly more expensive and difficult to manufacture, meaning they are not easily commercialised.
An object of the present invention is to provide a method for manufacturing an optical waveguide comprising an aluminium oxide waveguide core and cladding layer in which at least one of the abovementioned problems is at least partially solved.
According to the present invention, this object is achieved with a method as defined in claim
I, which is characterized in that depositing the aluminium oxide waveguide core comprises forming nano-crystallites in the aluminium oxide waveguide core, wherein a lowest temperature at which a quenching percentage of the deposited waveguide core significantly increases exceeds the given maximum temperature, and wherein the given maximum temperature is about 400 degrees
Celsius or higher.
The applicant has found that by deliberately allowing nano-crystallites to form during deposition, an aluminium oxide waveguide core can be manufactured that displays a lower quenching percentage than one made of amorphous material, while also being able to maintain said quenching percentage up to higher temperatures during subsequent processing steps.
When depositing at relatively low temperatures, no significant crystallization occurs, an amorphous layer doped with rare earth ions will be achieved, and some amount of ion clusters is formed. However, when such an amorphous aluminium oxide layer is subsequently subjected to a high temperature, e.g. 400 degrees Celsius and up, significantly more clustering will occur. In the amorphous material, rare earth ions can migrate towards each other, significantly increasing the quenching percentage.
When depositing at relatively high temperatures, crystallization will occur to such an extent that almost the entire deposited layer is filled with nano-crystallites.
Without being bound by theory, the Applicant notes that the energy required for rare earth ions in the abovementioned aluminium oxide layer with a large amount of relatively small crystallites to migrate and cluster is too high to be reached during the processing steps required to arrange a cladding layer.
That such a waveguide core is achieved can be confirmed by subjecting it to the given maximum temperature. No significant increase in the quenching percentage will occur, as very little clustering will occur inside the layer.
By deliberately allowing nano-crystallites to form, no to little amorphous material is present.
This means the rare earth ions are far less mobile and are therefore less likely to cluster. The applicant has thereby overcome the technical prejudice that aluminium oxide waveguide cores doped with rare earth ions have to be made of amorphous aluminium oxide and/or that such a core cannot be annealed.
The Applicant found that by forming the nano-crystallites such that the given maximum temperature lies in a range between about 400 and about 1400 degrees Celsius, advantageous quenching percentage of the optical waveguide can be obtained. A maximum temperature that is lower than 400 degrees Celsius would indicate that a relatively large amount of amorphous aluminium oxide would be available after deposition of the waveguide core, resulting in a relatively high mobility for the rare earth ions when arranging the cladding layer. On the other hand, a maximum temperature that is higher than 1400 degrees Celsius would risk deterioration of the aluminium oxide waveguide core. The skilled person will appreciate that around 1400 degrees
Celsius the glass transition temperature of aluminium oxide starts, so subjecting the aluminium oxide waveguide core to this temperature may cause reflow of the structure.
It is noted that the given maximum temperature preferably lies in a range between about 400 and about 1400, preferably between about 500 and about 800 degrees Celsius and is more preferably about 550 degrees Celsius.
In the context of the present application, an increase in quenching percentage may be considered significant when about 20% points or more, preferably when between about 5% to about 20%.
Depending on the particular cladding layer that is used, arranging the cladding layer may comprise depositing the cladding layer on the deposited waveguide core. The at east one processing step during which the given maximum temperature is achieved comprises annealing the combination of the substrate, deposited waveguide core, and deposited cladding layer at said given maximum temperature. In such embodiments, the quenching percentage of the aluminium oxide waveguide core after said deposition of the cladding layer and before said annealing may be between about 5% and about 35%. Additionally or alternatively, the quenching percentage of the waveguide core after said annealing is between about 0% and about 35%, preferably between about 0% and about 5%.
For some cladding layers, the at least one processing step comprises depositing the cladding layer on the aluminium oxide waveguide core at said given maximum temperature. In such embodiments, the quenching percentage of the aluminium oxide waveguide core after said deposition of the cladding layer may be between about 0% and about 35%, preferably between 5 about 0% and about 5%.
Various materials may be used as specific implementations for the rare earth ions. The rare carth metal may be a lanthanide, such as Erbium (Er3+), Ytterbiam (Yb3+), Thuliom (Tm3+) and/or Neodymium (Nd3+).
In a preferred embodiment, the aluminium oxide is stoichiometric. The skilled person will appreciate that this depends on the practical implementation and that this cannot always be achieved. Hence, for some embodiments, it can be said that the waveguide core comprises AlxOy, wherein 1.5 <x <2.5and 2.5 <y< 3.5, suchas x= 1.6, andy = 3.4, and preferably x = 2, andy = 3.
The skilled person will appreciate that the waveguide core can be grown using various methods, such as any one of reactive sputter deposition, atomic layer deposition, evaporation, or pulsed laser deposition.
Various types of cladding layers may also be used, such as a TEOS layer, a Silicon oxynitride layer, or a polymer layer. Depending on the desired cladding layer, one of a number of application methods may be used. That is, the cladding layer may be arranged using any one of plasma enhanced vapor deposition, low pressure chemical vapor deposition, evaporation, sputtering, or atomic layer deposition.
Various types of substrates may also be used, such as a silicon substrate, a silicon thermal oxide substrate, or a quartz substrate.
The optical waveguide can also take on any one of a number of forms, such as a slab waveguide or a channel waveguide.
In some embodiments, losses in the manufactured waveguide may be reduced further by including in the manufacturing method, between depositing the aluminium oxide waveguide core and arranging the cladding layer, the steps of reducing surface roughness of the aluminium oxide waveguide core, for example using chemical mechanical polishing.
In some embodiments, the method further comprises defining a shape and/or size of the aluminium oxide waveguide core using, for example, at least one of lithography and etching, before arranging the cladding layer.
The skilled person will appreciate that the exact settings necessary to manufacture an optical waveguide will always also depend on the particular machine used, the batch of resources / material used, etc. To figure out the exact settings ideal for providing an optical waveguide according the invention, in some embodiments the method further comprises:
- at a deposition rate for aluminium oxide, depositing aluminium oxide layers doped with rare earth ions at varying substrate temperatures and/or at varying substrate bias voltages on respective substrates; - for each deposited aluminium oxide layer, measuring its quenching percentage; - selecting, as optimal settings, said deposition rate and the substrate temperature and substrate bias voltage with which the aluminium oxide layer was manufactured that had the lowest quenching percentage; and - using the optimal settings when depositing the aluminium oxide waveguide core for manufacturing an optical waveguide according to any of the preceding claims.
According to a further aspect of the application, an optical waveguide core is provided that comprises a substrate, an aluminium oxide waveguide core and a cladding layer. The aluminium oxide waveguide core is doped with ions of a rare earth metal and is arranged on the substrate. The cladding layer is arranged on the waveguide core. The aluminium oxide waveguide core comprises nano-crystallites and has a quenching percentage of the optical waveguide is 5% or less. The cladding layer comprises a high-temperature cladding layer.
The morphology of the waveguide core as a whole can be considered nano-crystalline or polycrystalline depending on the size of the crystallites and how much of the waveguide core is in this form. In a particular embodiment, the nano-crystallites may be between about 1 nanometre and about 30 nanometre in size, preferably between about 1 nanometre and about 10 nanometre in size.
In a particular embodiment, the nano-crystallites form at least 50% by weight of the aluminium oxide waveguide core, preferably at least 75%, and more preferably at least 99%.
Various cladding layers can be used. For example, the high-temperature cladding layer may comprises at least one a TEOS layer or a Silicon oxynitride layer.
The optical waveguide can take on any one of a number of forms, including a slab waveguide or a channel waveguide.
An optical waveguide as discussed in the above is preferably manufactured by one of the earlier mentioned method.
Next, the present invention will be described by referring to the appended drawings, wherein identical reference signs will be used to refer to the same or similar components, and wherein:
Figure 1 shows a flowchart of a method for manufacturing an optical waveguide in accordance with the present invention;
Figure 2 shows a cross-section of a slab waveguide in accordance with the present invention;
Figure 3 shows a flowchart of a preferred embodiment of the method of figure 1;
Figure 4 shows an example of a reactive co-sputtering system that may be configured to deposit an aluminium oxide waveguide core in accordance with the present invention;
Figure 5 illustrates TEM pictures of deposited aluminium oxide waveguide cores for various substrate temperatures;
Figures 6a and 6b illustrate AFM pictures of a deposited aluminium oxide waveguide cores for various substrate temperatures;
Figure 7 shows a graph relating, on the X-axis, deposition temperatures for aluminium oxide waveguide cores, and, on the Y-axis, measured refractive index thereof, and a graph relating, for a number of deposition temperatures, on the X-axis, a wavelength of light propagated through aluminium oxide waveguide cores deposited at said temperatures, and, on the Y-axis, measured propagation losses therein.
Figure 8a shows a graph relating, on the X-axis, the temperature at which a waveguide core is deposited, to, on the Y-axis, the size of crystallites formed in said aluminium oxide waveguide core;
Figure 8b shows a graph relating, on the X-axis, the temperature at which a waveguide core is deposited, to, on the Y-axis, the percentage by weight of the waveguide core that isin a particular phase, specifically amorphous (A) or crystalline (C);
Figure 8c shows a graph relating, on the X-axis, the temperature at which a waveguide core is deposited, to, on the Y-axis, optical losses achieved in said waveguide core;
Figures 9a and 9b both show graphs relating, on the X-axis, the distance over which light propagated through a waveguide core, to, on the Y-axis, intensity of said light.
Figure 10 shows a testing set up for measuring the gain in an optical waveguide.
In the context of this application, the metric used to describe the amount of quenching that occurs in an optical waveguide — or, more specifically, would occur if said waveguide would be used for optical amplification and/or would be included in an optical amplifier — is the quenching percentage. The skilled person will be aware that this can be derived in a number of ways.
Regardless, according to one definition adhered to within the context of the present invention, the quenching percentage may refer to the percentage of rare earth ions that is not accessible by the signal photons. This may be because the decay-rate constant is too fast.
This percentage may be derived by causing steady state excitation in the doped waveguide core, i.e. providing pump energy to the waveguide core until it is saturated, and, after having stopped providing said pump energy, measure the non-radioactive decay. Depending on an assumed distribution of excited states, an assumption that the skilled person is aware of and that depends on the rare earth ion in question, and the measured total non-radioactive decay, it is possible to derive what percentage or fraction of the rare earth ions is quenched and which is not.
Figure 1 shows a flowchart including steps S1-S3 of one embodiment of a method for manufacturing an optical waveguide according to the present invention. Figure 2 shows a schematic cross-section of an optical waveguide, as, for example, can be manufactured with the method according to the invention. Figure 3 shows a flowchart of a preferred embodiment of said method.
In a step S1, a substrate 10 is provided. In a next step S2, an aluminium oxide waveguide core doped 11 with ions of a rare earth metal is deposited on the substrate. Specifically, aluminium oxide core 11 is deposited such that nano-crystallites are formed therein. In a next step S3, a cladding layer 12 is arranged on aluminium oxide waveguide core 11. During at least one processing step required to arrange cladding layer 12, aluminium oxide waveguide core 11 is subjected to a given maximum temperature, which is about 400 degrees Celsius or higher, and preferably between about 400 degrees and about 1400 degrees Celsius. The lowest temperature at which a quenching percentage of the deposited waveguide core significantly increases, exceeds the given maximum temperature.
Increasing the maximum temperature beyond about 1400 degrees Celsius risks deterioration of aluminium oxide waveguide core 11. The skilled person will appreciate that around 1400 degrees Celsius the glass transition temperature of aluminium oxide starts, so subjecting the waveguide core to this temperature may cause reflow of the structure. Moreover, such a maximum temperature may also deteriorate the performance of the other components of the waveguide, depending on the materials used. Substrate 10 may be made of silicon, which may start to melt around 1400 degrees Celsius. Substrate 10 may also comprise silicon dioxide, in which, when exposed to such temperatures, local density fluctuations may form that cause scattering and thus degrade performance.
In a particular embodiment, the substrate is made of thermal Si0O2 and is about 6.0 um thick, the waveguide core is made of Al203:Er3+ and is about 1.6 um wide and 0.78 um thick, and the cladding layer is made of CVD SiO2 and is about 8.0 um thick.
The applicant finds that, apart from the abovementioned aluminium oxide, other host materials that allow for formation of nano-crystallites and which have sufficiently high rare earth solubility can be used. One such alternative host material is aluminium nitride. The skilled person will be aware of how the following specification of a manufacturing process for an aluminium oxide waveguide core, can and/or should be adapted for manufacturing other host materials, such as an aluminium nitride waveguide core.
Other rare earth metals may also be used. The ions may for example be lanthanides. Some specific examples are Erbium (Er**), Yiterbium (Yb**), Thulium (Tm?) and/or Neodymium (Nd?*). The skilled person will be aware of how the following specification of a manufacturing process for an Erbium, can and/or should be adapted for manufacturing a waveguide core doped with other rare earth ions.
The concentration of rare earth ions may be anywhere between about 0.25% 10% ions/cm? and about 1x10*! ions/cm”, preferably between about 0.25x10%" ions/cm? and about 4x10% ions/cm®.
The method according to the invention ensures that clusters do not form or that at least very few clusters form. A corresponding positive formulation thereto is that the method according to the invention provides a waveguide core throughout which the rare earth metal ions are evenly and/or uniformly distributed. The skilled person will appreciate that the positioning of the rare earth ions is, however, never exactly even or uniform. However, that is also not necessary. In the context of this application, evenly distributed or uniformly distributed should be understood as that, when the distribution of the ions throughout the waveguide core is described as a stochastic process, said process would show an approximately uniform distribution.
Now referring to figure 3, step S3 of arranging the cladding layer may comprise a step S31 of depositing a cladding layer 12 on aluminium oxide waveguide core 11. Step 31 may be the processing step during which aluminium oxide waveguide core 11 is subjected to the given maximum temperature. This may for example apply in embodiments where a polymer-based cladding layer is deposited.
Alternatively, a high-temperature step is not part of the deposition of the cladding layer but part of a subsequent heating step. In figure 3, an example of such subsequent step is provided as step S32 in which the combination of substrate 10, deposited aluminium oxide waveguide core 11, and arranged cladding 12 layer is annealed thereby subjecting aluminium oxide waveguide core 11 to the given maximum temperature. This applies for example in embodiments where a TEOS cladding layer is deposited.
It should be noted that various other steps can be performed in between the deposition of aluminium oxide waveguide core 11 and the arrangement of cladding layer 12. For example, the deposited aluminium oxide layer can be subjected to chemical mechanical polishing to reduce surface roughness and to e-beam lithography and reactive etching steps to define a channel waveguide or other type of waveguide.
A first possible implementation for depositing the aluminium oxide waveguide core 11 such that nano-crystallites are formed is discussed below, referring to figures 4 to 7. A conceptual explanation of the nano-crystallites formed is given in relation to figures 8a-c.
The A10::Er** thin films used in embodiments of the present invention can be deposited by reactive sputtering onto a silicon wafer having an 8 micrometres oxide buffer layer. The advantage of reactive sputtering exploited here is a result of the energy available per adatom on the substrate.
The adatoms landing on the substrate have a high mobility, resulting in high-density layer morphologies available at relatively low substrate temperatures and high deposition rates. This allows for the deposition of high-density ALOs:Er'* layers at CMOS compatible wafer temperatures, with slab waveguide propagation losses below 0.1 dB/cm at 1550 nm.
While several methods for achieving Al:03:Er"" optical waveguides with low quenching have been discussed, no link with the morphology of the aluminium oxide has been demonstrated inthe prior art. The applicant realized that, given the complexity of reproducing reactive sputter deposition processes, an understanding of the morphology of the aluminium oxide can facilitate improved reproducibility and layer quality.
The morphology of an AlO3:Er?* layer deposited by reactive sputtering is primarily determined by the available energy per adatom, EPA, and the material properties of the deposited layer. The material properties determining the morphology are the activation energy and diffusion constants that determine the diffusion length of the adatom at a given kinetic energy available per adatom, and the critical nucleation dimension that determines a critical diffusion length required for stable nucleation. While the material properties are a given for an AlLO3:Er™ layer, the energy per adatom is a ratio of the deposition rate and the total energy contributions during deposition.
For reactive sputtering, the total energy flux is a linear combination of different contributions. The sputtering process contributions to the energy flux towards the substrate can be classified in at least four groups.
The contributions of the atoms and molecules adhering to the substrate required for Al,Os layer formation should be considered first. Adatoms that have been accelerated from the target have contributed their kinetic energy as they were adsorbed on the substrate. In addition, when an oxygen molecule is adsorbed, its kinetic energy is also contributed. Even when atoms or molecules are not adsorbed, part of their kinetic energies can still be transferred when colliding with the substrate. Especially when the gas molecules get energized by collisions with higher velocity ions, this contribution can become significant. Another form of kinetic energy is related to the temperature of the substrate. Furthermore, besides the kinetic energy contributions to the layer formation, the potential energy released by the exothermic chemical reaction forming Al:O3:Er> is a significant contribution.
The three other groups of energy contributions are radiation from the plasma, electrons incident on the substrate, and ions accelerated towards the substrate. Note, that a substrate bias can be applied. Increasing and/or decreasing said bias can be done to increase or decrease the electron and ion bombardment on the substrate.
All the energy contributions add to the available energy per adatom and thus influence the layer morphology and consequent propagation losses.
In an embodiment, the A1-03:Er?* layer can be deposited using an AJA ATC 1500 RF reactive co-sputtering system 100 on 10 centimetre silicon wafers having an 8 micrometre thick thermal oxide buffer layer.
System 100, which is schematically illustrated in figure 4, comprises a target 101 comprising aluminium with a 99.9995 % purity, which is arranged above cathode 102. System 100 further comprises a second target 101B (not shown) comprising the rare earth metal, e.g. erbium at 99.95% purity or ytterbium at 99.9%. The second target can be arranged on the same, or a separate cathode adjacent to cathode 102. Opposite to targets 101 and 101B, substrate 190 is arranged on anode 103, which is electrically connected to chamber 103A. RF power is applied between anode 103 and cathode 102. Two targets 101 and 101B can be powered with their own RF power source, thus having individual bias voltages. This causes the generation of a plasma 104 in which supplied
Ar atoms 105 are ionized into Ar ions 106 and electrons 107. Ar ions 106 are accelerated towards target 101 under the influence of a self-generated DC bias. At target 101, they will collide with Al atoms thereby generating a stream of Al atoms 108 towards substrate 10. At substrate 10, Al atoms 108 that have deposited onto substrate 10 will react with oxygen molecules 109 to form aluminium oxide. At target 101B, the Ar ions 106 collide with Er atoms thereby generating a stream of Er atoms, specifically Er?’ ions, towards substrate 10.
The main deposition chamber is evacuated through inlet 110 to a base pressure of 0.1 micro Torr to prevent incorporation of hydroxide ions in the Al0::Er* layer, which induce absorption losses around 750 nm, 970 nm, and 1400 nm.
For the magnetron discharge to be sustained, an equilibrium between the secondary electrons emission from target 101 under ion bombardment and the rate of electrons 107 escaping plasma 104 needs to be maintained. While an RF power source does not directly apply a DC potential difference between cathode 102 and anode 103, electrons 107 in plasma 104 absorb the RF energy much more efficiently than heavier argon ions 106. The high electron mobility causes electrons 107 to be collected on the electrodes. A self-generated DC bias voltage is then a consequence of the asymmetry between target 101 and chamber 103A of sputtering system 100.
A magnetic field is applied using permanent magnets below the targets to increase the electron density in plasma 104, thereby increasing the argon ionization rate and reducing the discharge voltage required. In addition, the magnetic field greatly increases the sputter yield by the increase of ionization and therefore bombardment rate of the target.
Sputtering system 100 further comprises heating means, such as infrared heaters 111, for heating substrate 10 either directly or via anode 103 on which substrate 10 is arranged.
Exemplary process conditions for depositing the aluminium oxide waveguide core are listed in the table below.
Substrate set temperature 420 460 500 540 580 620 660 | °C et
Target-substrate distance
Given the dependence of the layer morphology on available energy per adatom, it is possible to vary the substrate temperature for the purpose of varying the available energy per adatom as it is mostly independent of the other parameters in the process. This allows the investigation of layer morphology as it changes with substrate temperature and the corresponding optical propagation losses in the layers.
The substrate temperatures are set temperatures measured on the substrate holder and are therefore not the exact temperature of the substrate. A calibration of substrate temperature as a function of the set temperature can be provided.
Figure 5 illustrates TEM pictures of a deposited aluminium oxide waveguide layer for various substrate temperatures. The morphology of the layer at the lowest chosen temperature of 420 degrees Celsius is amorphous. As the substrate temperature is increased to 460 degrees Celsius nano-crystallites start to form, of which the density is significantly increased for 500 degrees
Celsius and 540 degrees Celsius.
As the temperature is increased from 500 to 580 degrees Celsius, the surface roughness increases with ever larger waviness. While the waviness of the surface is still present for the layer deposited at 580 degrees Celsius, a clear transition from a mostly amorphous layer with nano- crystallites to a mostly polycrystalline morphology has occurred. The waviness disappears from a temperature of 620 degrees Celsius as an increasingly polycrystalline morphology is observed with a slight columnar growth profile. As the temperature is further increased to 700 degrees Celsius, no significant difference in the morphology is observed.
Figures 6a and 6b illustrate AFM measurements of a deposited aluminium oxide waveguide layer for various substrate temperatures. The AFM measurements show the waviness appearing at 500 degrees Celsius (figure 6a, bottom left) , increasing in amplitude at 540 degrees Celsius (figure 6a, bottom right), and reducing and disappearing at 620 degrees Celsius (figure 6b, top right). In addition to the waviness, the layers grown at a temperature from 500 degrees Celsius (figure 6a,
bottom left) to 580 degrees Celsius (figure 6b top left) exhibit a decreased refractive index and thickness uniformity.
Figure 7, bottom, specifically shows the refractive index of aluminium oxide layers measured by ellipsometry at 1550 nm, for varying deposition temperatures.
The optical propagation losses for each aluminium oxide layer have been investigated using a Metricon 2010/M41, with a fibre loss module. These losses are illustrated in figure, top. Clearly, losses decrease with increasing deposition temperature down to 1.57 dB/cm at 377 nm and 0.84 dB/cm at 403 nm for the layer grown at 700 degrees Celsius substrate temperature.
In alternative embodiments, when depositing an aluminium nitride waveguide core, the exact deposition temperatures may be different from those mentioned in relation to figures 5 and 6, however the Applicant does find that the same behaviour occurs. The same changes in morphology, and/or the same trends in refractive index and thickness uniformity can be observed in aluminium nitride waveguide cores, when deposited at varying temperatures. The teachings derived from figures 4-7, while explaining based on the aluminium oxide waveguide core embodiment, can also be applied to the aluminium nitride waveguide core embodiment.
Figures 8a-c each show a graph that relates the deposition temperature at which an aluminium oxide waveguide core 11 is deposited, to various properties of said core 11. On the X- axis of each of these graphs the deposition temperature is shown. The skilled person will appreciate that the exact temperature values at which a particular waveguide core is deposited is strongly machine dependent, e.g. the machine given value for the ‘deposition temperature’ can deviate from an actual, practically very hard to know, temperature of the waveguide core. However, given a particular machine and a deposition rate that can be achieved, a temperature sweep can be performed to determine exact temperature values at which the behaviour as elucidated in the graphs shown in figures 8a-c occurs.
In the art, there is a clear preference for manufacturing amorphous Al203 waveguide cores to be doped with rare earth ions as these cores have displayed low optical losses. In figures 8a-8c, the deposition temperature at which such waveguides are achieved is referred to as temperature P1.
If, starting from PI, the deposition temperature is decreased, the deposited layer will become less dense and voids will be present in the amorphous aluminium oxide. Said voids may act as scattering objects and may cause losses. If, starting from P1, the deposition temperature is increased, nano-crystallites form in the amorphous material. Said nano-crystallites may act as scattering objects and may cause losses.
As shown in figures 8a-8c, PI is a local minimum at which a balance is struck between reducing the amount voids and preventing the formation of nano-crystallites. At P1, relatively low losses can be achieved. Known aluminium oxide optical waveguides are based on aluminium oxide layers deposited at temperatures corresponding to P1. However, such layers have the aforementioned disadvantage of being vulnerable to high temperature processing steps that follow the deposition of the aluminium oxide layer.
The Applicant realised that in aluminium oxide optical waveguides deposited at deposition temperatures in a range around Pl, the largest losses are caused by local differences in dielectric properties. Both voids and crystallites have different dielectric properties than amorphous aluminium oxide. More voids and/or more crystallites means such local differences occur more often and optical losses will increase.
The Applicant further realised that such local differences will most often occur, and therefore that the losses caused thereby may be at their highest, when the aluminium oxide layer comprises comparable amounts of amorphous material and nano crystallites. This may for example be seen in figure 8b, in which line A describes how much aluminium oxide in the layer, expressed in weight percentage, is in the amorphous phase, and line C describes how much aluminium oxide, expressed in weight percentage, is in the crystalline phase. The skilled person will appreciate that the amount of amorphous material and/or the number of nano-crystallites may also be expressed using other units and/or metrics.
The Applicant further realised that when the deposition temperature is increased, the nano- crystallites will at some temperature overtake the amorphous material as the dominant material in the deposited layer. As the number of discontinuities between amorphous and crystalline aluminium oxide decreases due to the decreasing amount of amorphous aluminium oxide, a reduction in optical losses can be observed beyond a temperature P2. In figure 8b, temperature P2 is chosen as the temperature at which the content of amorphous and crystalline aluminium oxide content is identical for illustrative purposes only.
The reduction in optical losses continues up to the deposition temperature at which substantially all aluminium oxide in the waveguide core takes the form of nano-crystallites and little to none of it is in the amorphous phase. This point may be referred to as P3. Figure 8c further indicates a rectangle R that illustrates the temperature range corresponding to the temperature variation in figure 7, top.
Equivocally, for deposition temperatures between P2 and P3, it is the sporadic presence of volumes of amorphous material in between the otherwise nano-crystalline aluminium oxide that can be considered the cause of scattering. Hence, when further increasing the deposition temperature, less and/or smaller volumes of amorphous material are formed, local differences occur less often, and losses decrease.
The Applicant furthermore realised that, while in the range P1 and P3, more and more aluminium oxide takes on the shape of nano-crystallites, that a size of the individual nano- crystallites does not increase significantly. This is conceptually reflected in figure 8a. Only when deposition temperatures above P3 are used, there may be a significant increase in the size of the individual crystallites while the percentage of aluminium oxide included in crystallites in itself stays the same. It should be noted that no size is indicated for deposition temperatures below Pl as almost no nano-crystallites are present. Increasing the temperature beyond P3 will cause nano- crystallites to combine into large crystallites. These relatively large crystallites cause an increase in optical scattering, thereby increases the optical losses in the layer. As such, at temperature P3 a local minimum can be observed in the losses that is comparable to the minimum at temperature P1.
However, unlike deposited aluminium oxide layers deposited at temperature PI, aluminium oxide layers deposited at temperature P3 are much less susceptible to subsequent heating steps, such as an annealing step for processing a deposited cladding layer.
The morphology achieved at deposition temperatures P3 may also be described as polycrystalline aluminium oxide, saturated with nano-crystallites. Here, nano-crystallites refer to crystallites with a size that is relatively small compared to the waveguide of the light that is to travel through the optical waveguide. This morphology is advantageous because: a) nano-crystallites are so small that they do not cause significant Rayleigh scattering due to their size; b) saturation of the core with nano-crystallites ensures little to no fluctuations in dielectric properties throughout the core thereby also limiting Rayleigh scattering; ¢) saturation of the core with nano-crystallites also means that existing nano-crystallites have little to no amorphous material in their surroundings to absorb and grow with; d) growth occurring due to nano-crystallites mutually aligning and forming a single larger crystallite only occurs at much higher temperatures.
Graphs in figures 8a-c conceptually show when depositing an aluminium oxide layer at various substrate temperatures. While points P1, P2, and P3 are indicated in each graph, the behaviour related therein does not have to occur exactly at the same temperatures for each property described in figures 8a-c. Also, while figure 8c suggests the local minima at Pl and P3 allow for achieving the same low losses, implementations of the method according to the invention may, for a plethora of reasons, result in local minima P1 and P3 achieving different levels of losses.
The Applicant finds that subjecting aluminium oxide waveguide core 11, in which nano- crystallites are formed, to temperatures of 550 or higher such as 800 degrees or higher may even be advantageous and/or decrease losses. The latter is for example shown in figures 9a and 9b.
When aluminium oxide waveguide core 11 is exposed to such a temperature, while the growth of the nano-crystallites is very limited, said growth will still consume all or at least most of the amorphous aluminium oxide that may have formed during deposition of aluminium oxide waveguide core 11. After being subjected to said temperature, if less amorphous aluminium oxide is present, local differences in dielectric properties occur less often and thus scattering decreases.
The skilled person will appreciate that it can be confirmed that an aluminium oxide waveguide core with nano-crystallites is achieved by depositing said core without the rare earth ions and by subjecting it to a temperature of about 800 degrees or higher, preferably between about 800 and about 1400 degrees. No significant changes in the optical performance will occur, as very little crystal growth will occur inside the undoped layer. The mentioned increase in size of said crystallites may be considered significant when about 100% or more, preferably when between about 100% and about 50%. This has to be tested without the rare earth ions as these already cause degradation of the optical performance due to clustering in amorphous materials at temperatures lower than 800, such as 400 degrees.
For figure 9a, the aluminium oxide waveguide core in question is one deposited such that nano-crystallites are formed in the aluminium oxide. No further processing step was performed during which the deposited aluminium oxide waveguide core was subjected to a temperature of 800 degrees Celsius or more. The losses achieved are 1 +/- 0.5 dB/cm.
For figure 9b, the aluminium oxide waveguide core of figure 9a was subjected to about 1150 degrees Celsius for about four hours, in a nitrogen environment. The losses achieved are 0.7 +/-0.2 dB/cm.
The intensity of light, as given on the Y-axis, is an estimate derived from scattering light measured over the propagation length of the waveguide core. Not willing to be bound by theory, the skilled person will appreciate that due to limitations of this estimate it may seem that the intensity of the light increases, while it is still safe to say that losses do occur. These losses are estimated by fitting the measurement data to a log-linear model using a maximum likelihood estimator sample consensus, MLESAC, algorithm. The given error margins are determined by fitting different sections of the total propagation. The skilled person will appreciate that other approaches to estimate the intensity of light inside the waveguide core, and derive average losses from that measurement data may also be used.
In alternative embodiments, when depositing an aluminium nitride waveguide core, the temperature values for Pi, P2, or P3 may be different from those found for aluminium oxide waveguide cores, however the Applicant does find that the same behaviour occurs. Similar changes in the phase that the aluminium nitride has, e.g. amorph or (nano-)crystalline, similar increase in size of the (nano-)crystallites, and a conceptually comparable loss profile can be identified in aluminium nitride waveguide cores, when deposited at varying temperatures. The teachings explained in figures 8a-c, and 9a-b, while explain based on the aluminium oxide waveguide core embodiment, can also be applied to the aluminium nitride embodiment.
A second possible implementation for depositing the aluminium oxide waveguide core 11 such that nano-crystallites are formed is discussed below. The conceptual explanation of the nano- crystallites given in relation to figures 8a-c applies to this implementation as well.
To deposit the waveguide core, an aluminium oxide film may be deposited using reactive magnetron sputtering. An O2 flow of 2.8 sccm with a deposition rate of 3.74 nm/min and a stage temperature of 760°C was used to deposit a 786 nm thick Al;03:Er” layer with a refractive index of 1.739 at 1030 nm, which was measured using variable angle spectroscopic ellipsometry, VASE.
Erbium concentration of the layer is approximately known to be 3.9 x 10?" ions/cm? using calibrated sputtering powers based on Rutherford backscattering measurements, RBS. Samples were stored in N2 ambient in between fabrication steps to avoid OH- contamination which is a known source of recombination centres in erbium-doped amplifiers. Electron-beam lithography,
EBL, was used to pattern negative resist at a dose of 1000 uC/cm? to be used as an etch mask for the definition of spirals, ring resonators and straight waveguides for signal enhancement and background loss characterization. Reactive ion-etching, RIE, was performed to define the waveguides with 25 and 10 sccm of BC13 and HBr gas flows respectively at a chamber pressure of 3 mTorr and 25W RF power. Plasma-enhanced chemical vapour deposition, PECVD, was used to deposit a SiO2 cladding at a deposition rate of 37 nm/min using 200 and 710 sccm of SiH4/N2 and
N20 respectively, with a chamber pressure of 650 mTorr at 300 °C stage temperature and 60W of power. Chips were diced and annealed at 550 °C in a tube furnace with N2 ambient. In order to reduce the coupling losses (ac), chip sidewall polishing was performed to reduce scattering losses using a Flex Waveguide Polisher from KrellTech with a variety of polishing pads of varying roughness of 3.0, 1.0 and 0.3 um wet with demi water.
Using this particular example, an A1203:Er** waveguide may be manufactured which demonstrates gain at 1532 nm of 33.5 dB, with 475 mW (26.1 dBm) of on-chip power for a 12.9 cm amplifier.
This can be derived, for example, using a set up as shown in figure 10, including amplifiers with bidirectional pumping using off-chip WDMs and a filter to cut-off spectra below 1500 nm. In such a set-up, two signal sources may be used for switching from low to high power signal regimes. The resulting signal may be monitored using an optical spectrum analyzer, OSA. Spirals of different lengths (see figure 11) were measured for varying pump and signal powers, demonstrating peak on-chip gain per unit length of 3.5 dB/cm at 1532 nm in a 4.9 cm amplifier.
The reactively sputtered ALOs:Er*" waveguide amplifiers has an erbium concentration of 3.9x10% ions/cm3 and is capable of achieving over 30 dB gain at 1532 nm using bidirectional pumping at 1480 nm, as can be observed relying on the set up shown in figure 10. Chip output powers shown here exceed 120 mW, demonstrating the advantages achieved in an optical waveguide core manufactured according to the method of the invention.
The inventive concept generally concerns providing a waveguide core, having a minimum amount of quenching. This can be achieved following the method of appended claim 1.
Quenching may be said to, more or less, be a result of the clustering of rare earth ions. If most ions are part of a cluster, it becomes more likely a photon emitted due to spontaneous emission is emitted in a cluster, meaning it is more likely to interact with other nearby ions in said cluster. Therefore, as an alternative, a method according to the invention can be characterized in that depositing the waveguide core comprises forming nano-crystallites in the waveguide core, wherein a lowest temperature at which a percentage of rare earth ions that is comprised by clusters significantly increases exceeds the given maximum temperature, and that the given maximum temperature is about 400 degrees Celsius or higher.
Larger clusters mean that a photon emitted by an ion due to spontaneous emission is more likely to interact with other nearby ions, if only because in larger clusters, there are more nearby ions. Therefore, as an alternative, a method according to the invention can be characterized in that depositing the waveguide core comprises forming nano-crystallites in the waveguide core, that the lowest temperature at which an average size of clusters of ions significantly increases, exceeds the maximum temperature and that the given maximum temperature is about 400 degrees Celsius or higher.
In the art of crystallography, clusters are sometimes described based on the number of ions included therein, e.g. a monomer refers to a lone ion in an otherwise at least locally uniform host material. A dimer refers to a cluster of two, and a trimer refers to a cluster of three. Having no clusters of rare earth ions can therefore be positively formulated as that the rare earth ions that are present, are monomers. Therefore, as an alternative, a method according to the invention can be characterized in that depositing the waveguide core comprises forming nano-crystallites in the waveguide core, that the lowest temperature at which a number of monomer ions significantly decreases exceeds the given maximum temperature, and that the given maximum temperature is about 400 degrees Celsius or higher.
In the above, the present invention has been explained using detailed embodiments thereof.
However, it should be apparent to the skilled person that various modifications are possible to these embodiments without deviating from the scope of the present invention, which is defined by the appended claims and their equivalents.

Claims (23)

CONCLUSIESCONCLUSIONS 1. Werkwijze voor het fabriceren van een optische golfgeleider, de werkwijze omvattende: het verschaffen van een substraat; het deponeren van een aluminiumoxide golfgeleider-kern gedoteerd met ionen van een zeldzaam aardmetaal op het substraat; het rangschikken van een mantellaag (“cladding layer”) op de gedeponeerde golfgeleider- kern, het rangschikken omvattende ten minste een verwerkingsstap waarbij de gedeponeerde golfgeleider-kern blootgesteld wordt aan een gegeven maximale temperatuur; met het kenmerk dat het deponeren van de golfgeleider-kern het vormen van nano- kristallieten in de golfgeleider-kern omvat; waarbij een laagste temperatuur waarop een uitdoof-percentage (“quenching percentage”) van de gedeponeerde golfgeleider-kern significant toeneemt de gegeven maximale temperatuur overschrijdt, waarbij de gegeven maximale temperatuur ongeveer 400 graden Celsius is of hoger.1. A method of manufacturing an optical waveguide, the method comprising: providing a substrate; depositing an aluminum oxide waveguide core doped with ions of a rare earth metal on the substrate; arranging a cladding layer on the deposited waveguide core, the arranging comprising at least one processing step of exposing the deposited waveguide core to a given maximum temperature; characterized in that depositing the waveguide core comprises forming nano-crystallites in the waveguide core; wherein a lowest temperature at which a quenching percentage of the deposited waveguide core increases significantly exceeds the given maximum temperature, wherein the given maximum temperature is about 400 degrees Celsius or higher. 2. Werkwijze volgens conclusie 1, waarbij een toename in uitdoof-percentage significant is wanneer deze ongeveer 20% punt of meer is. en bij voorkeur wanneer deze tussen ongeveer 5% en ongeveer 20% is.2. The method of claim 1, wherein an increase in extinction rate is significant when it is about 20% point or more, and preferably when it is between about 5% and about 20%. 3. Werkwijze volgens conclusie | of 2, waarbij de gegeven maximale temperatuur in een bereik ligt tussen 400 en 1400 graden Celsius, bij voorkeur tussen 500 en 800 graden Celsius, en meer bij voorkeur ongeveer 550 graden Celsius is.3. A method according to claim | or 2, wherein the given maximum temperature is in a range between 400 and 1400 degrees Celsius, preferably between 500 and 800 degrees Celsius, and more preferably about 550 degrees Celsius. 4. Werkwijze volgens conclusie 1, 2. of 3, waarbij het rangschikken van de mantellaag het deponeren van de mantellaag op de gedeponeerde golfgeleider-kern omvat en waarbij de ten minste een verwerkingsstap het annealen van de combinatie van het substraat, de gedeponeerde golfgeleider-kern, en de gedeponeerde mantellaag op de gegeven maximale temperatuur omvat.4. The method of claim 1, 2 or 3, wherein arranging the cladding layer comprises depositing the cladding layer onto the deposited waveguide core and wherein the at least one processing step comprises annealing the combination of the substrate, the deposited waveguide core, and the deposited cladding layer at the given maximum temperature. 5. Werkwijze volgens conclusie 4, waarbij het uitdoof-percentage van de aluminiumoxide golfgeleider-kern na het deponeren van de mantellaag en voor het annealen tussen ongeveer 5% en ongeveer 35% is.5. The method of claim 4, wherein the quenching percentage of the aluminum oxide waveguide core after deposition of the cladding layer and before annealing is between about 5% and about 35%. 6. Werkwijze volgens conclusie 5, waarbij het uitdoof-percentage van de golfgeleider-kern na het annealen tussen ongeveer 0% en ongeveer 35% is, en bij voorkeur tussen ongeveer 0% en ongeveer 5%.6. The method of claim 5, wherein the extinction percentage of the waveguide core after annealing is between about 0% and about 35%, and preferably between about 0% and about 5%. 7. Werkwijze volgens conclusie 1, 2, of 3, waarbij de ten minste een verwerkingsstap het deponeren van de mantellaag op de aluminiumoxide golfgeleider-kern bij de gegeven maximale temperatuur omvat.7. A method according to claim 1, 2, or 3, wherein the at least one processing step comprises depositing the cladding layer on the aluminum oxide waveguide core at the given maximum temperature. 8. Werkwijze volgens conclusie 7, waarbij het uitdoot-percentage van de aluminiumoxide golfgeleider-kern na het deponeren van de mantellaag tussen ongeveer 0% en ongeveer 35% is, bij voorkeur tussen ongeveer 0% en ongeveer 5%.8. The method of claim 7, wherein the quenching percentage of the aluminum oxide waveguide core after depositing the cladding layer is between about 0% and about 35%, preferably between about 0% and about 5%. 9. Werkwijze volgens een van de voorgaande conclusies, waarbij het zeldzame aardemetaal een lanthanide is, zoals Erbium, bij voorkeur Er’, Ytterbium, bij voorkeur Yb**, thuliam, bij voorkeur Tm’, en/of Neodymium, bij voorkeur Nd*.9. A method according to any preceding claim, wherein the rare earth metal is a lanthanide, such as Erbium, preferably Er’, Ytterbium, preferably Yb**, Thulium, preferably Tm’, and/or Neodymium, preferably Nd*. 10. Werkwijze volgens een van de voorgaande conclusies, waarbij de aluminiumoxide stoichiometrisch is. en/of de golfgeleider-kern AlxOy omvat, waarbij 1.5 <x <25en2.5<y<10. A method according to any preceding claim, wherein the aluminium oxide is stoichiometric and/or the waveguide core comprises AlxOy, where 1.5 < x < 25 and 2.5 < y< 3.5, zoalsx = 1.6, en y = 3.4, en bij voorkeur x = 2, en y = 3.3.5, such as x = 1.6, and y = 3.4, and preferably x = 2, and y = 3. 11. Werkwijze volgens een van de voorgaande conclusies, waarbij de aluminiumoxide golfgeleider-kern wordt gegroeid met gebruik van een van reactieve sputter depositie, atomische laag depositie, verdamping. or gepulseerde laser depositie.A method according to any preceding claim, wherein the aluminum oxide waveguide core is grown using one of reactive sputter deposition, atomic layer deposition, evaporation or pulsed laser deposition. 12. Werkwijze volgens een van de voorgaande conclusies, waarbij de mantellaag een TEOS-laag, een silicium-oxynitride laag, of een polymeer-laag omvat.12. A method according to any preceding claim, wherein the cladding layer comprises a TEOS layer, a silicon oxynitride layer, or a polymer layer. 13. Werkwijze volgens een van de voorgaande conclusies, waarbij de mantellaag wordt gerangschikt met gebruik van een plasma-versterkte dampdepositie, lage druk chemische dampdepositie, verdamping, sputteren, of atomische laag depositie.13. A method according to any preceding claim, wherein the cladding layer is arranged using plasma enhanced vapor deposition, low pressure chemical vapor deposition, evaporation, sputtering, or atomic layer deposition. 14. Werkwijze volgens een van de voorgaande conclusies, waarbij het substraat een silicium substraat, een silicium thermische oxide substraat, of een kwartssubstraat omvat.14. A method according to any preceding claim, wherein the substrate comprises a silicon substrate, a silicon thermal oxide substrate, or a quartz substrate. 15. Werkwijze volgens een van de voorgaande conclusies, waarbij de golfgeleider een plak-golfgeleider of een kanaal-golfgeleider is.15. A method according to any preceding claim, wherein the waveguide is a slice waveguide or a channel waveguide. 16. Werkwijze volgens een van de voorgaande conclusies, verder omvattende het 53 tussen het deponeren van de aluminiumoxide golfgeleider-kern en het rangschikken van de mantellaag in reduceren van oppervlakteruwheid van de aluminiumoxide golfgeleider-kern, bijvoorbeeld met gebruik van chemisch mechanisch polijsten.16. A method according to any preceding claim, further comprising reducing surface roughness of the aluminium oxide waveguide core between depositing the aluminium oxide waveguide core and arranging the cladding layer, for example using chemical mechanical polishing. 17. Werkwijze volgens een van de voorgaande conclusies, verder omvattende het definiëren van een vorm en/of grootte van de aluminiumoxide golfgeleider-kern met gebruik van bijvoorbeeld ten minste een van lithografie en etsen, voorafgaand aan het rangschikken van de mantellaag.17. A method according to any preceding claim, further comprising defining a shape and/or size of the aluminum oxide waveguide core using, for example, at least one of lithography and etching, prior to arranging the cladding layer. 18. Werkwijze volgens een van de voorgaande conclusies, omvattende: het met een depositiesnelheid voor aluminiumoxide deponeren van alaminiumoxidelagen gedoteerd met zeldzame aarde ionen bij verschillende substraattemperaturen en/of bij verschillende substraat-voorspanningen op respectievelijke substraten; het voor elke gedeponeerde aluminiumoxide laag meten van diens uitdoof-percentage; het als optimale instellingen selecteren van de genoemde depositiesnelheid en de substraattemperatuur en de substraat-voorspanning waarmee de aluminiumoxide laag was gefabriceerd die het laagste uitdoof-percentage had; het gebruikmaken van de optimale instellingen bij het deponeren van de aluminiumoxide golfgeleider-kern voor het fabriceren van de optische golfgeleider volgens een van de voorgaande conclusies.18. A method according to any preceding claim, comprising: depositing rare earth ion doped aluminum oxide layers at an aluminum oxide deposition rate at different substrate temperatures and/or at different substrate bias voltages on respective substrates; measuring the extinction percentage of each deposited aluminum oxide layer; selecting as optimal settings said deposition rate and the substrate temperature and substrate bias voltage at which the aluminum oxide layer having the lowest extinction percentage was fabricated; using the optimal settings when depositing the aluminum oxide waveguide core for fabricating the optical waveguide according to any preceding claim. 19. Optische golfgeleider, omvattende: een substraat; een aluminiumoxide golfgeleider-kern gedoteerd met ionen van een zeldzaam aardemetaal, gerangschikt op het substraat; en een mantellaag gerangschikt op de aluminiumoxide golfgeleider-kern; met het kenmerk, dat de aluminiumoxide golfgeleider-kern nano-kristallieten omvat, dat een uitdoofpercentage van de optische golfgeleider 5% of minder is, en waarbij de mantellaag een hoge-temperatuur mantellaag omvat.19. An optical waveguide comprising: a substrate; an aluminum oxide waveguide core doped with ions of a rare earth metal arranged on the substrate; and a cladding layer arranged on the aluminum oxide waveguide core; characterized in that the aluminum oxide waveguide core comprises nano-crystallites, a quenching percentage of the optical waveguide is 5% or less, and the cladding layer comprises a high-temperature cladding layer. 20. Optische golfgeleider volgens conclusie 19, waarbij de nano-kristallieten tussen 1 nanometer en 30 nanometer in grootte zijn, bij voorkeur tussen | nanometer en 10 nanometer in grootte zijn, en/of waarbij de nano-kristallieten ten minste 50% in gewicht van de aluminiumoxide golfgeleider-kern vormen, bij voorkeur ten minste 75%, en meer bij voorkeur ten minste 99%.20. An optical waveguide according to claim 19, wherein the nano-crystallites are between 1 nanometer and 30 nanometers in size, preferably between 1 nanometer and 10 nanometers in size, and/or wherein the nano-crystallites constitute at least 50% by weight of the aluminum oxide waveguide core, preferably at least 75%, and more preferably at least 99%. 21. Optische golfgeleider volgens een van de conclusies 19-22, waarbij de hoge- 53 temperatuur mantellaag ten minste een van een TEOS-laag of een silicium-oxynitride laag omvat.21. The optical waveguide of any one of claims 19 to 22, wherein the high temperature cladding layer comprises at least one of a TEOS layer or a silicon oxynitride layer. 22. Optische golfgeleider volgens een van de conclusies 19-23, waarbij de golfgeleider een plak-golfgeleider of een kanaal-golfgeleider is.22. An optical waveguide according to any one of claims 19 to 23, wherein the waveguide is a slice waveguide or a channel waveguide. 23. Optische golfgeleider volgens een van de conclusies 19-24, waarbij de optische golfgeleider is vervaardigd door een werkwijze volgens een van de conclusies 1-18.23. An optical waveguide according to any one of claims 19 to 24, wherein the optical waveguide is manufactured by a method according to any one of claims 1 to 18.
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