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JP2008173573A - Composite hollow fiber membrane - Google Patents

Composite hollow fiber membrane Download PDF

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JP2008173573A
JP2008173573A JP2007009868A JP2007009868A JP2008173573A JP 2008173573 A JP2008173573 A JP 2008173573A JP 2007009868 A JP2007009868 A JP 2007009868A JP 2007009868 A JP2007009868 A JP 2007009868A JP 2008173573 A JP2008173573 A JP 2008173573A
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support layer
hollow fiber
fiber membrane
resin
separation
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Takashi Minaki
尚 皆木
Masayuki Hanakawa
正行 花川
Shinichi Minegishi
進一 峯岸
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Toray Industries Inc
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Toray Industries Inc
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Abstract

<P>PROBLEM TO BE SOLVED: To provide a composite hollow fiber membrane for gas separation which is made of a thermoplastic resin having particularly high chemical resistance and hydrophobicity and is provided with high gas permeability, high rupture elongation, and high heat resistance in addition to high gas separation property. <P>SOLUTION: The composite hollow fiber membrane comprising a support layer having a spherical structure of a thermoplastic resin and a separation layer made of a non-porous material is produced. The composite hollow fiber membrane has the size of 2 μm or smaller in the voids at the point of 5 μm depth in the support layer direction from the interface in the separation layer side of the support layer in a longitudinal cross-sectional photograph of the composite hollow fiber membrane. <P>COPYRIGHT: (C)2008,JPO&INPIT

Description

本発明は、気体混合物の成分を選択分離するための複合中空糸膜に関する。さらに詳しくは、空気から酸素と窒素への分離、プラットフォーミング法のオフガスからの水素の分離回収、アンモニア合成時の水素の分離回収、火力発電やゴミ焼却の排ガスからの二酸化炭素の回収および窒素酸化物や硫黄酸化物の除去、油田のオフガスからの二酸化炭素の回収、メタンを主成分とする天然ガスからの硫化水素、二酸化炭素などの酸性ガスの除去やヘリウムの分離回収、精密機械用やオゾン発生機用の空気除湿、有機溶剤からの脱水など、多くの分野に適用される。   The present invention relates to a composite hollow fiber membrane for selectively separating components of a gas mixture. More specifically, separation of air from oxygen and nitrogen, separation and recovery of hydrogen from off-gas of the platform method, separation and recovery of hydrogen during ammonia synthesis, recovery of carbon dioxide from exhaust gas from thermal power generation and garbage incineration, and nitrogen oxidation Removal of substances and sulfur oxides, recovery of carbon dioxide from oilfield off-gas, removal of acidic gases such as hydrogen sulfide and carbon dioxide from natural gas mainly composed of methane, separation and recovery of helium, precision machinery and ozone It is applied to many fields such as air dehumidification for generators and dehydration from organic solvents.

すべての高分子素材は、大なり小なり気体透過性を有し、その透過性は素材の種類と気体の種類により大きく異なることから、高分子膜を用いて気体混合物から特定の成分を分離濃縮できることが古くから知られている。膜による気体分離は、他の分離方法と比較して、エネルギー的に有利で、装置が小型軽量、機構が簡単でメンテナンスフリーなどの特徴を有するため、各種産業分野で活発に適用されている。特に近年は、省資源、省エネルギー、有用なガスの回収などの観点から注目を集めている。   All polymer materials are more or less gas permeable, and their permeability varies greatly depending on the type of material and the type of gas. Therefore, a polymer membrane is used to separate and concentrate specific components from a gas mixture. It has been known for a long time. Gas separation by a membrane is actively applied in various industrial fields because it is advantageous in terms of energy as compared with other separation methods, and has features such as a small and light apparatus, a simple mechanism, and maintenance-free characteristics. In particular, in recent years, it has attracted attention from the viewpoints of resource saving, energy saving, and recovery of useful gas.

このような気体分離膜に対しては、混合気体から目的の気体成分を選択的に分離する性能と、効率良く目的の気体成分を透過する性能が高いことが要求される。すなわち気体分離性と気体透過性がともに高いことが重要である。一般に気体分離性は、緻密な膜の場合、本質的に膜素材固有の特性である。これに対して気体透過性は、均質の膜の場合、膜厚に反比例する。従って気体分離膜の製造に当たっては、いかに薄く、かつ緻密な膜を生成するかが重要な課題となるが、他方、膜厚の低下に伴い機械的強度が低下するので、実用化可能な膜厚には限界があった。   Such a gas separation membrane is required to have high performance for selectively separating a target gas component from a mixed gas and high performance for efficiently transmitting the target gas component. That is, it is important that both gas separation property and gas permeability are high. In general, gas separability is an inherent characteristic of a membrane material in the case of a dense membrane. In contrast, gas permeability is inversely proportional to film thickness in the case of a homogeneous film. Therefore, in the production of gas separation membranes, how to produce a thin and dense membrane is an important issue, but on the other hand, the mechanical strength decreases as the film thickness decreases, so the film thickness that can be put to practical use. There were limits.

また上述したように用途は様々であり、使用環境も様々である。そのため、混合気体を加圧するためにコンプレッサーを使用する場合や、温の混合気体をそのまま使用したりする場合には、高温での耐熱性が必要になる。しかしながら、従来の高分子膜は高温で使用すると、分離能の低下が起こるという問題があった。   Further, as described above, there are various uses and various usage environments. Therefore, when a compressor is used to pressurize the mixed gas, or when a warm mixed gas is used as it is, heat resistance at high temperatures is required. However, when the conventional polymer membrane is used at a high temperature, there is a problem that the separation performance is lowered.

以上のような背景から、膜素材固有の気体分離性に加えて、気体透過性と機械的強度、さらに耐熱性を有する分離膜が必要であり、種々提案されている。   In view of the above background, a separation membrane having gas permeability, mechanical strength, and heat resistance is required in addition to the gas separation property inherent to the membrane material, and various proposals have been made.

その一つとして、高分子膜に、高い気体分離性を有する薄い緻密層と、比較的厚く、機械的強度と気体透過性を併せもつ多孔質層の二層を一体的に生成させた、いわゆる非対称分離膜がある。例えば、特許文献1に、フルオレン骨格を有するポリエステル、ポリエーテル、ポリカーボネート、ポリアミド、ポリイミドのうち少なくとも1種のポリマーを含むポリマーの混合体の溶液を用い、従来の湿式紡糸法により表層が緻密で、膜全体に渡って実質的にスポンジ構造からなる中空糸膜が報告されている。しかし、緻密層の気体透過性をある程度高くする必要性から、溶液のポリマー濃度を高くできず、またスポンジ構造からなるために、その機械的強度は十分ではなく、耐熱性も低いという問題がある。   As one of them, a so-called thin dense layer having a high gas separation property and a relatively thick porous layer having both mechanical strength and gas permeability are integrally formed on a polymer membrane. There is an asymmetric separation membrane. For example, in Patent Document 1, using a solution of a polymer mixture containing at least one polymer of polyester, polyether, polycarbonate, polyamide, and polyimide having a fluorene skeleton, the surface layer is dense by a conventional wet spinning method, A hollow fiber membrane having a substantially sponge structure over the entire membrane has been reported. However, due to the necessity of increasing the gas permeability of the dense layer to some extent, the polymer concentration of the solution cannot be increased, and since it has a sponge structure, its mechanical strength is not sufficient and heat resistance is also low. .

そこでさらに別の方法として、高分子体の緻密な薄膜を、多孔質体の支持基材の上に積層する、いわゆる複合膜化がある。例えば、特許文献2、3に耐薬品性が高く、疎水性が高いために、気体分離膜に適している、ポリフッ化ビニリデンを素材とする支持層に高い気体透過性を有する、ポリアセチレンあるいはシリコーンポリマーからなる薄い緻密層を積層した中空糸膜が報告されている。しかし、いずれの場合も非溶媒誘起相分離により支持層を形成していることから、マクロボイドと呼ばれる欠陥を有したスポンジ構造からなり、その機械的強度は必ずしも十分ではない。またこのような複合膜の耐熱性は低い。その原因として、緻密な薄膜が熱変形、熱劣化することがあるが、それ以上に支持層の熱変形による影響が大きいことがわかっている。
特開平06−091145号公報 特開昭63−315104号公報 特開平09−066224号公報
Therefore, as another method, there is a so-called composite film formation in which a dense thin film of a polymer is laminated on a porous support substrate. For example, in Patent Documents 2 and 3, polyacetylene or silicone polymer having high gas permeability in a support layer made of polyvinylidene fluoride, which is suitable for gas separation membranes because of high chemical resistance and high hydrophobicity. A hollow fiber membrane in which a thin dense layer made of is laminated has been reported. However, in any case, since the support layer is formed by non-solvent induced phase separation, it has a sponge structure having defects called macrovoids, and its mechanical strength is not always sufficient. Moreover, the heat resistance of such a composite membrane is low. As a cause of this, a dense thin film may be thermally deformed or deteriorated. However, it is known that the influence of the heat deformation of the support layer is greater than that.
Japanese Patent Laid-Open No. 06-091145 JP-A-63-315104 Japanese Patent Application Laid-Open No. 09-066224

本発明では上記のような問題点に鑑み、特に耐薬品性、疎水性の高い熱可塑性樹脂からなり、高い気体分離性に加えて、高い気体透過性、高い破断強伸度、高い耐熱性を併せ持った、気体分離用の複合中空糸膜を提供することを目的とする。   In the present invention, in view of the above problems, it is made of a thermoplastic resin having high chemical resistance and high hydrophobicity. In addition to high gas separation properties, it has high gas permeability, high breaking strength, and high heat resistance. Another object is to provide a composite hollow fiber membrane for gas separation.

上記課題を解決するための本発明は、
(1)熱可塑性樹脂の球状構造からなる支持層と、非多孔質材料からなる分離層から構成される複合中空糸膜であって、複合中空糸膜の長手方向に垂直な断面写真において、支持層の分離層側の界面から支持層方向に深さ5μmの位置の空隙の大きさが2μm以下であることを特徴とする複合中空糸膜。
(2)支持層の分離層と反対側を形成する球状構造の平均直径D2が0.1μm以上2μm以下である請求項1記載の複合中空糸膜。
(3)支持層の分離層側を形成する球状構造の平均直径D1と前記平均直径D2が、D1<D2の関係を満たす請求項2に記載の複合中空糸膜。
(4)支持層の分離層側が三次元網目構造からなり、支持層の分離層と反対側が球状構造からなる請求項1または2に記載の複合中空糸膜。
(5)熱可塑性樹脂がポリフッ化ビニリデン樹脂である請求項1〜4のいずれかに記載の複合中空糸膜。
により構成される。
The present invention for solving the above problems is as follows.
(1) A composite hollow fiber membrane composed of a support layer composed of a spherical structure of a thermoplastic resin and a separation layer composed of a non-porous material, in a cross-sectional photograph perpendicular to the longitudinal direction of the composite hollow fiber membrane A composite hollow fiber membrane, wherein the size of a void at a depth of 5 µm in the direction of the support layer from the interface on the separation layer side of the layer is 2 µm or less.
(2) The composite hollow fiber membrane according to claim 1, wherein the spherical structure forming the opposite side of the support layer from the separation layer has an average diameter D2 of 0.1 μm or more and 2 μm or less.
(3) The composite hollow fiber membrane according to claim 2, wherein the average diameter D1 of the spherical structure forming the separation layer side of the support layer and the average diameter D2 satisfy a relationship of D1 <D2.
(4) The composite hollow fiber membrane according to claim 1 or 2, wherein the separation layer side of the support layer has a three-dimensional network structure, and the opposite side of the support layer to the separation layer has a spherical structure.
(5) The composite hollow fiber membrane according to any one of claims 1 to 4, wherein the thermoplastic resin is a polyvinylidene fluoride resin.
Consists of.

本発明によれば、気体分離性に加えて、気体透過性、破断強伸度、耐熱性、耐薬品性の高い中空糸膜を提供することができ、広範囲の気体分離用途に利用できる。   According to the present invention, in addition to gas separability, a hollow fiber membrane having high gas permeability, breaking strength, heat resistance, and chemical resistance can be provided, and can be used for a wide range of gas separation applications.

本発明の複合中空糸膜は、熱可塑性樹脂の球状構造からなる支持層と、非多孔質材料からなる分離層から構成される複合中空糸膜であって、複合中空糸膜の長手方向に垂直な断面写真において、支持層の分離層側の界面から支持層方向に深さ5μmの位置の空隙の大きさが2μm以下であることにより、高い破断強伸度、高い気体透過性、高い耐熱性を有することを特徴とする。すなわち複合中空糸膜が高性能を発現するためには、支持層の構造が非常に重要である。本発明の支持層は高い破断強伸度、高い気体透過性、高い耐熱性を有し、かつその上に形成される分離層を均一に形成させ、かつ分離層との接着性を高くすることができる。その結果、分離層は支持層上に薄く均一に形成させることができ、高い気体透過性を発現できる。   The composite hollow fiber membrane of the present invention is a composite hollow fiber membrane composed of a support layer composed of a spherical structure of a thermoplastic resin and a separation layer composed of a non-porous material, and is perpendicular to the longitudinal direction of the composite hollow fiber membrane. In a cross-sectional photograph, the void size at a depth of 5 μm in the direction of the support layer from the interface on the separation layer side of the support layer is 2 μm or less, so that high breaking strength, high gas permeability, and high heat resistance It is characterized by having. That is, the structure of the support layer is very important for the composite hollow fiber membrane to exhibit high performance. The support layer of the present invention has high breaking strength, high gas permeability, and high heat resistance, and the separation layer formed thereon is uniformly formed, and the adhesiveness with the separation layer is increased. Can do. As a result, the separation layer can be thinly and uniformly formed on the support layer and can exhibit high gas permeability.

本発明における重要である支持層の構造は、おもに熱可塑性樹脂の球状構造からなることが必要である。   The structure of the support layer, which is important in the present invention, needs to consist mainly of a spherical structure of a thermoplastic resin.

ここで熱可塑性樹脂とは、鎖状高分子物質からできており、加熱すると、外力によって変形・流動する性質が現れる樹脂のことをいう。この熱可塑性樹脂の例としては、ポリエチレン樹脂、ポリプロピレン樹脂、アクリル樹脂、ポリアクリロニトリル樹脂、アクリロニトリル−ブタジエン−スチレン(ABS)樹脂、ポリスチレン樹脂、アクリロニトリル−スチレン(AS)樹脂、塩化ビニル樹脂、ポリエチレンテレフタレート樹脂、ポリアミド樹脂、ポリアセタール樹脂、ポリカーボネート樹脂、変成ポリフェニレンエーテル樹脂、ポリフェニレンスルフィド樹脂、ポリフッ化ビニリデン樹脂、ポリアミドイミド樹脂、ポリエーテルイミド樹脂、ポリスルホン樹脂、ポリエーテルスルホン樹脂およびこれらの混合物や共重合体が挙げられる。これらと混和可能な他の樹脂および多価アルコールや界面活性剤を50重量%以下含んでいてもよい。   Here, the thermoplastic resin refers to a resin that is made of a chain polymer substance and that exhibits a property of being deformed / flowed by an external force when heated. Examples of this thermoplastic resin include polyethylene resin, polypropylene resin, acrylic resin, polyacrylonitrile resin, acrylonitrile-butadiene-styrene (ABS) resin, polystyrene resin, acrylonitrile-styrene (AS) resin, vinyl chloride resin, polyethylene terephthalate resin. , Polyamide resin, polyacetal resin, polycarbonate resin, modified polyphenylene ether resin, polyphenylene sulfide resin, polyvinylidene fluoride resin, polyamideimide resin, polyetherimide resin, polysulfone resin, polyethersulfone resin, and mixtures and copolymers thereof. It is done. Other resins miscible with these and polyhydric alcohols or surfactants may be contained in an amount of 50% by weight or less.

このうち本発明には、疎水性であり、耐薬品性、物理的強度が高いポリフッ化ビニリデン樹脂がより好ましく用いられる。ポリフッ化ビニリデン樹脂とはフッ化ビニリデンホモポリマーおよび/またはフッ化ビニリデン共重合体を含有する樹脂を意味し、複数の種類のフッ化ビニリデン共重合体を含有しても構わない。フッ化ビニリデン共重合体は、フッ化ビニリデン残基構造を有するポリマーであり、典型的にはフッ化ビニリデンモノマーとそれ以外のフッ素系モノマーなどとの共重合体である。かかる共重合体としては、例えば、フッ化ビニル、四フッ化エチレン、六フッ化プロピレン、三フッ化塩化エチレンから選ばれた1種類以上とフッ化ビニリデンとの共重合体が挙げられる。また、本発明の効果を損なわない程度に、前記フッ素系モノマー以外の例えばエチレンなどのモノマーが共重合されていても良い。   Among these, in the present invention, a polyvinylidene fluoride resin that is hydrophobic, has high chemical resistance, and high physical strength is more preferably used. The polyvinylidene fluoride resin means a resin containing a vinylidene fluoride homopolymer and / or a vinylidene fluoride copolymer, and may contain a plurality of types of vinylidene fluoride copolymers. The vinylidene fluoride copolymer is a polymer having a vinylidene fluoride residue structure, and is typically a copolymer of a vinylidene fluoride monomer and other fluorine-based monomers. Examples of the copolymer include a copolymer of vinylidene fluoride and at least one selected from vinyl fluoride, tetrafluoroethylene, hexafluoropropylene, and trifluoroethylene chloride. Further, a monomer such as ethylene other than the fluorine-based monomer may be copolymerized to such an extent that the effects of the present invention are not impaired.

次に球状構造とは支持層の長手方向に垂直な断面に見られる、球状の固形部が互いにその一部を共有することにより連結された構造である。比較的大きな固形部がその多くの部分を共有して連結された構造であることから物理的強度が高く、同時に空隙も大きくなることから気体透過性も高くなる。   Next, the spherical structure is a structure in which spherical solid portions, which are seen in a cross section perpendicular to the longitudinal direction of the support layer, are connected by sharing a part thereof. Since the relatively large solid part is connected to share many parts, the physical strength is high, and at the same time, the voids are large, so that the gas permeability is also high.

またその球状構造の平均直径は0.1μm以上2μm以下が好ましい。ここで球状構造の平均直径とは球状の固形部の平均直径(長径と短径の平均値)である。平均直径が0.1μm未満では、球状構造間の空隙も小さくなり気体透過性が低下してしまう。逆に2μmを超えると、球状の固形部間の連結が少なくなり、物理的強度が低下し、さらに高温下の熱収縮率が大きくなってしまうため耐熱性が低下する。また複合中空糸膜の気体透過性は、支持層より分離層の影響が大きいため、支持層の気体透過性を下げ、破断強伸度、耐熱性を高くする方が、気体分離膜として有効であることから、支持層の球状構造の平均直径は、より好ましくは0.1μm以上1.5μm以下、さらに好ましくは0.1μm以上0.7μm以下である。   The average diameter of the spherical structure is preferably 0.1 μm or more and 2 μm or less. Here, the average diameter of the spherical structure is the average diameter (average value of the major axis and the minor axis) of the spherical solid part. If the average diameter is less than 0.1 μm, the gaps between the spherical structures are also reduced and the gas permeability is lowered. On the other hand, when the thickness exceeds 2 μm, the connection between the spherical solid parts is reduced, the physical strength is lowered, and the heat shrinkage rate at high temperature is increased, so that the heat resistance is lowered. In addition, since the gas permeability of the composite hollow fiber membrane is more affected by the separation layer than the support layer, it is more effective as a gas separation membrane to lower the gas permeability of the support layer and increase the breaking strength and heat resistance. Therefore, the average diameter of the spherical structure of the support layer is more preferably 0.1 μm or more and 1.5 μm or less, and further preferably 0.1 μm or more and 0.7 μm or less.

本発明では球状構造からなることが必要であるが、三次元網目構造などその他の構造を含んでいてもよい。   In the present invention, it is necessary to have a spherical structure, but other structures such as a three-dimensional network structure may be included.

また本発明の支持層は、複合中空糸膜の長手方向に垂直な断面写真において、支持層の分離層側の界面から支持層方向に深さ5μmの位置の空隙の大きさが2μm以下であることが必要である。この空隙とは支持層の孔であり、支持層の分離層側の界面からの連通孔であっても、孤立孔であってもよい。この位置に2μmより大きい孔を有すると、それが界面からの連通孔の場合、分離層が孔内に入り込むことで支持層上に均一に形成されずに欠陥を生じてしまい、孤立孔の場合、その分離層側には薄い固形部が存在し、その部分は物理的耐久性が低く、気体透過時に圧力によって破壊されてしまう。   In the support layer of the present invention, in the cross-sectional photograph perpendicular to the longitudinal direction of the composite hollow fiber membrane, the size of the void at a depth of 5 μm in the support layer direction from the interface on the separation layer side of the support layer is 2 μm or less. It is necessary. This void is a hole in the support layer, and may be a communication hole from the interface on the separation layer side of the support layer or an isolated hole. If there is a hole larger than 2 μm at this position, if it is a communicating hole from the interface, the separation layer will enter the hole, causing a defect that is not formed uniformly on the support layer. A thin solid portion exists on the separation layer side, and the portion has low physical durability, and is destroyed by pressure during gas permeation.

すなわち、支持層上に均一に薄い分離層を強固に形成させるためには、支持層の分離層側の界面は、気体透過性を著しく損なわない程度に、できるだけ孔の小さい緻密な構造であることが望ましい。ここで、支持層の分離層側の界面から支持層方向に深さ5μmの位置の空隙の大きさは実施例に記載のとおり測定するものとする。   In other words, in order to firmly form a uniform thin separation layer on the support layer, the interface on the separation layer side of the support layer must have a dense structure with as few pores as possible so as not to significantly impair gas permeability. Is desirable. Here, the size of the void at a depth of 5 μm in the direction of the support layer from the interface on the separation layer side of the support layer is measured as described in the examples.

たまたま撮影した20μm四方の写真において空隙の大きさが2μmを超えることがなかったとしても、本発明の要件を満たすわけではなく、あらゆる箇所の写真において、同様に空隙の大きさを測定し、すべての箇所のすべての空隙の大きさが2μm以下である場合に、本発明の要件を満たすこととするが、逆に極めて低い確率で空隙の大きさが2μmを超えることがあったとしても、本発明の本質を損なうものではない。そこで、12箇所測定してすべての空隙の大きさが2μm以下であればよいものとする。   Even if the 20 μm square photographed by chance does not exceed 2 μm, it does not satisfy the requirements of the present invention. In the case where the size of all the gaps in the part is 2 μm or less, the requirement of the present invention is satisfied. Conversely, even if the size of the gap exceeds 2 μm with a very low probability, It does not impair the essence of the invention. Therefore, it is sufficient that the size of all voids is 2 μm or less by measuring 12 points.

このように、おもに球状構造からなる支持層の分離層側の界面を緻密な構造にするためには、球状構造の平均直径を小さくすること、あるいは支持層を凝固させる際にその表面の凝固速度を高くし緻密化を促進させることが好ましく採用される。   In this way, in order to make the interface on the separation layer side of the support layer mainly composed of a spherical structure, the average diameter of the spherical structure is reduced, or the solidification rate of the surface when the support layer is solidified. It is preferably employed to increase the density and promote densification.

またさらに好ましい方法としては、支持層を、支持層の分離層側を形成する球状構造の平均直径D1と支持層の分離層と反対側を形成する球状構造の平均直径D2が、D1<D2の関係を満たす構造にする方法である。   Furthermore, as a more preferable method, the support layer has an average diameter D1 of the spherical structure forming the separation layer side of the support layer and an average diameter D2 of the spherical structure forming the side opposite to the separation layer of the support layer, where D1 <D2. It is a method to make the structure satisfying the relationship.

すなわち支持層の分離層側は、支持層上に均一に薄い分離層を形成させるために、気体透過性を著しく損なわない程度に、球状構造の平均直径をできるだけ小さくして孔の小さい緻密な構造にし、もう一方側は高い気体透過性を持たせるために、物理的強度を著しく損なわない程度に、球状構造の平均直径をできるだけ大きくして孔の大きい疎な構造にすることが好ましい。孔の小さい緻密な構造と孔の大きい疎な構造は段階的に構成されても、連続的に構成されても構わない。   That is, the separation layer side of the support layer has a dense structure with small pores by reducing the average diameter of the spherical structure as much as possible so that the gas permeability is not significantly impaired in order to form a uniformly thin separation layer on the support layer. In order to provide high gas permeability on the other side, it is preferable to make the average diameter of the spherical structure as large as possible to make the structure sparse with large pores so that the physical strength is not significantly impaired. The dense structure with small holes and the sparse structure with large holes may be formed stepwise or continuously.

具体的にはD1、D2はともに0.1μm以上2μm以下にすることが好ましく、より好ましくは、D1が0.1μm以上1.5μm以下、D2が0.8μm以上2μm以下であり、さらに好ましくはD1が0.1μm以上0.7μm以下、D2が1.2μm以上2μm以下である。   Specifically, both D1 and D2 are preferably 0.1 μm or more and 2 μm or less, more preferably D1 is 0.1 μm or more and 1.5 μm or less, D2 is 0.8 μm or more and 2 μm or less, and more preferably D1 is 0.1 μm or more and 0.7 μm or less, and D2 is 1.2 μm or more and 2 μm or less.

ここで支持層の分離層側を形成する球状構造の平均直径D1および支持層の分離層と反対側を形成する球状構造の平均直径D2の測定方法については実施例のとおりである。   Here, the measurement methods of the average diameter D1 of the spherical structure forming the separation layer side of the support layer and the average diameter D2 of the spherical structure forming the side opposite to the separation layer of the support layer are as in the examples.

また球状構造だけでなく、支持層の分離層側に三次元網目構造を形成させてもよい。ここで三次元網目構造とは、固形部が三次元的に網目状に広がっている構造のことをいう。この場合、三次元網目構造の分離層側の界面に緻密な構造を形成させることが必要である。また三次元網目構造は固形部が細く密度が小さいため、破断強伸度が低いので、球状構造の平均直径は、高い破断強伸度を持たせるために、0.1μm以上2μm以下が好ましく、より好ましくは0.1μm以上1.5μm以下で、さらに好ましくは0.1μm以上0.7μm以下である。   In addition to the spherical structure, a three-dimensional network structure may be formed on the separation layer side of the support layer. Here, the three-dimensional network structure refers to a structure in which the solid part is three-dimensionally spread in a network. In this case, it is necessary to form a dense structure at the interface on the separation layer side of the three-dimensional network structure. In addition, since the solid part is thin and the density is small, the three-dimensional network structure has a low breaking strength and elongation. Therefore, the average diameter of the spherical structure is preferably 0.1 μm or more and 2 μm or less in order to have a high breaking strength and elongation. More preferably, they are 0.1 micrometer or more and 1.5 micrometers or less, More preferably, they are 0.1 micrometer or more and 0.7 micrometers or less.

また支持層の厚みは、物理的強度と気体透過性を考慮して20〜1000μmが好ましく、より好ましくは30〜500μm、さらに好ましくは50〜350μmである。   The thickness of the support layer is preferably 20 to 1000 μm, more preferably 30 to 500 μm, and still more preferably 50 to 350 μm in consideration of physical strength and gas permeability.

次に分離層は、支持層上に形成させ、非多孔質材料からなることが必要である。ここで非多孔質とは、電子顕微鏡で断面あるいは表面に孔が確認されない、直径10nm以上の孔を有さない構造である。分離層は支持層である中空糸膜の外表面側、内表面側のどちらに形成させてもよく、用途、操作性、製膜性を考慮して決めることが好ましい。   Next, the separation layer needs to be formed on the support layer and made of a non-porous material. The term “non-porous” as used herein refers to a structure having no pores having a diameter of 10 nm or more, in which pores are not confirmed on the cross section or surface by an electron microscope. The separation layer may be formed on either the outer surface side or the inner surface side of the hollow fiber membrane that is the support layer, and is preferably determined in consideration of the application, operability, and film forming property.

分離層の素材としては、分離対象とする気体の種類、必要な気体透過性、気体分離性などに応じて種々の有機ポリマー、無機物、それらの混合物などが利用できる。有機ポリマーとしてはポリジメチルシロキサン、ポリメチルビニルシロキサン、ポリメチルフェニルシロキサン、ポリイミドシロキサンなどのポリシロキサン、ポリ−1−トリメチルシリル−2−プロピン、ポリ−1−トリメチルシリル−3−プロピン、ポリ−p−トリメチルシリルフェニルアセチレン、ポリビニルトリメチルシランなどのポリ置換アセチレンおよび有機ケイ素化合物、ポリ−4−メチルペンテン−1、ポリエチレン、ポリプロピレン、ポリブテン−1、ポリビニルクロリド、ポリビニルフルオリド、ポリビニルクロリド、ポリフッ化ビニリデン、ポリビニルアルコール、ポリビニルエステル、ポリビニルアセテート、ポリビニルプロピオネート、ポリビニルピリジン、ポリビニルピロリドン、ポリビニルエーテル、ポリビニルケトン、ポリビニルアルデヒド、ポリビニルホルマール、ポリビニルブチラール、ポリビニルアミド、ポリビニルアミン、ポビニルウレタン、ポリビニルウレア、ポリビニルフォスフェート、ポリビニルスルフェート、ポリイソプレン、ポリアクリル酸およびそのエステル誘導体、ポリメタクリル酸およびそのエステル誘導体などのポリオレフィン、ポリフェニレンオキシド、ポリキシレンオキシド、ポリスチレンおよびその誘導体、メチルセルロース、酢酸セルロース、ニトロセルロース、ポリカーボネート、ポリスルホンなどの炭化水素系樹脂、アリールポリアミド、アリールポリイミドを含むポリアミド、ポリイミド、などがあり、これらの単独重合体でも、共重合体でも、混合物であってもよい。   As the material for the separation layer, various organic polymers, inorganic substances, mixtures thereof, and the like can be used according to the type of gas to be separated, the required gas permeability, gas separation properties, and the like. Examples of organic polymers include polysiloxanes such as polydimethylsiloxane, polymethylvinylsiloxane, polymethylphenylsiloxane, and polyimidesiloxane, poly-1-trimethylsilyl-2-propyne, poly-1-trimethylsilyl-3-propyne, and poly-p-trimethylsilyl. Polyacetylene and organosilicon compounds such as phenylacetylene and polyvinyltrimethylsilane, poly-4-methylpentene-1, polyethylene, polypropylene, polybutene-1, polyvinyl chloride, polyvinyl fluoride, polyvinyl chloride, polyvinylidene fluoride, polyvinyl alcohol, Polyvinyl ester, polyvinyl acetate, polyvinyl propionate, polyvinyl pyridine, polyvinyl pyrrolidone, polyvinyl ether, polyvinyl chloride Luketone, polyvinyl aldehyde, polyvinyl formal, polyvinyl butyral, polyvinyl amide, polyvinyl amine, polyvinyl urethane, polyvinyl urea, polyvinyl phosphate, polyvinyl sulfate, polyisoprene, polyacrylic acid and its ester derivatives, polymethacrylic acid and its ester derivatives Polyolefins such as polyolefin, polyphenylene oxide, polyxylene oxide, polystyrene and its derivatives, hydrocarbon resins such as methyl cellulose, cellulose acetate, nitrocellulose, polycarbonate, polysulfone, aryl polyamide, polyamide including aryl polyimide, polyimide, etc. These homopolymers, copolymers or mixtures may be used.

また分離層の厚みは、欠陥のない層の完全性と気体透過性を考慮して0.05〜100μmが好ましく、より好ましくは0.1〜50μm、さらに好ましくは0.5〜20μmである。   The thickness of the separation layer is preferably 0.05 to 100 μm, more preferably 0.1 to 50 μm, and further preferably 0.5 to 20 μm in consideration of the integrity of the layer having no defect and gas permeability.

次に本発明の複合中空糸膜の製造方法について述べる。   Next, a method for producing the composite hollow fiber membrane of the present invention will be described.

本発明の複合中空糸膜の支持層は球状構造からなることが必要であるが、球状構造は熱誘起相分離法を利用することにより形成させることができる。ここで熱誘起相分離とは、高温で溶解した樹脂溶液を冷却することにより固化せしめる相分離である。   Although the support layer of the composite hollow fiber membrane of the present invention needs to have a spherical structure, the spherical structure can be formed by utilizing a thermally induced phase separation method. Here, thermally induced phase separation is phase separation in which a resin solution dissolved at high temperature is solidified by cooling.

熱誘起相分離法には主に2種類の相分離機構がある。一つは高温時に均一に溶解した樹脂溶液が、降温時に溶液の溶解能力低下が原因で樹脂の濃厚相と希薄相に分離する液−液型、もう一つが高温時に均一に溶解した樹脂溶液が、降温時に樹脂の結晶が起こりポリマー固体相とポリマー希薄溶液相に相分離する固−液型である。おもに前者の機構では三次元網目構造が、後者の機構では球状構造が形成されるため、支持層を形成する際は後者の機構が利用される。固−液型熱誘起相分離を誘起させるためには、適切な溶媒および樹脂濃度を選択することが必要である。   There are mainly two types of phase separation mechanisms in the thermally induced phase separation method. One is a liquid-liquid type in which a resin solution that is uniformly dissolved at a high temperature is separated into a dense phase and a dilute phase due to a decrease in the dissolving ability of the solution when the temperature is lowered, and the other is a resin solution that is uniformly dissolved at a high temperature. In the solid-liquid type, the resin crystallizes when the temperature is lowered, and the phase is separated into a polymer solid phase and a polymer dilute solution phase. Since the former mechanism mainly forms a three-dimensional network structure and the latter mechanism forms a spherical structure, the latter mechanism is used when forming the support layer. In order to induce solid-liquid thermally induced phase separation, it is necessary to select an appropriate solvent and resin concentration.

該溶媒としては、ポリフッ化ビニリデン樹脂の貧溶媒が好ましく、シクロヘキサノン、γ−ブチロラクトン、イソホロン、ジメチルスルホキシド等のアルキルケトン、エステル等の比較的樹脂の溶解度が高い貧溶媒が好ましく、より好ましくはγ−ブチロラクトン、ジメチルスルホキシドである。   The solvent is preferably a poor solvent of polyvinylidene fluoride resin, preferably a poor solvent having relatively high solubility of the resin, such as alkyl ketone, ester such as cyclohexanone, γ-butyrolactone, isophorone, dimethyl sulfoxide, and more preferably γ- Butyrolactone and dimethyl sulfoxide.

樹脂溶液中の樹脂濃度は、高いほど一次核を形成しやすく、結果的に球状構造の平均直径が小さくなる傾向にある。球状構造の平均直径を0.1μm以上2.0μm以下にするためには、30〜60重量%にすることが好ましい。   As the resin concentration in the resin solution is higher, primary nuclei are more likely to be formed, and as a result, the average diameter of the spherical structure tends to be smaller. In order to make the average diameter of the spherical structure 0.1 μm or more and 2.0 μm or less, it is preferably 30 to 60% by weight.

このような組成で仕込み、高温で溶解した樹脂溶液を、二重管式口金の環状口から吐出した後、樹脂溶液の結晶化温度Tc以下に冷却し凝固させる前に、Tc+20℃以上Tc+55℃以下の温度で0.5分以上10分以下保持することが必要である。低い温度で長い時間保持することで、球状構造の一次核の生成数が増え、結果的に球状構造の平均直径が小さくなる。ここで樹脂溶液の結晶化温度Tcとは、示差走査熱量測定(DSC測定)装置を用いて、樹脂と溶媒など樹脂溶液と同組成の混合物を密封式DSC容器に密封し、昇温速度10℃/minで溶解温度まで昇温し30分保持して均一に溶解した後に、降温速度10℃/minで降温する過程で観察される結晶化ピークの立ち上がり温度とする。   The resin solution charged with such a composition and melted at a high temperature is discharged from the annular port of the double-tube type die, and then cooled to below the crystallization temperature Tc of the resin solution and solidified before Tc + 20 ° C. or more and Tc + 55 ° C. or less It is necessary to hold at a temperature of 0.5 to 10 minutes. By maintaining at a low temperature for a long time, the number of primary nuclei generated in the spherical structure increases, and as a result, the average diameter of the spherical structure decreases. Here, the crystallization temperature Tc of the resin solution means that a mixture having the same composition as the resin solution, such as resin and solvent, is sealed in a sealed DSC container using a differential scanning calorimetry (DSC measurement) device, and the temperature rising rate is 10 ° C. The temperature is raised to the dissolution temperature at / min and held for 30 minutes to dissolve uniformly, and then set to the rising temperature of the crystallization peak observed in the process of lowering the temperature at a temperature drop rate of 10 ° C./min.

Tc+55℃より高い温度、または0.5分未満では球状構造の直径が2μm以下になりにくく、Tc+20℃より低い温度、または10分を超えると、樹脂溶液の粘度が高くなりすぎて、曳糸性がなくなり中空糸膜を形成できなくなったりする。   When the temperature is higher than Tc + 55 ° C. or less than 0.5 minutes, the diameter of the spherical structure is difficult to be 2 μm or less, and when the temperature is lower than Tc + 20 ° C. or more than 10 minutes, the viscosity of the resin solution becomes too high, and the spinnability The hollow fiber membrane cannot be formed.

次に吐出した溶液を冷却する際は、冷却浴を用いることが好ましく、支持層の樹脂溶液の溶媒と支持層の樹脂の非溶媒の混合溶媒が好ましい。この際、支持層の外表面側に分離層を形成させる場合、支持層の外表面を緻密な構造にするため、冷却浴の混合溶媒中の支持層の樹脂の非溶媒濃度を高くすることが好ましい。   Next, when cooling the discharged solution, it is preferable to use a cooling bath, and a mixed solvent of a solvent of the resin solution of the support layer and a non-solvent of the resin of the support layer is preferable. In this case, when the separation layer is formed on the outer surface side of the support layer, the non-solvent concentration of the resin of the support layer in the mixed solvent of the cooling bath may be increased in order to make the outer surface of the support layer a dense structure. preferable.

例えばポリフッ化ビニリデン樹脂の非溶媒としては、水、ヘキサン、ペンタン、ベンゼン、トルエン、メタノール、エタノール、四塩化炭素、o−ジクロルベンゼン、トリクロルエチレン、エチレングリコール、ジエチレングリコール、トリエチレングリコール、プロピレングリコール、ブチレングリコール、ペンタンジオール、ヘキサンジオール、低分子量のポリエチレングリコール等の脂肪族炭化水素、芳香族炭化水素、脂肪族多価アルコール、芳香族多価アルコール、塩素化炭化水素、またはその他の塩素化有機液体およびその混合溶媒等が挙げられる。   For example, as a non-solvent for polyvinylidene fluoride resin, water, hexane, pentane, benzene, toluene, methanol, ethanol, carbon tetrachloride, o-dichlorobenzene, trichloroethylene, ethylene glycol, diethylene glycol, triethylene glycol, propylene glycol, Aliphatic hydrocarbons such as butylene glycol, pentanediol, hexanediol, low molecular weight polyethylene glycol, aromatic hydrocarbons, aliphatic polyhydric alcohols, aromatic polyhydric alcohols, chlorinated hydrocarbons, or other chlorinated organic liquids And mixed solvents thereof.

また二重管式口金の中心の管からも、支持層溶液の溶媒と支持層の樹脂の非溶媒の混合溶媒を吐出させることが好ましい。この際、冷却浴と同様に、支持層の内表面側に分離層を形成させる場合、支持層の内表面を緻密な構造にするため、混合溶媒中の支持層の樹脂の非溶媒濃度を高くすることが好ましい。   Further, it is preferable that a mixed solvent of the solvent of the support layer solution and the non-solvent of the resin of the support layer is also discharged from the central tube of the double tube type die. At this time, as with the cooling bath, when the separation layer is formed on the inner surface side of the support layer, the non-solvent concentration of the resin of the support layer in the mixed solvent is increased in order to make the inner surface of the support layer a dense structure. It is preferable to do.

支持層の分離層側を形成する球状構造の平均直径D1と支持層の分離層と反対側を形成する球状構造の平均直径D2が、D1<D2の関係を満たす構造にする方法としては、2つの樹脂溶液を用い、支持層を二層構造にする方法が好ましい。この際、二層構造を同時に形成させる方法と、順に形成させる方法がある。   As a method of making the structure in which the average diameter D1 of the spherical structure forming the separation layer side of the support layer and the average diameter D2 of the spherical structure forming the opposite side of the separation layer of the support layer satisfy the relationship of D1 <D2, 2 A method of using two resin solutions and making the support layer into a two-layer structure is preferable. At this time, there are a method of simultaneously forming a two-layer structure and a method of sequentially forming them.

前者としては、三重管式口金を用いた複合紡糸法、後者としては一つの樹脂溶液で中空糸膜を形成した後、他方の樹脂溶液に浸漬後ノズルなどに通して掻き取り形成させる方法、あるいは他方の樹脂溶液をスプレーコーティングする方法などである。二層を形成する樹脂溶液がともに高粘度であり、また二層間の接着性を高める観点から、三重管式口金を用いた複合紡糸法のように同時に形成させる方法がより好ましく用いられる。すなわち三重管式口金の外側と内側の2つの環状口から2つの樹脂溶液を吐出する方法である。   The former is a compound spinning method using a triple tube type die, the latter is a method in which a hollow fiber membrane is formed with one resin solution and then immersed in the other resin solution and then scraped through a nozzle or the like, or For example, the other resin solution may be spray coated. From the viewpoint of increasing the viscosity of both the resin solutions forming the two layers and improving the adhesion between the two layers, a method of forming simultaneously such as a composite spinning method using a triple tube die is more preferably used. That is, it is a method of discharging two resin solutions from the two annular ports on the outer side and the inner side of the triple tube type die.

球状構造の平均直径は、前記した通り、おもに樹脂溶液中の樹脂濃度、樹脂溶液を凝固させる前の保持温度と保持時間によって制御できるので、2つの樹脂溶液をそれぞれに適切な条件に設定することが必要である。   As described above, the average diameter of the spherical structure can be controlled mainly by the resin concentration in the resin solution, the holding temperature and the holding time before the resin solution is solidified, so the two resin solutions should be set to appropriate conditions for each. is required.

また支持層の分離層側が三次元網目構造からなり、支持層の分離層と反対側が球状構造からなる構造にする場合も同様に、2つの樹脂溶液を用い、支持層を二層構造にする方法が好ましい。三次元網目構造を形成する樹脂溶液は比較的樹脂濃度が低いため、前記した、二層を同時に形成させる方法と、順に形成させる方法がともに好ましく採用される。分離層側の表面に緻密な構造を有する三次元網目構造を形成させるためには、非溶媒誘起相分離法を利用することができる。ここで非溶媒誘起相分離とは、樹脂溶液を非溶媒に接触させることにより固化せしめる相分離である。   Similarly, when the separation layer side of the support layer has a three-dimensional network structure and the opposite side of the support layer has a spherical structure, similarly, a method of using two resin solutions and making the support layer a two-layer structure Is preferred. Since the resin solution that forms the three-dimensional network structure has a relatively low resin concentration, both the method of forming the two layers simultaneously and the method of forming them in order are preferably employed. In order to form a three-dimensional network structure having a dense structure on the surface on the separation layer side, a non-solvent induced phase separation method can be used. Here, the non-solvent induced phase separation is phase separation in which a resin solution is solidified by contacting with a non-solvent.

非溶媒誘起相分離法を利用する場合、樹脂溶液の溶媒としては、樹脂の良溶媒が好ましく、例えばポリフッ化ビニリデン樹脂の良溶媒としては、N−メチル−2−ピロリドン、ジメチルアセトアミド、ジメチルホルムアミド、メチルエチルケトン、アセトン、テトラヒドロフラン等の低級アルキルケトン、エステル、アミド等およびその混合溶媒が挙げられる。このように三次元網目構造と球状構造は、形成する際に利用する相分離機構が異なるため、特に同時に形成させる方法では、冷却浴および口金の中心の管から吐出する溶媒中の樹脂の非溶媒濃度、あるいは三次元網目構造と球状構造の二層の厚さを適切に調整する。   When the non-solvent induced phase separation method is used, the resin solvent is preferably a resin good solvent. For example, the polyvinylidene fluoride resin good solvent includes N-methyl-2-pyrrolidone, dimethylacetamide, dimethylformamide, Examples thereof include lower alkyl ketones such as methyl ethyl ketone, acetone and tetrahydrofuran, esters, amides and the like, and mixed solvents thereof. Thus, the three-dimensional network structure and the spherical structure are different in the phase separation mechanism used when forming, so in the method of forming at the same time, the non-solvent of the resin in the solvent discharged from the cooling bath and the central tube of the base The concentration or the thickness of the two layers of the three-dimensional network structure and the spherical structure are adjusted appropriately.

このようにして製造された支持層は、球状構造間の空隙を拡大し気体透過性を向上させるおよび破断強度を強化させるなどのために、延伸してもよい。さらに溶媒または非溶媒で湿潤しているため、水などの低沸点の樹脂の非溶媒で洗浄後、乾燥することが好ましく採用される。   The support layer thus produced may be stretched in order to enlarge the gap between the spherical structures, improve the gas permeability and strengthen the breaking strength. Furthermore, since it is wet with a solvent or a non-solvent, it is preferably employed after washing with a non-solvent of a low boiling point resin such as water and then drying.

その後、本発明では支持層を、100℃以上支持層の融点未満の温度で熱処理し、支持層の長さ方向に収縮率10%以上30%以下で収縮させることが好ましい。ここで支持層の融点は、乾燥状態の支持層をDSC測定装置を用いて、速度10℃/minで昇温させたときに現れる、もっとも低い吸熱ピークのピークトップの温度である。ポリフッ化ビニリデンからなる中空糸膜の場合170℃付近である。球状構造からなる支持層にこのような処理を行うことにより、球状の固形部が優先的に収縮し、固形部間の大きな空隙はほとんど収縮しないために、支持層の気体透過性は維持しつつ、破断強伸度が著しく向上し、また処理温度以下での熱収縮が著しく抑制される。   Thereafter, in the present invention, the support layer is preferably heat-treated at a temperature of 100 ° C. or higher and lower than the melting point of the support layer, and contracted in the length direction of the support layer at a contraction rate of 10% or more and 30% or less. Here, the melting point of the support layer is the peak top temperature of the lowest endothermic peak that appears when the dried support layer is heated at a rate of 10 ° C./min using a DSC measuring apparatus. In the case of a hollow fiber membrane made of polyvinylidene fluoride, the temperature is around 170 ° C. By carrying out such a treatment on the support layer having a spherical structure, the spherical solid portions shrink preferentially, and the large gaps between the solid portions hardly shrink, so that the gas permeability of the support layer is maintained. Further, the breaking strength and elongation are remarkably improved, and the heat shrinkage below the processing temperature is remarkably suppressed.

次に分離層を形成させる方法について述べる。   Next, a method for forming the separation layer will be described.

分離層は支持膜の外表面側あるいは内表面側に形成させる。外表面側に形成させる方法としては、支持層を分離層を形成する樹脂あるいはモノマーの溶液中に浸漬し、その後乾燥あるいは架橋、重合させる方法、あるいはプラズマ蒸着およびそれに関連する方法も利用できる。内表面側に形成させる方法は、通常の例に倣って支持層の中空糸膜モジュールを形成した後、モジュールの一端側から他端側に、分離層を形成する樹脂あるいはモノマーの溶液を注入後、乾燥あるいは架橋、重合させる方法などが利用できる。   The separation layer is formed on the outer surface side or the inner surface side of the support membrane. As a method for forming on the outer surface side, a method in which the support layer is immersed in a solution of a resin or a monomer for forming a separation layer and then dried, crosslinked, polymerized, or plasma deposition and a related method can be used. The method of forming on the inner surface side is that after forming a hollow fiber membrane module of a support layer according to a normal example, and then injecting a solution of a resin or monomer that forms a separation layer from one end side to the other end side of the module A method of drying, crosslinking, polymerizing, or the like can be used.

以下に具体的な実施例を挙げて本発明を説明するが、本発明はこれら実施例により何ら限定されるものではない。ここで本発明に関連するパラメーターは以下の方法で測定した。   Hereinafter, the present invention will be described with reference to specific examples, but the present invention is not limited to these examples. Here, parameters related to the present invention were measured by the following methods.

(1)支持層の分離層側の界面から支持層方向に深さ5μmの位置の空隙の大きさ
図1の模式図を用いて説明する。支持層2の長手方向に垂直な断面を電子顕微鏡を用いて、3000倍で、支持層2の分離層1側の界面3が写真の対向する辺のそれぞれに含まれるように20μm四方の写真を撮影する。次に写真中で、支持層2の分離層1側の界面3の写真の両端、すなわち界面3を形成する固形部の写真の両端の二点(A,C)からそれぞれ深さ方向(分離層1とは反対の方向)に5μmの距離にある二点(B、D)をとり、その二点(B、D)を結ぶ直線を引く。その直線中で空隙4を通る部分(線分)の長さを、支持層2の分離層1側の界面3から深さ5μmの位置の空隙の大きさ5とする。ここで2つの固形部が写真の奥行き方向に重なり合っている場合、写真奥の固形部は無視する。任意の12箇所の写真において、同様に空隙の大きさを測定し、すべての箇所のすべての空隙の大きさが2μm以下である(○)か、否(×)かを判定する。
(1) The size of the void at a depth of 5 μm from the interface on the separation layer side of the support layer in the direction of the support layer. Using a electron microscope, the cross section perpendicular to the longitudinal direction of the support layer 2 is 3000 times, and a 20 μm square photograph is included so that the interface 3 on the separation layer 1 side of the support layer 2 is included in each of the opposite sides of the photograph. Take a picture. Next, in the photograph, both ends of the photograph of the interface 3 on the separation layer 1 side of the support layer 2, that is, two points (A, C) on both ends of the photograph of the solid portion forming the interface 3, respectively, in the depth direction (separation layer). Take two points (B, D) at a distance of 5 μm in the direction opposite to 1) and draw a straight line connecting the two points (B, D). The length of the portion (line segment) passing through the gap 4 in the straight line is the size 5 of the gap at a depth of 5 μm from the interface 3 on the separation layer 1 side of the support layer 2. Here, when two solid parts overlap in the depth direction of the photograph, the solid part at the back of the photograph is ignored. In any 12 photographs, the size of the void is measured in the same manner, and it is determined whether the size of all the voids in all the locations is 2 μm or less (◯) or not (×).

(2)支持層の分離層側を形成する球状構造の平均直径D1と支持層の分離層と反対側を形成する球状構造の平均直径D2
支持層の長手方向に垂直な断面を電子顕微鏡を用いて、3000〜6000倍で、支持層の分離層側の界面から支持層方向の深さ(分離層とは反対の方向)に10μmの距離にある任意の1点を中心として、10μm四方の写真を撮影する。該写真中の球状構造の平均直径をD1とする。次に支持層の長手方向に垂直な断面を電子顕微鏡を用いて、3000〜6000倍で、支持層の分離層と反対側の表面(さらに層が設けられている場合は界面となる)から深さ方向(分離層の方向)に10μmの距離にある任意の1点を中心として、10μm四方の写真を撮影する。該写真中の球状構造の平均直径をD2とする。

(3)中空糸膜の破断強度、破断伸度
引張試験機((株)東洋ボールドウィン製TENSILON/RTM100)を用いて、中空糸膜を試験長50mm、フルスケール5kgの加重でクロスヘッドスピード50mm/分にて測定し求めた。
(2) The average diameter D1 of the spherical structure forming the separation layer side of the support layer and the average diameter D2 of the spherical structure forming the opposite side of the support layer from the separation layer
The cross section perpendicular to the longitudinal direction of the support layer is 3000 to 6000 times using an electron microscope, and the distance of 10 μm from the interface of the support layer on the separation layer side to the depth in the support layer direction (the direction opposite to the separation layer) A photograph of 10 μm square is taken centering on an arbitrary point in the area. The average diameter of the spherical structure in the photograph is D1. Next, the cross section perpendicular to the longitudinal direction of the support layer is 3000 to 6000 times using an electron microscope, and is deep from the surface of the support layer on the side opposite to the separation layer (or an interface if further layers are provided). A photograph of 10 μm square is taken around an arbitrary point at a distance of 10 μm in the vertical direction (direction of the separation layer). The average diameter of the spherical structure in the photograph is D2.

(3) Breaking strength and breaking elongation of hollow fiber membrane Using a tensile tester (TENSILON / RTM100 manufactured by Toyo Baldwin Co., Ltd.), the hollow fiber membrane was tested with a test length of 50 mm and a full-scale load of 5 kg and a crosshead speed of 50 mm / Measured in minutes.

(4)中空糸膜の気体透過性
長さ約20cmの4本の中空糸膜を束ねてガラス製のミニモジュールに挿入し、両端をエポキシ樹脂でポッティングし、試験用膜モジュールを作製した。気体として酸素ガスを用いて、中空糸膜の分離層側から高圧をかけたとき、中空糸膜の支持層側に透過してくる気体の体積(単位はcmであり、透過量は25℃、1気圧を標準として換算)を測定時間(sec)、中空糸膜の両側の気体の圧力差(cmHg)、膜の表面積(cm)、および膜の厚さ(cm)で規格化して求めた。
(4) Gas permeability of hollow fiber membrane Four hollow fiber membranes having a length of about 20 cm were bundled and inserted into a glass mini-module, and both ends were potted with an epoxy resin to prepare a test membrane module. When oxygen gas is used as the gas and a high pressure is applied from the separation layer side of the hollow fiber membrane, the volume of the gas permeating to the support layer side of the hollow fiber membrane (unit is cm 3 , the permeation amount is 25 ° C. 1 atmospheric pressure as a standard) is obtained by standardizing the measurement time (sec), the pressure difference (cmHg) of the gas on both sides of the hollow fiber membrane, the membrane surface area (cm 2 ), and the membrane thickness (cm). It was.

(5)中空糸膜の熱収縮率
乾燥した中空糸膜を、無張力状態で100℃の乾燥機中に10分保持(熱処理)し、次式に従い熱収縮率を求める。
(5) Heat Shrinkage Ratio of Hollow Fiber Membrane The dried hollow fiber membrane is held (heat treated) for 10 minutes in a dryer at 100 ° C. in a tensionless state, and the heat shrinkage rate is obtained according to the following formula.

熱収縮率(%)=(初期試料長−熱処理後試料長)/初期試料長×100
(実施例1)
重量平均分子量41.7万のフッ化ビニリデンホモポリマー36重量%とジメチルスルホキシド64重量%を130℃で溶解した。この樹脂溶液(Tc:32℃)を63℃で1.9分保持した後、二重管式口金の外側の環状口から吐出し、同時にジメチルスルホキシド60重量%の水溶液を二重管式口金の中心の管から吐出し、ジメチルスルホキシド85重量%の水溶液からなる温度10℃の浴中で固化させた後、水洗した。得られた支持層は球状構造からなり、支持層の融点は170℃であった。その後、回転速度が8m/分と7.6m/分の二つの駆動ロール間で、熱風により雰囲気を120℃にした乾熱雰囲気中を通過させて、中空糸膜の長さ方向に収縮率5%で収縮させた。
Thermal shrinkage (%) = (initial sample length−sample length after heat treatment) / initial sample length × 100
(Example 1)
36% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 64% by weight of dimethyl sulfoxide were dissolved at 130 ° C. This resin solution (Tc: 32 ° C.) was held at 63 ° C. for 1.9 minutes, and then discharged from the outer annular port of the double-tube die. At the same time, an aqueous solution of 60% by weight of dimethyl sulfoxide was added to the double-tube die. The mixture was discharged from the central tube, solidified in a bath composed of an aqueous solution of 85% by weight of dimethyl sulfoxide, and then washed with water. The obtained support layer had a spherical structure, and the melting point of the support layer was 170 ° C. After that, it is passed between two drive rolls with rotational speeds of 8 m / min and 7.6 m / min through a dry heat atmosphere in which the atmosphere is 120 ° C. with hot air, and the shrinkage rate is 5 in the length direction of the hollow fiber membrane. %.

得られた支持層8本を束ねてガラス製のミニモジュールに挿入し、両端をエポキシ樹脂でポッティングした。この支持層の中空部に、ポリジメチルシロキサンを主成分とする室温硬化型シリコーンポリマーの10重量%シクロヘキサン溶液を通液させた後、空気を通気し余分なシリコーンポリマーを除去して、支持層の内表面側に硬化薄膜を形成させた。   The obtained eight support layers were bundled and inserted into a glass mini-module, and both ends were potted with an epoxy resin. After passing a 10% by weight cyclohexane solution of a room temperature curable silicone polymer containing polydimethylsiloxane as a main component into the hollow portion of the support layer, the excess silicone polymer was removed by ventilating the air. A cured thin film was formed on the inner surface side.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

(実施例2)
重量平均分子量41.7万のフッ化ビニリデンホモポリマー38重量%とγ−ブチロラクトン62重量%を150℃で溶解した。この樹脂溶液(Tc:51℃)を97℃で0.7分保持した後、二重管式口金の外側の環状口から吐出し、同時にγ−ブチロラクトン75重量%の水溶液を二重管式口金の中心の管から吐出し、γ−ブチロラクトン85重量%の水溶液からなる温度5℃の浴中で固化させた後、水洗して90℃の水中で1.4倍に延伸した。得られた支持層は球状構造からなり、支持層の融点は173℃であった。その後、回転速度が8m/分と6.6m/分の二つの駆動ロール間で、熱風により雰囲気を160℃にした乾熱雰囲気中を通過させて、中空糸膜の長さ方向に収縮率17%で収縮させた。
(Example 2)
38% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 62% by weight of γ-butyrolactone were dissolved at 150 ° C. After this resin solution (Tc: 51 ° C.) was held at 97 ° C. for 0.7 minutes, it was discharged from the outer annular port of the double tube die, and at the same time, an aqueous solution of 75% by weight of γ-butyrolactone was added to the double tube die. The mixture was discharged from the center tube, solidified in a 5 ° C. bath composed of an 85% by weight aqueous solution of γ-butyrolactone, washed with water, and stretched 1.4 times in 90 ° C. water. The obtained support layer had a spherical structure, and the melting point of the support layer was 173 ° C. After that, it is passed between two drive rolls with rotational speeds of 8 m / min and 6.6 m / min through a dry heat atmosphere with an atmosphere of 160 ° C. by hot air, and the shrinkage rate is 17 in the length direction of the hollow fiber membrane. %.

薄膜は実施例1と同様にして形成させた。   The thin film was formed in the same manner as in Example 1.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

(実施例3)
重量平均分子量41.7万のフッ化ビニリデンホモポリマー40重量%とγ−ブチロラクトン60重量%を150℃で溶解した。この樹脂溶液(Tc:55℃)を90℃で2.3分保持した後、二重管式口金の外側の環状口から吐出し、同時にγ−ブチロラクトン85重量%の水溶液を二重管式口金の中心の管から吐出し、γ−ブチロラクトン85重量%の水溶液からなる温度5℃の浴中で固化させた後、水洗して90℃の水中で1.2倍に延伸した。得られた支持層は球状構造からなり、支持層の融点は173℃であった。その後、回転速度が8m/分と7.4m/分の二つの駆動ロール間で、熱風により雰囲気を120℃にした乾熱雰囲気中を通過させて、中空糸膜の長さ方向に収縮率7%で収縮させた。
(Example 3)
40% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 60% by weight of γ-butyrolactone were dissolved at 150 ° C. After holding this resin solution (Tc: 55 ° C.) at 90 ° C. for 2.3 minutes, the resin solution (Tc: 55 ° C.) is discharged from the outer annular port of the double tube die, and at the same time, an aqueous solution of 85% by weight of γ-butyrolactone is added to the double tube die. After being discharged from the central tube of the tube and solidified in a bath at a temperature of 5 ° C. consisting of an aqueous solution of 85% by weight of γ-butyrolactone, it was washed with water and stretched 1.2 times in 90 ° C. water. The obtained support layer had a spherical structure, and the melting point of the support layer was 173 ° C. After that, it is passed between two drive rolls with rotational speeds of 8 m / min and 7.4 m / min through a dry heat atmosphere in which the atmosphere is 120 ° C. with hot air, and the shrinkage rate is 7 in the length direction of the hollow fiber membrane. %.

薄膜は実施例1と同様にして形成させた。   The thin film was formed in the same manner as in Example 1.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

(実施例4)
重量平均分子量41.7万のフッ化ビニリデンホモポリマー34重量%とジメチルスルホキシド66重量%を130℃で溶解し樹脂溶液1とした。また重量平均分子量41.7万のフッ化ビニリデンホモポリマー37重量%とジメチルスルホキシド63重量%を130℃で溶解し樹脂溶液2とした。この樹脂溶液1(Tc:28℃)を58℃で1.6分保持した後、三重管式口金の外側の環状口から吐出し、同時に樹脂溶液2(Tc:34℃)を62℃で2.1分保持した後、三重管式口金の内側の環状口から吐出し、さらにジメチルスルホキシド60重量%の水溶液を三重管式口金の中心の管から吐出し、ジメチルスルホキシド85重量%の水溶液からなる温度10℃の浴中で固化させた後、水洗した。得られた支持層は球状構造からなり、支持層の融点は170℃であった。その後、回転速度が8m/分と7.6m/分の二つの駆動ロール間で、熱風により雰囲気を120℃にした乾熱雰囲気中を通過させて、中空糸膜の長さ方向に収縮率5%で収縮させた。
Example 4
A resin solution 1 was prepared by dissolving 34% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 66% by weight of dimethyl sulfoxide at 130 ° C. Further, 37% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 63% by weight of dimethyl sulfoxide were dissolved at 130 ° C. to obtain Resin Solution 2. After this resin solution 1 (Tc: 28 ° C.) was held at 58 ° C. for 1.6 minutes, it was discharged from the outer annular port of the triple tube die, and at the same time, the resin solution 2 (Tc: 34 ° C.) was 2 at 62 ° C. After holding for 1 minute, it is discharged from the inner ring opening of the triple tube type die, and further 60% by weight of dimethyl sulfoxide aqueous solution is discharged from the central tube of the triple tube type die, and consists of 85% by weight aqueous solution of dimethyl sulfoxide. After solidifying in a bath at a temperature of 10 ° C., it was washed with water. The obtained support layer had a spherical structure, and the melting point of the support layer was 170 ° C. After that, it is passed between two drive rolls with rotational speeds of 8 m / min and 7.6 m / min through a dry heat atmosphere in which the atmosphere is 120 ° C. with hot air, and the shrinkage rate is 5 in the length direction of the hollow fiber membrane. %.

薄膜は実施例1と同様にして形成させた。   The thin film was formed in the same manner as in Example 1.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

(実施例5)
重量平均分子量41.7万のフッ化ビニリデンホモポリマー38重量%とγ−ブチロラクトン62重量%を150℃で溶解し樹脂溶液1とした。また重量平均分子量41.7万のフッ化ビニリデンホモポリマー40重量%とγ−ブチロラクトン60重量%を150℃で溶解し樹脂溶液2とした。この樹脂溶液1(Tc:51℃)を99℃で0.6分保持した後、三重管式口金の外側の環状口から吐出し、同時に樹脂溶液2(Tc:55℃)を94℃で1.5分保持した後、三重管式口金の内側の環状口から吐出し、さらにγ−ブチロラクトン85重量%の水溶液を三重管式口金の中心の管から吐出し、γ−ブチロラクトン85重量%の水溶液からなる温度5℃の浴中で固化させた後、水洗して90℃の水中で1.4倍に延伸した。得られた支持層は球状構造からなり、支持層の融点は170℃であった。その後、回転速度が8m/分と6.9m/分の二つの駆動ロール間で、熱風により雰囲気を150℃にした乾熱雰囲気中を通過させて、中空糸膜の長さ方向に収縮率14%で収縮させた。
(Example 5)
A resin solution 1 was prepared by dissolving 38% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 62% by weight of γ-butyrolactone at 150 ° C. Further, 40% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 60% by weight of γ-butyrolactone were dissolved at 150 ° C. to obtain a resin solution 2. After this resin solution 1 (Tc: 51 ° C.) was held at 99 ° C. for 0.6 minutes, it was discharged from the annular port outside the triple tube die, and at the same time, the resin solution 2 (Tc: 55 ° C.) was 1 at 94 ° C. After holding for 5 minutes, it was discharged from the inner annular port of the triple tube type die, and an aqueous solution of 85% by weight of γ-butyrolactone was further discharged from the tube at the center of the triple tube type die to obtain an aqueous solution of 85% by weight of γ-butyrolactone. After solidifying in a bath at a temperature of 5 ° C., it was washed with water and stretched 1.4 times in 90 ° C. water. The obtained support layer had a spherical structure, and the melting point of the support layer was 170 ° C. After that, it is passed between two drive rolls with a rotational speed of 8 m / min and 6.9 m / min through a dry heat atmosphere in which the atmosphere is set to 150 ° C. with hot air, and the shrinkage ratio is 14 in the length direction of the hollow fiber membrane. %.

薄膜は実施例1と同様にして形成させた。   The thin film was formed in the same manner as in Example 1.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

(実施例6)
重量平均分子量41.7万のフッ化ビニリデンホモポリマー38重量%とγ−ブチロラクトン62重量%を150℃で溶解し樹脂溶液1とした。また重量平均分子量41.7万のフッ化ビニリデンホモポリマー40重量%とγ−ブチロラクトン60重量%を150℃で溶解し樹脂溶液2とした。この樹脂溶液1(Tc:51℃)を96℃で1.1分保持した後、三重管式口金の外側の環状口から吐出し、同時に樹脂溶液2(Tc:55℃)を90℃で3.2分保持した後、三重管式口金の内側の環状口から吐出し、さらにγ−ブチロラクトン85重量%の水溶液を三重管式口金の中心の管から吐出し、γ−ブチロラクトン85重量%の水溶液からなる温度5℃の浴中で固化させた後、水洗して90℃の水中で1.1倍に延伸した。得られた支持層は球状構造からなり、支持層の融点は172℃であった。その後、回転速度が8m/分と7.4m/分の二つの駆動ロール間で、熱風により雰囲気を120℃にした乾熱雰囲気中を通過させて、中空糸膜の長さ方向に収縮率7%で収縮させた。
(Example 6)
A resin solution 1 was prepared by dissolving 38% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 62% by weight of γ-butyrolactone at 150 ° C. Further, 40% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 60% by weight of γ-butyrolactone were dissolved at 150 ° C. to obtain a resin solution 2. The resin solution 1 (Tc: 51 ° C.) was held at 96 ° C. for 1.1 minutes, and then discharged from the annular port outside the triple tube die. At the same time, the resin solution 2 (Tc: 55 ° C.) was added at 90 ° C. for 3 minutes. After holding for 2 minutes, it was discharged from the inner annular port of the triple tube die, and an 85% by weight aqueous solution of γ-butyrolactone was discharged from the tube at the center of the triple tube die, and an 85% by weight aqueous solution of γ-butyrolactone was discharged. After solidifying in a bath at a temperature of 5 ° C., it was washed with water and stretched 1.1 times in water at 90 ° C. The obtained support layer had a spherical structure, and the melting point of the support layer was 172 ° C. After that, it is passed between two drive rolls with rotational speeds of 8 m / min and 7.4 m / min through a dry heat atmosphere in which the atmosphere is 120 ° C. with hot air, and the shrinkage rate is 7 in the length direction of the hollow fiber membrane. %.

薄膜は実施例1と同様にして形成させた。   The thin film was formed in the same manner as in Example 1.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

(実施例7)
球状構造からなる支持層を実施例1で三重管式口金の中心の管からジメチルスルホキシド85重量%の水溶液を吐出して得た。
(Example 7)
A support layer having a spherical structure was obtained in Example 1 by discharging an aqueous solution of 85% by weight of dimethyl sulfoxide from the central tube of the triple tube die.

該支持層に、重量平均分子量28.4万のフッ化ビニリデンホモポリマー13重量%、重量平均分子量2万のポリエチレングリコール5重量%、およびジメチルホルムアミド82重量%を溶解した溶液中に浸漬し、シリコーン樹脂製のノズルを用いて余分な溶液を掻き取り、水凝固し乾燥させた。得られた支持層は三次元網目構造と球状構造からなり、支持層の融点は168℃であった。   The support layer was immersed in a solution in which 13% by weight of a vinylidene fluoride homopolymer having a weight average molecular weight of 2840, 5% by weight of polyethylene glycol having a weight average molecular weight of 20,000, and 82% by weight of dimethylformamide were dissolved. The excess solution was scraped off using a resin nozzle, water-coagulated and dried. The obtained support layer had a three-dimensional network structure and a spherical structure, and the melting point of the support layer was 168 ° C.

得られた支持層をポリジメチルシロキサンを主成分とする室温硬化型シリコーンポリマーの10重量%シクロヘキサン溶液中に浸漬し、シリコーン樹脂製のノズルを用いて余分な溶液を掻き取り、乾燥させて支持層の外表面側に硬化薄膜を形成させた。   The obtained support layer was immersed in a 10% by weight cyclohexane solution of a room temperature curable silicone polymer mainly composed of polydimethylsiloxane, and the excess solution was scraped off using a silicone resin nozzle and dried. A cured thin film was formed on the outer surface side of the film.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

(実施例8)
球状構造からなる支持層を、実施例2で三重管式口金の中心の管からγ−ブチロラクトン85重量%の水溶液を吐出して得た以外は、実施例7と同様にして支持層が三次元網目構造と球状構造からなる複合中空糸膜を得た。
(Example 8)
The support layer is three-dimensional in the same manner as in Example 7, except that a support layer having a spherical structure was obtained in Example 2 by discharging an aqueous solution of 85% by weight of γ-butyrolactone from the tube at the center of the triple tube die. A composite hollow fiber membrane having a network structure and a spherical structure was obtained.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

(実施例9)
球状構造からなる支持層を、実施例3と同様にして得た以外は、実施例7と同様にして支持層が三次元網目構造と球状構造からなる複合中空糸膜を得た。
Example 9
A composite hollow fiber membrane in which the support layer has a three-dimensional network structure and a spherical structure was obtained in the same manner as in Example 7, except that the support layer having a spherical structure was obtained in the same manner as in Example 3.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

(比較例1)
重量平均分子量41.7万のフッ化ビニリデンホモポリマー32重量%とジメチルスルホキシド68重量%を130℃で溶解した。この樹脂溶液(Tc:26℃)を85℃で0.2分保持した後、二重管式口金の外側の環状口から吐出し、同時にジメチルスルホキシド85重量%の水溶液を二重管式口金の中心の管から吐出し、ジメチルスルホキシド85重量%の水溶液からなる温度10℃の浴中で固化させた後、水洗し乾燥させた。得られた支持層は球状構造であった。
(Comparative Example 1)
32% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 68% by weight of dimethyl sulfoxide were dissolved at 130 ° C. After holding this resin solution (Tc: 26 ° C.) at 85 ° C. for 0.2 minutes, the resin solution was discharged from the outer annular port of the double tube die, and at the same time, an aqueous solution of 85% by weight of dimethyl sulfoxide was added to the double tube die. The mixture was discharged from the central tube, solidified in a bath composed of an aqueous solution of 85% by weight of dimethyl sulfoxide at a temperature of 10 ° C., washed with water and dried. The obtained support layer had a spherical structure.

薄膜は実施例1と同様にして形成させた。   The thin film was formed in the same manner as in Example 1.

得られた複合中空糸膜の構造と性能を表1に示す。   Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

樹脂溶液を二重管式口金の外側の環状口から吐出する前の、保持温度が高く、保持時間が短かかったため、支持層の球状構造の平均直径が2μmより大きくなり、破断強伸度が低く、また中空糸膜の内表面に薄膜が均一に形成されておらず、球状構造がむき出しの部分がみられた。   Since the holding temperature before discharging the resin solution from the outer annular port of the double-tube type die was high and the holding time was short, the average diameter of the spherical structure of the support layer was larger than 2 μm, and the elongation at break was high. The thin film was not formed uniformly on the inner surface of the hollow fiber membrane, and the exposed portion of the spherical structure was observed.

(比較例2)
重量平均分子量41.7万のフッ化ビニリデンホモポリマー40重量%とγ−ブチロラクトン60重量%を150℃で溶解し樹脂溶液1とした。また重量平均分子量41.7万のフッ化ビニリデンホモポリマー36重量%とγ−ブチロラクトン64重量%を150℃で溶解し樹脂溶液2とした。この樹脂溶液1(Tc:55℃)を90℃で2.3分保持した後、三重管式口金の外側の環状口から吐出し、同時に樹脂溶液2(Tc:48℃)を115℃で0.1分保持した後、三重管式口金の内側の環状口から吐出し、さらにγ−ブチロラクトン85重量%の水溶液を三重管式口金の中心の管から吐出し、γ−ブチロラクトン85重量%の水溶液からなる温度5℃の浴中で固化させた後、水洗して90℃の水中で1.4倍に延伸し乾燥させた。得られた支持層は球状構造であった。
(Comparative Example 2)
Resin solution 1 was prepared by dissolving 40% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 60% by weight of γ-butyrolactone at 150 ° C. Further, 36% by weight of vinylidene fluoride homopolymer having a weight average molecular weight of 41,000 and 64% by weight of γ-butyrolactone were dissolved at 150 ° C. to obtain a resin solution 2. The resin solution 1 (Tc: 55 ° C.) was held at 90 ° C. for 2.3 minutes, and then discharged from the outer annular port of the triple tube die. At the same time, the resin solution 2 (Tc: 48 ° C.) was 0 ° C. at 115 ° C. After holding for 1 minute, it was discharged from the inner annular port of the triple tube type die, and an aqueous solution of 85% by weight of γ-butyrolactone was further discharged from the tube at the center of the triple tube type die to obtain an aqueous solution of 85% by weight of γ-butyrolactone. After solidifying in a bath at a temperature of 5 ° C., it was washed with water, stretched 1.4 times in water at 90 ° C. and dried. The obtained support layer had a spherical structure.

薄膜は実施例1と同様にして形成させた
得られた複合中空糸膜の構造と性能を表1に示す。
The thin film was formed in the same manner as in Example 1. Table 1 shows the structure and performance of the obtained composite hollow fiber membrane.

樹脂溶液2を二重管式口金の内側の環状口から吐出する前の、保持温度が高く、保持時間が短かかったため、支持層の分離層側を形成する球状構造の平均直径が2μmより大きくなり、中空糸膜の内表面に薄膜が均一に形成されておらず、球状構造がむき出しの部分がみられた。   Since the holding temperature was high and the holding time was short before discharging the resin solution 2 from the inner annular port of the double tube type die, the average diameter of the spherical structure forming the separation layer side of the support layer was larger than 2 μm. Thus, a thin film was not uniformly formed on the inner surface of the hollow fiber membrane, and an exposed portion of the spherical structure was observed.

Figure 2008173573
Figure 2008173573

本発明で規定する支持層の分離層側の界面から支持層方向に深さ5μmの位置の空隙の大きさの測定方法を表す模式図である。It is a schematic diagram showing the measuring method of the magnitude | size of the space | gap of the position of a depth of 5 micrometers in the support layer direction from the interface by the side of the separated layer of the support layer prescribed | regulated by this invention.

符号の説明Explanation of symbols

1 分離層
2 支持層
3 支持層の分離層側の界面
4 空隙
5 支持層の分離層側の界面から支持層方向に深さ5μmの位置の空隙の大きさ
DESCRIPTION OF SYMBOLS 1 Separation layer 2 Support layer 3 Separation layer side interface 4 of support layer Void 5 Void size at a depth of 5 μm from support layer separation layer side interface toward support layer

Claims (5)

熱可塑性樹脂の球状構造からなる支持層と、非多孔質材料からなる分離層から構成される複合中空糸膜であって、複合中空糸膜の長手方向に垂直な断面写真において、支持層の分離層側の界面から支持層方向に深さ5μmの位置の空隙の大きさが2μm以下であることを特徴とする複合中空糸膜。 A composite hollow fiber membrane composed of a support layer composed of a spherical structure of a thermoplastic resin and a separation layer composed of a non-porous material, and the separation of the support layer in a cross-sectional photograph perpendicular to the longitudinal direction of the composite hollow fiber membrane A composite hollow fiber membrane, wherein the size of a void at a depth of 5 µm in the direction of the support layer from the layer side interface is 2 µm or less. 支持層の分離層と反対側を形成する球状構造の平均直径D2が0.1μm以上2μm以下である請求項1記載の複合中空糸膜。 The composite hollow fiber membrane according to claim 1, wherein an average diameter D2 of a spherical structure forming the side opposite to the separation layer of the support layer is 0.1 µm or more and 2 µm or less. 支持層の分離層側を形成する球状構造の平均直径D1と前記平均直径D2が、D1<D2の関係を満たす請求項2に記載の複合中空糸膜。 The composite hollow fiber membrane according to claim 2, wherein the average diameter D1 of the spherical structure forming the separation layer side of the support layer and the average diameter D2 satisfy a relationship of D1 <D2. 支持層の分離層側が三次元網目構造からなり、支持層の分離層と反対側が球状構造からなる請求項1または2に記載の複合中空糸膜。 The composite hollow fiber membrane according to claim 1 or 2, wherein the separation layer side of the support layer has a three-dimensional network structure, and the opposite side of the support layer to the separation layer has a spherical structure. 熱可塑性樹脂がポリフッ化ビニリデン樹脂である請求項1〜4のいずれかに記載の
複合中空糸膜。
The composite hollow fiber membrane according to any one of claims 1 to 4, wherein the thermoplastic resin is a polyvinylidene fluoride resin.
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US8388743B2 (en) 2008-10-30 2013-03-05 Aisan Kogyo Kabyshiki Kaisha Separation membrane module and fuel vapor processing apparatus incorporating the same
CN104474922A (en) * 2014-11-14 2015-04-01 东莞市长安东阳光铝业研发有限公司 Preparation method of polyvinylidene fluoride hollow fiber water treatment membrane
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US9174174B2 (en) 2008-09-19 2015-11-03 Toray Industries, Inc. Separation membrane and method for producing the same
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Publication number Priority date Publication date Assignee Title
US9174174B2 (en) 2008-09-19 2015-11-03 Toray Industries, Inc. Separation membrane and method for producing the same
US8388743B2 (en) 2008-10-30 2013-03-05 Aisan Kogyo Kabyshiki Kaisha Separation membrane module and fuel vapor processing apparatus incorporating the same
WO2016006611A1 (en) * 2014-07-07 2016-01-14 東レ株式会社 Separation membrane and method for producing same
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JPWO2016006611A1 (en) * 2014-07-07 2017-05-18 東レ株式会社 Separation membrane and manufacturing method thereof
CN106536029B (en) * 2014-07-07 2019-09-27 东丽株式会社 Separation membrane and its manufacturing method
US10702834B2 (en) 2014-07-07 2020-07-07 Toray Industries, Inc. Separation membrane and method for producing same
CN104474922A (en) * 2014-11-14 2015-04-01 东莞市长安东阳光铝业研发有限公司 Preparation method of polyvinylidene fluoride hollow fiber water treatment membrane
CN104524996A (en) * 2014-12-30 2015-04-22 山东华夏神舟新材料有限公司 Polyvinylidene fluoride hollow fibrous membranes with pressure response characteristic and preparation method thereof
CN104984663A (en) * 2015-06-15 2015-10-21 黄义忠 Film casting liquid for PVDF flat membrane and preparing method for PVDF flat membrane
JP2017213515A (en) * 2016-05-31 2017-12-07 株式会社クラレ Porous film, composite membrane, and porous film manufacturing method

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