JP4805539B2 - 複合材でできた部品の酸化からの保護 - Google Patents
複合材でできた部品の酸化からの保護 Download PDFInfo
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- C—CHEMISTRY; METALLURGY
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/85—Coating or impregnation with inorganic materials
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- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C8/00—Enamels; Glazes; Fusion seal compositions being frit compositions having non-frit additions
- C03C8/14—Glass frit mixtures having non-frit additions, e.g. opacifiers, colorants, mill-additions
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- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C8/00—Enamels; Glazes; Fusion seal compositions being frit compositions having non-frit additions
- C03C8/14—Glass frit mixtures having non-frit additions, e.g. opacifiers, colorants, mill-additions
- C03C8/20—Glass frit mixtures having non-frit additions, e.g. opacifiers, colorants, mill-additions containing titanium compounds; containing zirconium compounds
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/50—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
- C04B41/5022—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials with vitreous materials
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/52—Multiple coating or impregnating multiple coating or impregnating with the same composition or with compositions only differing in the concentration of the constituents, is classified as single coating or impregnation
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/85—Coating or impregnation with inorganic materials
- C04B41/86—Glazes; Cold glazes
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/89—Coating or impregnation for obtaining at least two superposed coatings having different compositions
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/97—Rocket nozzles
- F02K9/974—Nozzle- linings; Ablative coatings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D69/02—Composition of linings ; Methods of manufacturing
- F16D69/023—Composite materials containing carbon and carbon fibres or fibres made of carbonizable material
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00241—Physical properties of the materials not provided for elsewhere in C04B2111/00
- C04B2111/00362—Friction materials, e.g. used as brake linings, anti-skid materials
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00474—Uses not provided for elsewhere in C04B2111/00
- C04B2111/00982—Uses not provided for elsewhere in C04B2111/00 as construction elements for space vehicles or aeroplanes
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/02—Light metals
- F05C2201/025—Boron
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/222—Silicon
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D2200/00—Materials; Production methods therefor
- F16D2200/0034—Materials; Production methods therefor non-metallic
- F16D2200/0039—Ceramics
- F16D2200/0047—Ceramic composite, e.g. C/C composite infiltrated with Si or B, or ceramic matrix infiltrated with metal
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
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- Application Of Or Painting With Fluid Materials (AREA)
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Description
前記部品に粉末状の少なくとも1つのホウ化物、ガラスを形成することによる修復特性を有する粉末状の少なくとも1つのガラス状耐火酸化物、および耐火セラミックの前駆体である樹脂を含むバインダの混合物を含む組成物を適用し、かつ前記樹脂を硬化することを含む方法で達成され、
その方法において、前記ホウ化物粉末はその大部分がホウ化チタンTiB2で構成され、かつ少なくとも1つのガラス状耐火性酸化物の前記粉末はその大部分がホウケイ酸塩混合物を含む。
−少なくとも大部分が(50重量%以上)細かく分割された形態のホウ化チタン(TiB2)を含む金属ホウ化物粉末であって、ホウ化アルミニウムAlB2および/またはAlB12、および/またはホウ化ケイ素SiB4および/またはSiB6のような、1つまたは複数のほかのホウ化物を随意に添加され得る;
−前記部品に対して意図された操作温度で自己修復性であるケイ酸塩ガラスを生成または形成することができる、微細に分割された粉末状の耐火性酸化物、その酸化物は大部分が酸化ホウ素および酸化ケイ素を含む;
−バインダとして働く耐火セラミックの前駆体である樹脂;
−前記樹脂の溶媒;および
−セラミック材料で作られる短繊維状または“ウィスカー”状の任意の固体フィラー、
を含む。
SiO2 80.6%
B2O3 12.60%
Na2O 4.2%
Al2O3 2.25%
Cl 0.1%
CaO 0.1%
MgO 0.05%
Fe2O3 0.04%
参照「8330」、「8337B」、「8486」、および「88656」でドイツの会社スコッチにより製造される、それらのような酸化ホウ素または酸化ケイ素から主に形成される、他のガラスが使用されることができる
耐火セラミックの前駆体を構成する樹脂は、ポリカルボシラン(PCB);シリコンカーバイドSiCの前駆体;ポリチタンカルボシラン(PTCS)、またはチタンがいくつかの他の金属(ジルコニウムのような)を置き換わった他の誘導体、そのSiC前駆体物質は特に日本の会社宇部興産から特に販売されている;またはポリシラジン、ポリシロキサン、ポリビニルシラン(PVS)またはシリコーン樹脂のようなSi−C−OまたはSi−C−Nシステムのためのほかの前駆体から例えば選択される。
本発明の保護被覆を立証するために、C/C複合材のサンプルは以下の条件の下で保護被覆を供され、かつ高温(1000℃またはそれ以上)で、乾燥空気または湿った空気中で検査された。
TiB2粉末: 320 grams(g)
“Pyrex(登録商標)”: 83.6 g
PCS樹脂(乾燥した固体状): 100 g
溶媒(キシレン): 150 g
混合物が均一化された後、組成物はペイントブラシを用いてそれぞれのサンプルの外側表面の全体にわたり適用され、2つの連続被覆は中間乾燥段階、およびいくらかの場合PCSの硬化の中間段階を適用された。
実施例1のものと同一のC/C複合材サンプルは保護被覆を、以下の組成物の1つまたは2つの被覆を適用することで供された(2つの被覆が適用されたとき第1被覆を硬化する中間工程があった)。
“Pyrex(登録商標)”: 20.9 g
シリコーン樹脂: 31.25 g
溶媒(キシレン): 31.25 g
本実施例の方法では、使用されたシリコーン樹脂は参照「H62C」でドイツの会社Wacker Chemieによって販売されている樹脂であった。
実施例1のものと同一のC/C複合材サンプルは実施例2の組成物の1つの被覆(サンプルIおよびJ)、または2つの被覆(サンプルKおよびL)、その場合中間乾燥および第1被覆の硬化があった、を適用することで保護被覆を供された。
C/C複合材サンプルは実施例1の組成物を使用した2つの硬化された被覆からなる保護被覆を供された。
同一のC/C複合材サンプルが以下の3つの方法:
−サンプルM:最終セラミック化を900℃で、実施例2の方法を用いた;
−サンプルN:C/C複合材サンプル超音波によって攪拌されたタンク内に浸透させることを含み、かつ「Marlophen 89」という名でドイツの会社Hulsによって販売されている潤滑剤の0.5重量%の水溶液を収容し、かつそれから乾燥後、リン酸アルミニウムAl(H2PO4)3の50重要%溶液を水にペイントブラシを使用して適用することを含む、文献US5 853 821の実施例1の方法を使用した;乾燥後、熱処理は窒素雰囲気下において漸次700℃まで上昇した温度でなされた;および
−サンプルO:サンプルNへの米国特許5 853 821に従って適用される保護に続いて、サンプルMへの本発明に従い適用される保護を連続的に適用した。
Claims (14)
- 複合材部品を酸化から保護する方法であって、前記方法は、粉末状の少なくとも1つのホウ化物と、ガラスを形成することによる修復特性を有する粉末状の少なくとも1つのガラス状耐火酸化物と、ポリカルボシラン、ポリチタンカルボシラン、ポリシラザン、ポリビニルシラン、およびシリコーン樹脂から選ばれ、Siを含んだ耐火セラミックの前駆体である樹脂を含んだバインダとの混合物を含んだ組成物を前記部品に適用することと、前記樹脂を硬化することと、前記前駆体が耐火性セラミックに転換されるセラミック化の熱処理工程とを含み、
前記ホウ化物粉末はその50重量%以上がホウ化チタンTiB2で構成され、かつ少なくとも1つのガラス状耐火性酸化物の前記粉末はその50重量%以上がホウケイ酸塩混合物を含むことを特徴とする方法。 - 前記硬化は、400℃より低い温度でなされることを特徴とする請求項1記載の方法。
- 前記部品には、硬化後に200μmから700μmの範囲にある厚さを有する被覆を形成する組成物が適用されることを特徴とする請求項1または2に記載の方法。
- 前記組成物は、前記部品に、複数の連続被覆として、中間硬化を伴って適用されることを特徴とする請求項1または2に記載の方法。
- 前記熱処理工程は、不活性雰囲気中において600℃よりも高い温度でなされることを特徴とする請求項1から4のいずれか1項記載の方法。
- 前記熱処理工程は、酸化性雰囲気中、800℃よりも高いかまたはそれと同等の温度でなされることを特徴とする請求項1から4のいずれか1項記載の方法。
- 前記熱処理は、炉内でのフラッシュ酸化、空気中での火炎処理、および電磁結合による部分加熱からなる方法の1つによりなされることを特徴とする請求項6記載の方法。
- 炭素/炭素複合材部品を保護するために、前記組成物は耐火性下地被覆を形成した後に適用されることを特徴とする請求項1から7のいずれか1項記載の方法。
- シリコンカーバイドを含んだ耐火性下地被覆が形成されることを特徴とする請求項8記載の方法。
- 前記部品に少なくとも1つのリン酸塩を含む組成物を浸透させる前工程を含むことを特徴とした請求項1から9のいずれか1項記載の方法。
- 前記組成物は、前記セラミック−前駆体のための溶媒をさらに含み、それにより前記組成物の粘度を調節することを特徴とする請求項1から10のいずれか1項記載の方法。
- 前記組成物は、コーティングまたは噴霧によって適用されることと、その後、前記溶媒を乾燥によって除去することとを特徴とする請求項11記載の方法。
- 前記組成物は耐火材料の短繊維をさらに含むことを特徴とする請求項1から12のいずれか1項記載の方法。
- 前記ホウ化物粉末は、アルミニウムのホウ化物およびケイ素のホウ化物から選ばれた少なくとも1つのホウ化物をさらに含むことを特徴とする請求項1から13のいずれか1項に記載の方法。
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Application Number | Priority Date | Filing Date | Title |
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FR0204410A FR2838071B1 (fr) | 2002-04-09 | 2002-04-09 | Protection contre l'oxydation de pieces en materiau composite |
FR02/04410 | 2002-04-09 | ||
PCT/FR2003/001114 WO2003084899A1 (fr) | 2002-04-09 | 2003-04-09 | Protection contre l'oxydation de pieces en materiau composite |
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JP2010250046A Division JP5583554B2 (ja) | 2002-04-09 | 2010-11-08 | 複合材でできた部品の酸化からの保護 |
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JP4805539B2 true JP4805539B2 (ja) | 2011-11-02 |
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JP2010250046A Expired - Fee Related JP5583554B2 (ja) | 2002-04-09 | 2010-11-08 | 複合材でできた部品の酸化からの保護 |
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Country Status (15)
Country | Link |
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US (1) | US6740408B2 (ja) |
EP (1) | EP1494981B1 (ja) |
JP (2) | JP4805539B2 (ja) |
KR (1) | KR100912315B1 (ja) |
CN (1) | CN1646450B (ja) |
AT (1) | ATE334951T1 (ja) |
AU (1) | AU2003246800A1 (ja) |
CA (1) | CA2482001C (ja) |
DE (1) | DE60307254T2 (ja) |
ES (1) | ES2270069T3 (ja) |
FR (1) | FR2838071B1 (ja) |
MX (1) | MXPA04009928A (ja) |
RU (1) | RU2323916C2 (ja) |
UA (1) | UA79272C2 (ja) |
WO (1) | WO2003084899A1 (ja) |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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US10323339B2 (en) | 2015-03-25 | 2019-06-18 | Goodrich Corporation | Aircraft brake disc materials and methods |
Also Published As
Publication number | Publication date |
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KR20050005435A (ko) | 2005-01-13 |
DE60307254T2 (de) | 2007-08-30 |
US20030194574A1 (en) | 2003-10-16 |
US6740408B2 (en) | 2004-05-25 |
DE60307254D1 (de) | 2006-09-14 |
RU2004129296A (ru) | 2005-08-20 |
CA2482001C (en) | 2010-10-05 |
EP1494981A1 (fr) | 2005-01-12 |
RU2323916C2 (ru) | 2008-05-10 |
JP2011093797A (ja) | 2011-05-12 |
JP5583554B2 (ja) | 2014-09-03 |
FR2838071B1 (fr) | 2004-07-09 |
WO2003084899A1 (fr) | 2003-10-16 |
FR2838071A1 (fr) | 2003-10-10 |
JP2005522395A (ja) | 2005-07-28 |
ATE334951T1 (de) | 2006-08-15 |
KR100912315B1 (ko) | 2009-08-14 |
CN1646450B (zh) | 2012-12-26 |
MXPA04009928A (es) | 2004-12-07 |
CA2482001A1 (en) | 2003-10-16 |
ES2270069T3 (es) | 2007-04-01 |
UA79272C2 (en) | 2007-06-11 |
EP1494981B1 (fr) | 2006-08-02 |
CN1646450A (zh) | 2005-07-27 |
AU2003246800A1 (en) | 2003-10-20 |
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