JP2000504093A - 三次元強化アブレーティブ/断熱複合材 - Google Patents
三次元強化アブレーティブ/断熱複合材Info
- Publication number
- JP2000504093A JP2000504093A JP9527904A JP52790497A JP2000504093A JP 2000504093 A JP2000504093 A JP 2000504093A JP 9527904 A JP9527904 A JP 9527904A JP 52790497 A JP52790497 A JP 52790497A JP 2000504093 A JP2000504093 A JP 2000504093A
- Authority
- JP
- Japan
- Prior art keywords
- ablative
- composite
- layer
- carbon
- resin
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/08—Interconnection of layers by mechanical means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/245—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it being a foam layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/52—Protection, safety or emergency devices; Survival aids
- B64G1/58—Thermal protection, e.g. heat shields
-
- 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
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L59/00—Thermal insulation in general
- F16L59/02—Shape or form of insulating materials, with or without coverings integral with the insulating materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/34—Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2266/00—Composition of foam
- B32B2266/02—Organic
- B32B2266/0214—Materials belonging to B32B27/00
- B32B2266/0285—Condensation resins of aldehydes, e.g. with phenols, ureas, melamines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/304—Insulating
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Critical Care (AREA)
- Health & Medical Sciences (AREA)
- Thermal Sciences (AREA)
- Emergency Medicine (AREA)
- General Health & Medical Sciences (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Laminated Bodies (AREA)
Abstract
Description
Claims (1)
- 【特許請求の範囲】 1.a) 高密度布系アブレーティブ層; b) 複数の耐熱糸のステッチ、ここで、前記ステッチはアブレーティブ層を通 過し、かつ前記ステッチはアブレーティブ層の内表面の外側に補強ループを形成 する;および c) 低密度樹脂系断熱層、ここで前記断熱層は前記ループの周囲に形成され、 アブレーティブ層の内表面に結合する を含んでなる三次元強化アブレーティブ/断熱複合材。 2.布系アブレーティブ層が a) 積み重ねて配置された多重層の布; b) 布層を互いに結合して、布の予備的形成品を形成する手段;および c) 布の予備的形成品内に配置された非繊維アブレーティブ材 を含む請求項1記載の複合材。 3.結合手段が第二の耐熱糸でなされた複数のロックステッチを含む請求項2記 載の複合材。 4.布の予備的形成品が炭素布の多重層を含む請求項2記載の複合材。 5.予備的形成品内に配置した非繊維アブレーティブ材がさらに硬化炭素含有樹 脂を含む請求項4記載の複合材。 6.硬化炭素含有樹脂がフェノール樹脂を含む請求項5の複合材。 7.予備的形成品内に配置した非繊維アブレーティブ材が炭素である請求項4記 載の複合材。 8.第二の耐熱糸が炭素糸である請求項3記載の複合材。 9.耐熱糸が、本質的に炭素糸、石英糸、窒化ケイ素糸および炭化ケイ素糸から なる群より選択される請求項1記載の複合材。 10.断熱層が a) 硬化樹脂;および b) 微細中空球 を含む請求項1記載の複合材。 11.硬化樹脂が、本質的にフェノール樹脂、ゴム化フェノール樹脂、シリコー ン樹脂、エポキシ樹脂およびポリイミド樹脂からなる群より選択される請求項1 0記載の複合材。 12.微細中空球が、本質的にフェノール樹脂中空球、炭素中空球およびガラス 中空球からなる群より選択される請求項10記載の複合材。 13.さらに高温度繊維を含む請求項10記載の複合材。 14.高温度繊維が、本質的に炭素繊維、セラミック繊維およびシリカ繊維から なる群より選択される請求項13記載の複合材。 15.アブレーションからの熱保護のための三次元強化アブレーティブ/断熱複 合材であって、 a) 炭素布の多重層を含有する高密度アブレーティブ層、ここで前記布は硬化 フェノール樹脂をも含有する; b) 複数の炭素糸のステッチ、ここで前記ステッチはアブレーティブ層を通過 し、かつ前記ステッチはアブレーティブ層の内表面の外側に補強ループを形成す る;および c) シンタクチックゴム改質フェノール樹脂フォームの低密度断熱層、ここで 前記フォームは微細中空球および高温度繊維を含有する を含んでなる三次元強化アブレーティブ/断熱複合材。 16.熱浸透条件下での熱保護のための三次元強化アブレーティブ/断熱複合材 であって、 a) 石英布の多重層を含有する高密度アブレーティブ層、ここで前記布は硬化 シリコーン樹脂をも含有する; b) 複数の石英糸のステッチ、ここで前記ステッチはアブレーティブ層を通過 し、かつ前記ステッチはアブレーティブ層の内表面の外側に補強ループを形成す る;および c) シンタクチックシリコーンフォームの低密度断熱層、ここで前記フォーム は微細中空球および高温度繊維を含有する を含んでなる三次元強化アブレーティブ/断熱複合材。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US59427096A | 1996-01-30 | 1996-01-30 | |
US08/594,270 | 1996-01-30 | ||
PCT/US1997/001763 WO1997028399A1 (en) | 1996-01-30 | 1997-01-30 | Three-dimensionally reinforced ablative/insulative composite |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2000504093A true JP2000504093A (ja) | 2000-04-04 |
JP3766694B2 JP3766694B2 (ja) | 2006-04-12 |
Family
ID=24378231
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP52790497A Expired - Lifetime JP3766694B2 (ja) | 1996-01-30 | 1997-01-30 | 三次元強化アブレーティブ/断熱複合材 |
Country Status (8)
Country | Link |
---|---|
EP (1) | EP0877893B1 (ja) |
JP (1) | JP3766694B2 (ja) |
CN (1) | CN1083553C (ja) |
AU (1) | AU2256897A (ja) |
BR (1) | BR9707462A (ja) |
DE (1) | DE69706829T2 (ja) |
IL (1) | IL125473A (ja) |
WO (1) | WO1997028399A1 (ja) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004527441A (ja) * | 2001-01-10 | 2004-09-09 | アルバニー インターナショナル テクニウエィブ インコーポレイテッド | 繊維可変密度を有する熱防護システム |
JP2009298148A (ja) * | 2008-06-13 | 2009-12-24 | Itt Manufacturing Enterprises Inc | 熱バリアシステム |
JP2010105455A (ja) * | 2008-10-28 | 2010-05-13 | Kawasaki Heavy Ind Ltd | 断熱材ならびにそれを備えるフェアリング、回収カプセル、および宇宙往還機 |
JP2011000921A (ja) * | 2009-06-17 | 2011-01-06 | Ihi Aerospace Co Ltd | 突入カプセル、およびその頭頂部の製造方法 |
JP2018155477A (ja) * | 2017-02-08 | 2018-10-04 | ザ・ボーイング・カンパニーThe Boeing Company | 硬化ハイブリッド絶縁非酸化物断熱システム、及び硬化ハイブリッド絶縁非酸化物断熱システムを製造するための非酸化物セラミック複合材料を生成する方法 |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5985405A (en) * | 1996-01-30 | 1999-11-16 | Textron Systems Corporation | Three dimensionally reinforced ablative/insulative composite |
DE102005024408A1 (de) | 2005-05-27 | 2006-11-30 | Airbus Deutschland Gmbh | Verstärkung von Schaumwerkstoffen |
ATE488363T1 (de) | 2005-09-27 | 2010-12-15 | Milliken & Co | Formbare konstruktion mit bindungsschnittstelle |
CN100467348C (zh) * | 2007-01-08 | 2009-03-11 | 新康电脑科技(苏州)有限公司 | 防止航天飞机及其外燃料箱隔热层泡沫块脱落的方法 |
DE102007055684A1 (de) | 2007-11-21 | 2009-06-10 | Airbus Deutschland Gmbh | Vorrichtung zur Herstellung eines verstärkten Schaumwerkstoffes |
WO2010116716A1 (ja) * | 2009-04-07 | 2010-10-14 | パナソニック株式会社 | 繊維断熱体およびこれを用いた真空断熱体 |
CN102729482B (zh) * | 2012-06-29 | 2014-06-25 | 中国人民解放军国防科学技术大学 | 复合材料防热承力筒及其制备方法 |
CN103723269B (zh) * | 2013-09-11 | 2018-01-30 | 太仓派欧技术咨询服务有限公司 | 一种热防护结构 |
CN103540155B (zh) * | 2013-09-29 | 2016-02-10 | 湖北三江航天红阳机电有限公司 | 一种耐高温的烧蚀树脂基复合材料的制备方法 |
CN108032570B (zh) * | 2017-11-28 | 2020-01-31 | 上海航天化工应用研究所 | 一种轻质高强耐海洋气候复合隔热材料及其制备方法 |
CN108274826A (zh) * | 2018-01-22 | 2018-07-13 | 山东大学 | 一种耐高温耐冲蚀碳纤维复合材料管及其制备方法 |
CN109910390B (zh) * | 2019-03-04 | 2020-10-09 | 湖北菲利华石英玻璃股份有限公司 | 一种梯度密度树脂复合材料预制体制备方法 |
CN110481062A (zh) * | 2019-08-02 | 2019-11-22 | 湖北三江航天江北机械工程有限公司 | 一种固体火箭发动机燃烧室壳体外防热层缠绕成型方法 |
CN110549643B (zh) * | 2019-09-06 | 2021-09-07 | 长沙晶优新材料科技有限公司 | 一种天线盖板仿形预制件穿刺方法及天线盖板成型方法 |
DE102020112101A1 (de) | 2020-05-05 | 2021-11-11 | Technische Universität Dresden, Körperschaft des öffentlichen Rechts | Verbundbauteil, Bauteil, und Verfahren zum Herstellen eines Verbundbauteils |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4063684A (en) * | 1975-11-25 | 1977-12-20 | The United States Of America As Represented By The Secretary Of The Air Force | Composite rocket nozzle structure |
US4567076A (en) * | 1984-03-23 | 1986-01-28 | The Boeing Company | Composite material structure with integrated insulating blanket and method of manufacture |
FR2569237B1 (fr) * | 1984-08-14 | 1987-01-09 | Aerospatiale | Dispositif de protection thermique resistant a l'ablation et aux vibrations, et un procede de fabrication |
US5310592A (en) * | 1984-11-02 | 1994-05-10 | The Boeing Company | Fibrous ceramic aerobrake |
FR2625793A1 (fr) * | 1988-01-13 | 1989-07-13 | Bronzavia Air Equipement Sa | Bloc d'isolation thermique |
-
1997
- 1997-01-30 AU AU22568/97A patent/AU2256897A/en not_active Abandoned
- 1997-01-30 IL IL12547397A patent/IL125473A/en not_active IP Right Cessation
- 1997-01-30 JP JP52790497A patent/JP3766694B2/ja not_active Expired - Lifetime
- 1997-01-30 CN CN97191953A patent/CN1083553C/zh not_active Expired - Lifetime
- 1997-01-30 WO PCT/US1997/001763 patent/WO1997028399A1/en active IP Right Grant
- 1997-01-30 DE DE69706829T patent/DE69706829T2/de not_active Expired - Lifetime
- 1997-01-30 EP EP97905745A patent/EP0877893B1/en not_active Expired - Lifetime
- 1997-01-30 BR BR9707462-4A patent/BR9707462A/pt not_active IP Right Cessation
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004527441A (ja) * | 2001-01-10 | 2004-09-09 | アルバニー インターナショナル テクニウエィブ インコーポレイテッド | 繊維可変密度を有する熱防護システム |
JP2009298148A (ja) * | 2008-06-13 | 2009-12-24 | Itt Manufacturing Enterprises Inc | 熱バリアシステム |
JP2010105455A (ja) * | 2008-10-28 | 2010-05-13 | Kawasaki Heavy Ind Ltd | 断熱材ならびにそれを備えるフェアリング、回収カプセル、および宇宙往還機 |
JP2011000921A (ja) * | 2009-06-17 | 2011-01-06 | Ihi Aerospace Co Ltd | 突入カプセル、およびその頭頂部の製造方法 |
JP2018155477A (ja) * | 2017-02-08 | 2018-10-04 | ザ・ボーイング・カンパニーThe Boeing Company | 硬化ハイブリッド絶縁非酸化物断熱システム、及び硬化ハイブリッド絶縁非酸化物断熱システムを製造するための非酸化物セラミック複合材料を生成する方法 |
JP7029288B2 (ja) | 2017-02-08 | 2022-03-03 | ザ・ボーイング・カンパニー | 硬化ハイブリッド絶縁非酸化物断熱システム、及び硬化ハイブリッド絶縁非酸化物断熱システムを製造するための非酸化物セラミック複合材料を生成する方法 |
Also Published As
Publication number | Publication date |
---|---|
WO1997028399A1 (en) | 1997-08-07 |
CN1083553C (zh) | 2002-04-24 |
CN1209867A (zh) | 1999-03-03 |
IL125473A0 (en) | 1999-03-12 |
EP0877893A1 (en) | 1998-11-18 |
BR9707462A (pt) | 2000-01-04 |
JP3766694B2 (ja) | 2006-04-12 |
DE69706829D1 (de) | 2001-10-25 |
AU2256897A (en) | 1997-08-22 |
IL125473A (en) | 2002-02-10 |
EP0877893B1 (en) | 2001-09-19 |
DE69706829T2 (de) | 2002-04-04 |
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