[특허]Pressure vessels for high temperature applications and a method for their manufacture

Pressure vessels for high temperature applications and a method for their manufacture 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02K-009/00
출원번호	US-0611185 (2009-11-03)
등록번호	US-8613190 (2013-12-24)
우선권정보	DE-10 2008 054 293 (2008-11-03)
발명자 / 주소	Murawski, Bernd Maierhofer, Helmut
출원인 / 주소	MT Aerospace AG
대리인 / 주소	Rothwell, Figg, Ernst & Manbeck, P.C.
인용정보	피인용 횟수 : 0 인용 특허 : 30

초록 ▼

The invention relates to a pressure vessel consisting of a housing and an insulating layer lining the inner surface of the housing. The housing is formed from a fiber composite material which has a high mechanical and thermal resistance and the insulating layer is formed from a gas-tight silicone elastomer, with the housing and the insulating layer being bonded to each other. The invention also relates to a method for the manufacture of such pressure vessels.

대표청구항 ▼

1. A pressure vessel (10) having high specific stiffness, consisting of a housing (15) and a layer of insulation (20) lining the inner surface (16) of the housing (15), wherein the housing (15) is made from a mechanically and thermally high-strength fiber composite material that is composed of mechanically and thermally high-strength reinforcing fibers in a mechanically and thermally high-strength resin matrix and from a gas-tight filled silicon elastomer, and wherein the layer of insulation (20) and the housing (15) are adhesively bonded, such that the pressure vessel is operable at a mean temperature of at least 200° C. 2. The pressure vessel of claim 1, wherein the fibers are chosen from carbon, glass, silicon carbide, mullite, boron carbide, aramid and/or carbon aramid fibers. 3. The pressure vessel of claim 2, wherein the fibers are carbon fibers. 4. The pressure vessel of claim 1, wherein the resin forming the resin matrix is a thermosetting resin. 5. The pressure vessel of claim 4, wherein the thermosetting resin is a polyphenol cyanate. 6. The pressure vessel of claim 1, wherein the silicone elastomer is fiber reinforced. 7. The pressure vessel of claim 1, wherein the silicone elastomer is filled with powdered silica. 8. The pressure vessel of claim 7, wherein the silicone elastomer has an expansibility of at least 3%. 9. The pressure vessel of claim 1, wherein said pressure vessel has an essentially elongated cylindrical geometry. 10. The pressure vessel of claim 1 in the form of a gas bottle. 11. The pressure vessel of claim 1 in the form of a solid fuel combustion chamber for guided missiles.

이 특허에 인용된 특허 (30)

Gerrish ; Jr. Howard W. (Ridgecrest CA) Vetter Ronald F. (Ridgecrest CA) Sieg George F. (Ridgecrest CA) Bennett Harold L. (Ridgecrest CA), Ablative liner.
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Gajiwala, Himansu M., Basalt fiber and nanoclay compositions, articles incorporating the same, and methods of insulating a rocket motor with the same.
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Martin Jon W. (Los Alamitos CA) Griese Richard A. (Redlands CA), Carbon and silicone polymer ablative liner material.
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Decker Owen H. (Okesa OK) Mumford Neal A. (Brigham UT), Chemorheologically tailored matrix resin formulations and their use in making pre-impregnated fibers and in fabricating.
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Mumford Neal A. (Brigham City UT) Chin Cheng-Chi (Salt Lake City UT) Johns Rolf M. (Brigham City UT) Lloyd Ben A. (Brigham City UT), Chemorheologically tailored matrix resin formulations containing anhydride curing agents.
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Yorgason James A. (Ogden UT), Composite/metal hybrid rocket motor case and methods for manufacturing.
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Kotcharian Michel (Paris FRX), Cryogenic tank.
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Goetz Douglas P. (St. Paul MN) Hine Andrew M. (St. Paul MN) Schultz William J. (Vadnais Heights MN) Thompson Wendy L. (Roseville MN), Curable resin sols and fiber-reinforced composites derived therefrom.
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Mine Katsutoshi (Ichihara JPX) Yokoyama Masuo (Ichihara JPX), Curable two-part silicone rubber compositions with improved adhesion properties.
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Hughes, Craig D.; Blau, Reed J., Double-base rocket propellants, and rocket assemblies comprising the same.
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Enders Mark L. ; Robinson Tony T., Insensitive munitions composite pressure vessels.
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Hawkinson Elden L. (Canoga Park CA), Laminated shield for missile structures and substructures.
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Felix Bernard R. (Saratoga CA) Slosarik Stephen E. (Los Gatos CA), Liner for a solid propellant rocket motor.
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Murray Cornelius F. (Lincoln NE), Metal-lined pressure vessel.
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Decker Owen H. (West Reading PA) Lloyd Ben A. (Brigham City UT) Mumford Neal A. (Brigham City UT), Method for increasing fiber strength translation in composite pressure vessels using matrix resin formulations containin.
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Chen Cheng-Chi (Arlington TX) Lloyd Ben A. (Brigham City UT) Mumford Neal A. (Brigham City UT) Johns Rolf M. (Brigham City UT), Method for increasing fiber strength translation in composition pressure vessels using matrix resin formulations contain.
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Guillot, David G., Method of insulating a case of a solid propellant rocket motor.
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Guillot,David G., Method of insulating a case of a solid propellant rocket motor.
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Olliff ; Jr. Martin T. (Huntsville AL), Method of preserving a composite material cased solid propellant rocket motor.
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Coffinberry George A. (West Chester OH), Multiple-propellant air vehicle and propulsion system.
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Iida,Yasushi; Kitano,Akihiko; Yamagiwa,Masayoshi; Kobayashi,Masanobu; Noguchi,Kenichi, Pressure vessel and process for producing the same.
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DeLay, Thomas K.; Patterson, James E.; Olson, Michael A., Pressure vessel with improved impact resistance and method of making the same.
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Sorathia Usman A. (Arnold MD) Houghton Deborah A. (Annapolis MD) Owen David P. (Pasadena MD) Pipyne Markus R. (Burke VA) Jones Wayne C. (Catonsville MD) Castelli Vincent J. (Severna Park MD) Fischer , Protective device for container.
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Steele Robin S. ; Stenger Jennifer L., Reinforced composite structure.
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Itoh Takahiro (Nagoya JPX) Togawa Morito (Nagoya JPX) Okada Masuo (Neyagawa JPX) Matsumura Sowjun (Toyonaka JPX) Chiba Tadashi (Hirakata JPX), Rocket engine combustion chamber.
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Vetter Ronald F. (Ridgecrest CA), Rocket motor end flap.
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Chase Michael John (Kidderminster EN) Smith Derek Anthony (London EN) Dudley Michael Alan (Beaconsfield CA), Rocket motor with ablative insulating casing liner.
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Smith Bradley W. (Ogden UT), Solid propellant canister loaded multiple pulsed or staged rocket motor.
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Chase Michael J. (Shropshire GB2), Thermal insulators for rocket motors.
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Sayles David C. (Huntsville AL), Thermoplastic para-polyphenylene sulfide, high temperature-resistant rocket motor cases.
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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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Pressure vessels for high temperature applications and a method for their manufacture 원문보기

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Pressure vessels for high temperature applications and a method for their manufacture 원문보기

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연구과제 타임라인

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