$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Oxidation resistant insulating sandwich tiles

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B32B-003/26
출원번호 US-0620737 (2000-07-20)
발명자 / 주소
  • Rawal, Suraj P.
  • Kustas, Frank M.
출원인 / 주소
  • Lockheed Martin Corporation
대리인 / 주소
    Marsh, Fischmann & Breyfogle LLP
인용정보 피인용 횟수 : 9  인용 특허 : 26

초록

A lightweight insulating sandwich tile (110) having applications such as spacecraft and reusable launch vehicle thermal protection is disclosed. In one embodiment, the lightweight insulating sandwich tile (110) includes an outer structural facesheet (120) that is bonded or co-cured with an inner ins

대표청구항

A lightweight insulating sandwich tile (110) having applications such as spacecraft and reusable launch vehicle thermal protection is disclosed. In one embodiment, the lightweight insulating sandwich tile (110) includes an outer structural facesheet (120) that is bonded or co-cured with an inner ins

이 특허에 인용된 특허 (26)

  1. Haldeman Charles W. (Concord MA), Ablative protective material for reentry bodies.
  2. Schmidt Ronald P. (Crowley TX), Aircraft thermal protection system.
  3. Parrot Pierre (Bordeaux FRX) Lalanne Philippe (Bordeaux FRX) Herman Philippe (Saint Medard en Jalles FRX) Tisne Jean-Louis (Martignas FRX), Arrangement for thermal protection of an object, such as a thermal shield.
  4. Washburn Robert M. (Santa Clara CA) Dodson Jerry D. (Fremont CA), Carbon-carbon composite and method of preparation.
  5. Stover Edward R. (Wayne PA), Carbon/carbon composite for re-entry vehicle applications.
  6. Sorenson Eric Todd ; Daws David Eric, Ceramic matrix composite/organic matrix composite hybrid fire shield.
  7. Riccitiello Salvatore R. (San Jose CA) Smith Marnell (San Jose CA) Goldstein Howard E. (Saratoga CA) Zimmerman Norman B. (Los Gatos CA), Ceramic/ceramic shell tile thermal protection system and method thereof.
  8. Chee Wan T. (Bellevue WA) McLaren Douglas (Seattle WA) Therrien Keith E. (Wausau WI), Composite material structure with integral fire protection.
  9. Zwan Allen D. (San Diego CA), Dual-mode semi-passive nosetip for a hypersonic weapon.
  10. Taverna Arthur R. (Lexington MA) Thompson Warren S. (Stoneham MA), Erosion-resistant nosetip construction.
  11. Seibold ; Robert W. ; Parechanian ; Haig S. ; Weatherill ; William T. ; Lowe ; Robert E., Fiber-resin-carbon composites and method of fabrication.
  12. Seibold Robert W. (Santa Monica CA) Parechanian Haig S. (Fountain Valley CA) Weatherill William T. (La Palma CA) Lowe Robert E. (Santa Ana CA), Fiber-resin-carbon composites and method of fabrication.
  13. Baker Anna L. (Seattle WA) Garrigus Darryl F. (Seattle WA), Fibrous ceramic aerobrake.
  14. Liu Matthew T. (Slidell LA), High temperature ablative foam.
  15. Shih Wei-Teh ; Tallon James Acker ; Janah Ashok Kumar, High temperature composite and method.
  16. Kolodziej Paul ; Bull Jeff ; Kowalski Thomas ; Switzer Matthew, Integrated thermal insulation system for spacecraft.
  17. Gentilman Richard L. (Acton MA), Laser hardened missile casing.
  18. Curran Richard Norman (Auburn WA), Method for forming a contoured insulated honeycomb core panel and panel produced.
  19. Kolodziej Paul ; Carroll Joe A. ; Smith Dane, Method for molding planar billet of thermally insulative material into predetermined non-planar shape.
  20. Lacombe Alain (Pessac FRX) Rouges Jean-Michel (Merignac FRX), Method of manufacturing thermal shielding elements for space planes.
  21. Tanzilli Richard A. (Malvern PA) Gebhardt Joseph J. (Malvern PA) Fenton Richard M. (Hatboro PA) Kreitz ; Jr. James C. (Bechtelsville PA), Rigidized, low density, insulation.
  22. Black William E. (San Diego CA) Parekh Ebrahim M. (San Diego CA), Sublimitable carbon-carbon structure for nose tip for re-entry space vehicle.
  23. Leger ; Lubert J., Thermal insulation attaching means.
  24. Dotts Robert L. (Seabrook TX) Maraia Robert J. (Seabrook TX) Smith James A. (Seabrook TX) Strouhal George (Friendswood TX), Thermal insulation protection means.
  25. Hogenson Peter A. (Long Beach CA), Thermal insulation system and method of forming thereof.
  26. Brazel James P. (Berwyn PA), Tri-element carbon based heat shield.

이 특허를 인용한 특허 (9)

  1. Toombs, Gordon R., Applying sealant to narrow deep gaps in an ablative heat shield surface.
  2. Gettle, Guy Leath, Blast effect mitigating assembly using aerogels.
  3. Stackpoole, Margaret M.; Ghandehari, Ehson M.; Thornton, Jeremy J.; Covington, Melmoth Alan, Flexible ablators.
  4. Wood, Adam C., In-flight insulation generation using matrix-based heat sink for missiles and other flight vehicles.
  5. Renzi, Peter Nicholas, Launch pad flame deflector structure and method of making the same.
  6. Halamandaris, George P.; Pinney, Thomas R.; Embler, Jonathan D.; Lang, Adam J.; Rackers, Keith G.; Lehman, Stephen E., Mechanically attached thermal protection system.
  7. Brown, Scott C.; Cain, Andrew W.; Thompson, Randell L., Method for the manufacturing of a composite.
  8. Quertelet, Clément, Missile structural wall for thermal protection fairing.
  9. Uskert, Richard Christopher; Freeman, Ted Joseph; Thomas, David John; Lane, Jay, Multi-layer ceramic composite porous structure.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트