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"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Co-molding metallic-lined phenolic components

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B23P-015/00   
미국특허분류(USC) 029/890.01; 086/056
출원번호 US-0851973 (2004-05-20)
등록번호 US-7493691 (2009-02-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ingrassia Fisher & Lorenz, P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 28
초록

A method is provided for manufacturing a missile component for use in a high temperature environment, where the missile component has a flow passage therethrough and the flow passage has a shape. An apparatus manufactured by the inventive method is provided as well. The method includes the steps of depositing a first metal onto a mandrel having the shape of the flow passage to create a first metal layer, applying an insulating material on to the first metal layer to create an insulating layer, machining a predetermined shape into at least a portion of th...

대표
청구항

We claim: 1. A method for manufacturing a missile component for use in a high temperature environment, the missile component having a flow passage therethrough, wherein the flow passage has a shape, the method comprising: depositing a first metal onto a mandrel having the shape of the flow passage to create a first metal layer; packing an insulating material around the mandrel and the first metal layer while the mandrel is disposed in a container; heating and pressurizing the mandrel to cause the insulating material to fuse into an insulating layer; mac...

이 특허에 인용된 특허 (28)

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  2. Donadio Robert F.. Chemical vapor deposition method. USP1998095800753.
  3. Myers W. Neill ; Cornelius Charles S.. Combustion chamber/nozzle assembly and fabrication process therefor. USP2000126164060.
  4. Singer Victor ; Solberg Mark A.. Design for a gun-launched rocket. USP2000086094906.
  5. Harvey, Albert R.; Ellertson, John W.. Fiber-reinforced rocket motor insulation. USP2004026691505.
  6. Cherry Charles C. (McGregor TX) Wiechering Raymond E. (Waco TX). Foamed in place igniter and aft-end assembly for rocket motor comprising the same. USP1993065220783.
  7. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C.. Hybrid rocket system and disposable cartridge for use therein. USP2000076082097.
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  9. Metcalf, Gary S.; White, William E.. Method of constructing insulated metal dome structure for a rocket motor. USP2003046554936.
  10. Ring Peter J. (20335 Hickory Hill Way Saratoga CA 95070) Kangilaski Mihkel (260 S. 15th St. San Jose CA 95112). Method of fabricating a rocket thrust chamber. USP1997035613299.
  11. Tuffias Robert H. ; Williams Brian E. ; Kaplan Richard B.. Method of forming a composite structure such as a rocket combustion chamber. USP1999015855828.
  12. Ring Peter John. Method of making a rocket thrust chamber. USP2001036205661.
  13. Knaresboro Donald Lee ; Goodson Forrest Ray ; Inman Frank Stephen. Method of manufacturing solid rocket motors. USP2000086101948.
  14. Vandendriessche Georges (Vernon FRX). Method of manufacturing the wall of a combustion chamber, in particular for a rocket engine, and a combustion chamber ob. USP1993085233755.
  15. Russell, Mark C.; Doyle, Sean P.; Russell, Charles T.. Method of producing a channeled wall fluid control apparatus. USP2003066582542.
  16. Tsantrizos Peter G.,CAX ; Kim George E.,CAX ; Cavasin Alexander P.,CAX ; Grenier Serge,CAX. Near net-shape VPS formed multilayered combustion system components and method of forming the same. USP2000076087023.
  17. Tsantrizos Peter G.,CAX ; Kim George E.,CAX ; Cavasin Alexander P.,CAX ; Grenier Serge,CAX. Near net-shape VPS formed multilayered combustion system components and method of forming the same. USP2001106296723.
  18. Bihlmaier John A. (Marengo IL). Process for making articles with smooth complex internal geometries. USP1991055012853.
  19. Hawkinson Elden L. (West Hills CA). Production method for a channeled wall thrust nozzle. USP1990074942653.
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  21. Priceman Seymour (Seaford NY). Refractory metal composite coated article. USP1993065223045.
  22. Cesaroni Anthony J.,CAXITX L3R 8J1 ; Bartel Scott ; Kline Korey R.. Reloadable/modular solid propellant rocket motor. USP2000066079202.
  23. Hans Paul C. (Scottsdale AZ) Rosenfield Gary C. (Las Vegas NV) Meyer Daniel H. (Henderson NV). Reloadable/modular solid propellant rocket motor. USP1993055212946.
  24. Holmes Richard R. ; McKechnie Timothy N.. Rocket combustion chamber coating. USP2001116314720.
  25. Cornelius Charles S. ; Counts Richard H. ; Myers W. Neill ; Lackey Jeffrey D. ; Peters Warren ; Shadoan Michael D. ; Sparks David L. ; Lawrence Timothy W.. Rocket engine thrust chamber assembly. USP2001036195984.
  26. Dombrowski Daniel C. (Elkton MD) Frey Thomas J. (Elkton MD) Nevrincean Andrew G. (Elkton MD) Carr ; Jr. Clyde E. (Lincoln University PA). Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture. USP1997025600946.
  27. Sayles David C. (Huntsville AL). Thermoplastic para-polyphenylene sulfide, high temperature-resistant rocket motor cases. USP1995015380570.
  28. Siemers Paul A. (Clifton Park NY) Kopp Robert W. (Ballston Lake NY) Jackson Melvin R. (Schenectady NY) Duke Steven R. (Williston VT) Perrin David P. (Charlotte VT) Liu Ying H. (South Burlington VT). Wear resistant gun barrel and method of forming. USP1986034577431.