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Pressure relief device for solid propellant motors subjected to high external temperatures

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/00   
미국특허분류(USC) 060/253; 060/039.1
출원번호 US-0488179 (1990-03-05)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Bush, Freddie M.
인용정보 피인용 횟수 : 23  인용 특허 : 1
초록

A rocket motor that has a solid propellant with closure means that is secd to the rocket motor housing by heat responsive means that melts before the solid propellant ignites to prevent the rocket motor from becoming propulsive when subjected to excessive external heat sufficient to cause the rocket propellant to ignite.

대표
청구항
▼

1. A rocket motor comprising a housing with a solid propellant mounted therein, said housing having a first groove extending into and around an internal surface which is void of said solid propellant at one of said housing, said housing having a second groove extending into and around an internal surface void of said propellant at the other end of said housing; closure means having a groove extending into and around the periphery of an external surface, said groove being in an adjacent position when installed to said first groove of said housing; heat re...

이 특허에 인용된 특허 (1)

  1. Telmo Frisco T. (King George VA). Enclosure for a warhead case. USP1984014423683.

이 특허를 인용한 특허 피인용횟수: 23

  1. Friedlander, III, Mark Peyser. Apparatus and method for passive venting of rocket motor or ordnance case. USP2005106952995.
  2. Taub, Robert D.; Cabanilla, J. Alexander; Tourtellot, George. Collaborative music creation. USP2010057714222.
  3. Diehl, Matthew D.; Schneck, Eric Michael; Bogan, Gregory Norman. Decoupling assembly for a plumbing network. USP2017129851188.
  4. Singer Victor ; Solberg Mark A.. Design for a gun-launched rocket. USP2000086094906.
  5. Singer Victor ; Solberg Mark A.. Gun-launched rocket. USP1998085792981.
  6. Roach, Eric E.. Method and apparatus for releasably attaching a closure plate to a casing. USP2004066752085.
  7. Prytz,Alf. Method and arrangement for preventing encased explosives being caused to explode by an external fire. USP2006057051511.
  8. Rose Larry D. ; Marchant Brent R.. Pressure relief in airbag module reaction canisters. USP1998025718447.
  9. Diehl, Matthew D.; Schneck, Eric Michael; Bogan, Gregory Norman. Pressure vessel with safety features. USP2014128919254.
  10. Park, Byeong Yeol; Koo, Song Hoe; Yoo, Ji Chang; Doh, Young Dae. Propulsion system and rocket having the same. USP2016049303591.
  11. Cesaroni Anthony J.,CAXITX L3R 8J1 ; Bartel Scott ; Kline Korey R.. Reloadable/modular solid propellant rocket motor. USP2000066079202.
  12. Woo, Timothy; Moy, Leon; Elmasri, Bishara; Morales, Christina; Cohen, Alan N.; Prillaman, Daniel Lee. Riveted cartridge venting. USP2013108550004.
  13. Diehl, Matthew D.; Schneck, Eric Michael; Bogan, Gregory Norman. Rocket motor tube with safety features. USP2013118578855.
  14. Solberg, Mark A.; Black, Robert E.. Rocket motors with insensitive munitions systems. USP2003096619029.
  15. Solberg, Mark A.; Black, Robert E.. Rocket motors with insensitive munitions systems and projectiles including same. USP2005116966264.
  16. Kaddour, Abdul-Salam; Cook, John. Rupturing devices. USP2013128616131.
  17. Cherry, Charles C.; Wiechering, Raymond E.. Solid propellant rocket motor with fusible end closure holder. USP199303H001144.
  18. Johnson Randolph T.. Thermally actuated release mechanism. USP2001116321656.
  19. Ellingsen Warren W.. Thermostatic bimetallic retaining ring for use in rocket motor assembly. USP1998045735114.
  20. Steven S. Kim ; John R. Luense. Vented MK 66 rocket motor tube with a thermoplastic warhead adapter. USP2002016338242.
  21. Cannon, Thomas C.. Venting cap system. USP2013088505458.
  22. Kim,Steven S.; Hawley,Eric; Johnson,Joni; Nolder,Matt; Luense,John. Venting system for explosive warheads. USP2008027331292.
  23. Moy, Leon; Ruland, Daniel; Yang, Edward; Foltynski, Jacek. Water-lined munition container. USP2016059329010.

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