$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Gas generating eject motor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) C06D-005/00    F41F-003/04   
미국특허분류(USC) 102/291; 102/287; 102/289; 102/374; 60/256; 89/001807; 89/001818
출원번호 US-0436357 (1999-11-09)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sullivan Law Group
인용정보 피인용 횟수 : 16  인용 특허 : 5
초록

A gas generating eject motor includes a case containing an ignitable low temperature gas generant material that does not produce toxic gases upon the combustion thereof. The gas generant material is generally contained with a screen enclosure housed within the case. An igniter is disposed within the gas generant material for selectively igniting the gas generant to thereby generate combustion gases. A nozzle is disposed within an open aft end of the case for focusing and directing the combustion gases generated by the ignited gas generant material. The c...

대표
청구항

1. An eject motor to be coupled to a missile that is launched from a launch platform structure and is propelled by ignited combustible rocket motor propellant for initiating a launch sequence of the missile by propelling the missile from the launch platform structure prior to ignition of the combustible rocket motor propellant, said eject motor comprising:a case including structure for coupling said case to the missile; an ignitable gas generant material stored in said case; a screen enclosure disposed within said case for retaining said ignitable gas ge...

이 특허를 인용한 특허 피인용횟수: 16

  1. Ryu,Chulsung; Seol,Wooseok; Han,Sangyeop. Ablative baffle for a liquid rocket engine thrust chamber. USP2006057036303.
  2. Danforth, Jeremy; Loehr, Richard D.. Cartridge-loaded rocket motor with castellated grain segments. USP2012108281568.
  3. Blomquist, Harold R.; Helmy, Abdelkader M.; Sampson, William P.; Mangum, Michael G.. Cool burning gas generating material for a vehicle occupant protection apparatus. USP2005046875295.
  4. Oleynik, Vladislav; Ezell, Melvin Jason; Riggs, Jeffrey L.; Albul, Gennadiy. Electrical power generator. USP2012108294287.
  5. Riggs, Jeffrey L.; Oleynik, Vladislav; Borovikov, Valery; Albul, Gennadiy. Explosive decompression propulsion system. USP2012058181561.
  6. Olden, Thomas A.; Wrigglesworth, Walter. Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof. USP2014098826640.
  7. Veitch,Alan J.; Machell,Anthony; Winter,John W. M.; Harriss,Roger T.. Launching of missiles. USP2007047207254.
  8. Olden, Thomas A.; Cavalleri, Robert J.. Modular divert and attitude control system. USP2012088242422.
  9. Oleynik, Vladislav; Ezell, Melvin Jason; Riggs, Jeffrey L.; Albul, Gennadiy. Multiphase material generator vehicle. USP2013028378509.
  10. Cavalleri, Robert J.; Olden, Thomas A.. Pellet loaded attitude control rocket motor. USP2012038127534.
  11. Olden, Thomas A.; Cavalleri, Robert J.. Pellet-loaded multiple impulse rocket motor. USP2014038667776.
  12. Riggs, Jeffrey L.; Oleynik, Vladislav; Borovikov, Valery; Albul, Gennadiy. Projectile propulsion system. USP2012128327747.
  13. Gany, Alon; Michales, Dan. Propulsion system and method using a combustion chamber discharging a concentrated mass. USP2014078789795.
  14. Cavalleri, Robert J.; Olden, Thomas A.. Rocket motor with pellet and bulk solid propellants. USP2010037685940.
  15. Sloman, Roger Mark. Rocket motors and their use. USP2018069989013.
  16. Olden, Thomas A.; Wrigglesworth, Walter. Systems and methods for composite structures with embedded interconnects. USP2014088809689.