$\require{mediawiki-texvc}$
  • 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"

과학기술 지식인프라 ScienceON

상세검색 다국어 입력
도움말도움말
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

MyON담기
내보내기

Rocket motor with pellet and bulk solid propellants

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/10    F02K-009/12   
미국특허분류(USC) 102/376; 060/253
출원번호 UP-0053475 (2008-03-21)
등록번호 US-7685940 (2010-04-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    SoCal IP Law Group LLP
인용정보 피인용 횟수 : 7  인용 특허 : 19
초록

There is disclosed a solid fuel rocket motor which may include a case and a nozzle coupled to the case. A plurality of fuel pellets may be disposed within the case. An igniter may be disposed to ignite at least a portion of the fuel pellets. A pellet retainer may be positioned within the case to retain the plurality of fuel pellets within the case. The pellet retainer may be perforated to allow exhaust gases to flow from the ignited fuel pellets to the nozzle while preventing unburned fuel pellets from being expelled through the nozzle.

대표
청구항
▼

It is claimed: 1. A solid fuel rocket motor comprising: a case a propellant charge disposed within the case a plurality of propellant pellets disposed within the case an igniter disposed to ignite the propellant charge and the plurality of propellant pellets a nozzle coupled to the case a pellet retainer to retain unburned propellant pellets within the case, wherein combustion gases flow from ignited propellant pellets to the nozzle through perforations in the pellet retainer a total of the area of the perforations in the pellet retainer is greater than...

이 특허에 인용된 특허 (19)

  1. Rotkopf, Menachem. Armor piercing projectile. USP2004066745696.
  2. Koorey Alfred J. (Maitland FL). Boost-sustain-boost rocket. USP1988044738100.
  3. Katoh Masayoshi (Kawagoe JPX) Ishii Takashi (Tokyo JPX) Nagaoka Tadahiko (Sayama JPX). Combusting device for generation of a combustion gas. USP1981024249673.
  4. Wagstaff Douglas C.,GBX. Fire mitigation device. USP1999095959235.
  5. Kline, Korey R.; Smith, Kevin W.; Cesaroni, Anthony Joseph. Flame holder for a hybrid rocket motor. USP2004056739121.
  6. Barnes Michael W. (Brigham City UT) Taylor Robert D. (Hyrum UT). Gas generant compositions containing amine nitrates plus basic copper (II) nitrate and/or cobalt(III) triammine trinitra. USP1997035608183.
  7. Daniel W. Doll ; Gary K. Lund ; Craig D. Hughes ; Marc A. Hall ; David J. Macon. Gas generating eject motor. USP2002036352030.
  8. Osofsky Irving B. (28327 San Nicolas Dr. Rancho Palos Verdes CA 90274). High velocity impulse rocket. USP1995085440993.
  9. Stevens, George L.. Igniter pellet cup. USP1985094539910.
  10. Metcalf, Gary S.; White, William E.. Method of constructing insulated metal dome structure for a rocket motor. USP2003046554936.
  11. Martins, Laura J.; Cragun, Richard B.; Lund, Gary K.; Wells, Michael V.; Mancini, Vincent E.. Method of making multi-base propellants from pelletized nitrocellulose. USP2004026692655.
  12. Cesaroni, Anthony Joseph; Dennett, Michael J.; Kline, Korey R.; Mahaffy, Kevin E.; Smith, Kevin W.. Oxidizer package for propellant system for rockets. USP2003116647888.
  13. Cesaroni,Anthony J.; Dennett,Michael J.; Louwers,Jeroen. Propellant system for solid fuel rocket. USP2006047022196.
  14. Krishnan, Vinu B.. Propulsion from combustion of solid propellant pellet-projectiles. USP2005116968676.
  15. Krishnan,Vinu B.. Propulsion from combustion of solid propellant pellet-projectiles. USP2007037194852.
  16. Alan Z. Glasser. Propulsion system. USP2002036357357.
  17. Canterberry J. B. (Taft TN) Flanigan David A. (Ogden UT). Rapid burning propellant charge for automobile air bag inflators, rocket motors, and igniters therefor. USP1991065024160.
  18. Dombrowski Daniel C. (Elkton MD) Frey Thomas J. (Wilmington DE) Nevrincean Andrew G. (Oxford PA). Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture. USP1997105675966.
  19. Le Helley,Philippe; Jacques,Louis; Magni챕re,Christophe; Uhrig,Gilles; Bondon,Bernard; Tricot,Jean Claude; Boury,Didier; Telara,Marco; Bellomi,Paolo; Mastrangelo,Georgio. System and method of controlling pressure oscillations of hydrodynamic origin for a solid propellant thruster. USP2006027003942.

이 특허를 인용한 특허 피인용횟수: 7

  1. Olden, Thomas A.; Wrigglesworth, Walter. Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof. USP2014098826640.
  2. Olden, Thomas A.; Cavalleri, Robert J.. Modular divert and attitude control system. USP2012088242422.
  3. Cavalleri, Robert J.; Olden, Thomas A.. Pellet loaded attitude control rocket motor. USP2012038127534.
  4. Olden, Thomas A.; Cavalleri, Robert J.. Pellet-loaded multiple impulse rocket motor. USP2014038667776.
  5. Dupont, James H.; Whitmarsh, Sean J.. Solid propellant rocket motors employing tungsten alloy burst discs and methods for the manufacture thereof. USP2014058713912.
  6. Portela, Mario Placido. Solid rocket braking system. USP2014048683933.
  7. Olden, Thomas A.; Wrigglesworth, Walter. Systems and methods for composite structures with embedded interconnects. USP2014088809689.

IPC 상위 출원인