• 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

Steering arrangement for projectiles of the missile kind, and projectiles fitted with this arrangement

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/18   
미국특허분류(USC) 244/322
출원번호 US-0894209 (1978-04-06)
우선권정보 FR-0010755 (1977-04-08)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 20  인용 특허 : 1

A steering arrangement for missile type projectiles. A source of steering propulsion which is accommodated in the vicinity of the center of gravity of the missile comprises two gas generators which are positioned symmetrically on either side of the center of gravity a system being provided to switch or divert the gases to the exterior of the missile in at least two directions which are transverse to the projectile and to its axis. The arrangement according to the invention considerably improves the reliability and effectiveness with which the projectile ...


A piloting arrangement for a guided missile having a body comprising, in combination, two gas generators in said missile body for providing a source of gas flow, said two gas generators being coupled in parallel and disposed symmetrically at either side of the center of gravity of said missile body, a nozzle having a throat disposed between said two gas generators coaxially with the longitudinal axis of said missile, conduit means in said missile for conducting said gas flow from said gas generators to said nozzle throat, a plurality of peripheral ejecti...

이 특허를 인용한 특허 피인용횟수: 20

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Carlson, Russell; Barr, Dustin; Yan, Allen. Attitude control system. USP2018039927217.
  3. Uhle Heiko (Egmating DEX). Control system particularly for wingless guided ammunition. USP1986064595157.
  4. Clancy,John A.; Bybee,Thomas D.; Friedrich,William A.. Fixed canard 2-D guidance of artillery projectiles. USP2006016981672.
  5. Kranz Walter (Taufkrichen DEX). Fluid distributor. USP1990104964592.
  6. Metz Pierre (Palaiseau FRX). Gas propellor for guided missile. USP1987014637572.
  7. Bergmann, Edward; London, Brian; Dineen, Andrew. Guidance control system for projectiles. USP2012098269156.
  8. Crepin Roger (Ville D\Avray FRX). Lateral gas jet piloting device. USP1986124632336.
  9. Nelson Steven D. ; Sipes William J. ; Hoffmaster David K.. Mems synthesized divert propulsion system. USP2001016178741.
  10. Facciano, Andrew B.; Moore, Robert T.; Hlavacek, Gregg J.; Do, Michael D.. Methods and apparatus for transferring a fluid. USP2011087989744.
  11. Bains William R. (Lake Elsinore CA). Pneumatically actuated ram air steering system for a guided missile. USP1987084685639.
  12. Zacharias Athanassios,DEX. Process for guiding a flying object and flying objects. USP1999035880396.
  13. Dryer, Richard L.. Projectile control device. USP2011128076623.
  14. Morenus Richard C. (Long Beach CA) Frazer Alson C. (Santa Ana CA). Ram air combustion steering system for a guided missile. USP1986034573648.
  15. Bains William R. (Lake Elsinore CA) Sumrall Calhoun W. (Irvine CA). Ram air steering system for a guided missile. USP1985064522357.
  16. Lawhorn, William S.; Clinkenbeard, Ivan L.. Small caliber guided projectile. USP1985084537371.
  17. Sutton Trevor G. (Maricopa AZ). Small vehicle roll control and steering. USP1988104779821.
  18. Crawford, James I.; Howell, W. Max. Spin stabilized impulsively controlled missile (SSICM). USP1985124560120.
  19. Raynaud Jacques (Savigny-sur-Orge FRX) Darmois Jean (Bourg-la-Reine FRX) Jolivet Pierre (Arcueil FRX) Guillot Jean (Chatenay-Malabry FRX). System for piloting a missile by means of lateral gaseous jets and missile comprising such a system. USP1985074531693.
  20. Rossi, Rinaldo. System for steering a flying object using pairs of lateral nozzles. USP2015129212880.