$\require{mediawiki-texvc}$
  • 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 flight direction control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-015/02   
미국특허분류(USC) 244/52 ; 244/322 ; 60/230 ; 239/26535
출원번호 US-0313891 (1989-02-23)
우선권정보 JP-0038546 (1988-02-23); JP-0021793 (1988-02-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 15  인용 특허 : 4
초록
▼

To quickly change rocket flight direction immediately after a rocket has been launched without increasing the wing area, the rocket flight direction control system comprises four steering wings for controlling rocket flight directions; four deflectable nozzles for jetting combustion gas backward to generate rocket thrust; a controller for generating steering control signals; and at least one actuator for actuating the deflectable nozzles in response to the steering control signals in synchronism with steering motion of the steering wings. Further, when t...

대표
청구항
▼

A rocket flight direction control system for a rocket including a rocket body and a combustion chamber, said rocket flight direction control system comprising: (a) steering wing means, pivotally attached to said rocket body, for controlling rocket flight directions; (b) deflectable nozzle means, deflectively attached to said rocket body, for jetting combustion gas from said combustion chamber to generate rocket thrust, said deflectable nozzle means comprising; (1) a fixed divergent nozzle of the overexpansion type, fixedly coupled to said combustion cham...

이 특허에 인용된 특허 (4)

  1. Maudal Inge (Claremont CA). Integrated thrust vector aerodynamic control surface. USP1977084044970.
  2. Young Robert W. (Luton GB2). Jet propulsion efflux outlets. USP1984024432512.
  3. Canfield Alan R. (North Ogden UT) Faupell Lawrence C. (Logan UT) Cardall Stanley H. (Providence UT). Low friction, movable, rocket nozzle. USP1979064157788.
  4. Seeger Hans-Jochen (Ganderkesee DEX). Steering of an aerodynamic vehicle. USP1979084163534.

이 특허를 인용한 특허 피인용횟수: 15

  1. Larsen Richard K. (Lahambra CA). Actuation system with passive compensation for transient loads. USP1997035607123.
  2. Ransom Stephen (Stuhr DEX) Relotius Klaus-Dieter (Bremen DEX). Apparatus for controlling the structural dynamic response of a rocket. USP1997015593110.
  3. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA). Differential yoke-aerofin thrust vector control system. USP1997055630564.
  4. Teneze, Bernard; Blin, Michel. Flying object for observing the ground. USP2010077763834.
  5. Haight, Stephen D.; Chasman, Daniel; Perez, Juan A.. Hybrid missile propulsion system with reconfigurable multinozzle grid. USP2012028117847.
  6. Danielson, Arnold O.. Integrated aerodynamic fin and stowable TVC vane system. USP1994065320304.
  7. Haag Thomas W.. Ion thruster support and positioning system. USP1998045738308.
  8. Chasman,Daniel B.; Leal,Michael; Haight,Stephen D.. Missile control system and method. USP2007107287725.
  9. Chasman,Daniel; Haight,Stephen D.; Facciano,Andrew B.. Missile control system and method. USP2006097108223.
  10. Corder, David A; Merems, Paul A. Passive stability system for a vehicle moving through a fluid. USP2016089429401.
  11. Chasman, Daniel; Haight, Stephen D.. Propulsion system with canted multinozzle grid. USP2010127856806.
  12. Lane, Jeffery G.; Magarro, Richard B.. Rocket engine nacelle. USP2004076758437.
  13. Cesaroni, Anthony Joseph. Surface skimming munition. USP2015018939084.
  14. Cesaroni, Anthony Joseph. Surface skimming munition. USP2016099448049.
  15. Bernard Marc (Marcilly en Villette FRX). System of vehicle guidance by continuous gas jets. USP1991045004184.

IPC 상위 출원인