$\require{mediawiki-texvc}$
  • 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

Variable coupling arrangement for an integrated missile steering system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00   
미국특허분류(USC) 244/003.22 ; 600/228 ; 239/265.29 ; 239/265.31 ; 244/169
출원번호 US-0935571 (1997-09-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Bissell
인용정보 피인용 횟수 : 15  인용 특허 : 7
초록
▼

An integrated system for missile steering, which uses both jet reaction control (JRC) and aerofin control systems, is provided with a variable coupling mechanism for adjusting the relative responsiveness of the two systems in accordance with the pressurization state of the JRC system pressure chamber. In one embodiment, the pivoting action of a joystick which actuates the gas flow control pintles of the JRC system is permitted only under sufficient pressurization of the pressure chamber. In a second embodiment, the extent to which the pintles protrude fr...

대표
청구항
▼

[ What is claimed is:] [1.]1. Variable response jet reaction control apparatus for controlling the flight of a missile, said apparatus comprising:a pressure chamber;a plurality of thrust nozzles in communication with said pressure chamber, said thrust nozzles adapted for directional emission of gases generated in said pressure chamber;a movably mounted gas flow controller;a plurality of pintles each associated with a corresponding one of said plurality of thrust nozzles, said pintles adapted to vary the flow of gases through said thrust nozzles in respon...

이 특허에 인용된 특허 (7)

  1. Girardeau Jean-Louis (Paris FRX) Grossi Augustin (Montesson FRX) Farges Jol (Arcueil FRX) Fiandesio Patrick (Longjumeau FRX). Device for actuating a mechanical member, in particular for the force guidance of a missile, and missile equipped with s. USP1995045405103.
  2. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA). Differential yoke-aerofin thrust vector control system. USP1996045505408.
  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. Kranz Walter (Taufkirchen DEX). Guided missile. USP1991055016835.
  5. Morris Joseph W. (Rancho Cordova CA) Carlson Russell W. (Folsom CA) Peterson Kevin L. (Sacramento CA) Reich Edward M. (Orangevale CA). Multiple pintle nozzle propulsion control system. USP1995105456425.
  6. Machell Anthony (Stevenage GB2) Foulsham Peter G. (Stevenage GB2). Reaction control system. USP1990094955558.
  7. Bennett James (Stevenage GBX) Heath Martin R. (Stevenage GBX) Foulsham Peter G. (Stevenage GBX). Thruster system. USP1989054826104.

이 특허를 인용한 특허 피인용횟수: 15

  1. Morgan, Robert W; Normoyle, James P; Wuest, Kurt J; Drake, David. Air vehicle with control surfaces and vectored thrust. USP2015099121680.
  2. Schroeder,Richard W.. Fin retention and deployment mechanism. USP2009017475846.
  3. Smith,Douglas L.; Morris,Joseph P.. Frictional roll control apparatus for a spinning projectile. USP2008087412930.
  4. Kim,Won Hoon; Bae,Joo Chan; Lim,Seong Taek; Park,Sung Han. Jet vane thrust vector control system. USP2008017313910.
  5. Lawandy, Nabil M.; Conroy, Jeffrey L.; Smuk, Andrei. Marking articles using a covert digitally watermarked image. USP2009057529385.
  6. Lawandy,Nabil M.; Conroy,Jeffrey L.; Smuk,Andrei. Marking articles using a covert digitally watermarked image. USP2007027184569.
  7. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016019242745.
  8. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016109469419.
  9. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2017079696726.
  10. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016049302790.
  11. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016069365300.
  12. Morris,Joseph P.; Smith,Douglas L.. Projectile trajectory control system. USP2008047354017.
  13. Ericson,Charles R.; May,Michael C.. Tandem motor actuator. USP2007087255304.
  14. Kawai, Ronald Tatsuji. Thrust vectoring system and method. USP2012088240125.
  15. Fink,Lawrence E.. Two-axis thrust vectoring nozzle. USP2007057216476.

IPC 상위 출원인