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특허 상세정보

Gas jet steering device and method missile comprising such a device

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/02   
미국특허분류(USC) 244/322 ; 239/26519 ; 239/26527 ; 239/26529
출원번호 US-0370100 (1982-04-20)
우선권정보 FR-0007915 (1981-04-21)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 28  인용 특허 : 1
초록

A steering device comprising an annular element having N exhaust nozzles and a rotary element disposed coaxially inside said annular element; the rotary element comprising M gas passageways may be positioned in MN discrete directions so as to provide a transverse thrust force orientated in one of the steering planes.

대표
청구항

A gas jet steering device for a guided missile, said get jet steering device comprising: (a) an annular element having a plurality N of equi-angularly spaced fixed exhaust nozzles inclined at and angle a

이 특허를 인용한 특허 피인용횟수: 28

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  3. Kranz Walter (Taufkirchen DEX). Apparatus for correcting the flight path of a missile. USP1987074681283.
  4. Kranz Walter (Taufkirchen DEX). Brake and release apparatus for a rotary nozzle body. USP1987094691876.
  5. Kranz Walter (Taufkirchen DEX). Controllable flow deflection system. USP1987034646991.
  6. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA). Differential yoke-aerofin thrust vector control system. USP1997055630564.
  7. O'Dwyer, James Michael. Directional control of missiles. USP2005056889935.
  8. Ransom, Richard Sutton. Flight control of missiles. USP2012028119959.
  9. Guinan Daniel P. ; Wendt David E.. Flow diverter system for multiple streams for gas turbine engine. USP2000086102329.
  10. Thouron Ren (La Ferte St. Aubin FRX). Guidance/control device for a carrier comprising a movable nozzle. USP1991055016836.
  11. Smirra Karl,DEX. Lateral-thrust control arrangement for missiles with solid-fuel hot-gas generator. USP2001096289669.
  12. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  13. Frank F. Webster. Modular rocket boosted penetrating warhead. USP2002126494140.
  14. Bains William R. (Lake Elsinore CA). Pneumatically actuated ram air steering system for a guided missile. USP1987084685639.
  15. Joseph R. Mayersak. Precision guidance system for aircraft launched bombs. USP2002106460801.
  16. Dryer, Richard L.. Projectile control device. USP2011128076623.
  17. Preston, Kenneth G.; Leal, Michael A.; Wilson, Rondell J.; Hussey, Richard C.. Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control. USP2014058735788.
  18. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.
  19. Schmacker Bruce E.. Rocket-boosted guided hard target penetrator. USP2001086276277.
  20. Carlson, Robert J.. Steerable projectile charging system. USP2013018362408.
  21. Kranz Walter (Taufkirchen DEX) Tillmann Heinz (Riemerling DEX). Stepping mechanism for rotary motions. USP1991065024395.
  22. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M. System and method for attitude control of a flight vehicle using pitch-over thrusters. USP2010127851732.
  23. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M.. System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system. USP2011087989743.
  24. 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.
  25. Mazenq, Lionel. System for steering, about its axes of rotation, a moving body propelled by jet reaction, particularly a missile. USP2015079080843.
  26. Fujita,Toshiharu; Hidaka,Shozo. Three-axis attitude control propulsion device and flying object comprising the same. USP2006097102113.
  27. Kranz Walter (Taufkirchen DEX). Thrust nozzle system. USP1986054589594.
  28. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.