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Air vehicle with bilateral steering thrusters

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/66    F42B-010/00    F42B-012/62   
출원번호 US-0743834 (2013-01-17)
등록번호 US-9068808 (2015-06-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Renner, Otto, Boisselle & Sklar, LLP
인용정보 피인용 횟수 : 2  인용 특허 : 38
초록
▼

An air vehicle, such as a missile or a steerable submunition released from a missile or another air vehicle, has a bilateral thrust system for steering. The thrust system includes a pair of diametrically-opposed divert thrusters that provide thrust having radial components in opposite radial directions. In order to control the direction of thrust, the air vehicle controls rotation of the divert thrusters and/or timing of the firing of the thrusters. The air vehicle (or some part of the air vehicle that includes the divert thrusters) may be discretely rol...

대표
청구항
▼

1. An air vehicle comprising: a thrust system that includes a pair of diametrically-opposed divert thrusters that provide thrust having radial components in opposite radial directions;a rotation system for rotating the divert thrusters circumferentially about a longitudinal axis of the air vehicle; anda control system operatively coupled to the thrust system and the rotation system;wherein the thrust system includes a pressurized gas source that provides continuous flow of pressurized gas, and a valve that apportions the continuous flow between the diver...

이 특허에 인용된 특허 (38)

  1. Hanlon, Casey; Geck, Kellan; Johnson, Andrew T.. Actuation assembly. USP2012128338768.
  2. Metz Pierre (Paris FRX). Control device using gas jets for a guided missile. USP1984114482107.
  3. O'Dwyer, James Michael. Directional control of missiles. USP2005056889935.
  4. Schroeder Wayne K. (Arlington TX). Dual-control scheme for improved missle maneuverability. USP1997055631830.
  5. Hasson, Joseph; Goldner, Galya. Exo atmospheric intercepting system and method. USP2010097791006.
  6. Metz Pierre (Paris FRX). Gas jet steering device and method missile comprising such a device. USP1984084463921.
  7. Horwath, Tibor G.. Guidance seeker system with optically triggered diverter elements. USP2004076766979.
  8. Horwath, Tibor G.. Guidance seeker system with optically triggered diverter elements. USP2004116817569.
  9. Thouron Ren (La Ferte St. Aubin FRX). Guidance/control device for a carrier comprising a movable nozzle. USP1991055016836.
  10. Metz Pierre (Paris FRX). Guided projectile. USP1993085238204.
  11. Minick, Alan B.; Hobart, Stephen Alan; Widman, Frederick; Kokan, Timothy S.; Massey, Frederic H.. Guided projectile. USP2011027891298.
  12. Heitmann,Thomas; Schwenzer,Michael. Lateral thrust control. USP2006107118065.
  13. Bagley Cloy J. (Fountain Valley CA). Lateral thruster for missiles. USP1990114967982.
  14. Smirra Karl,DEX. Lateral-thrust control arrangement for missiles with solid-fuel hot-gas generator. USP2001096289669.
  15. Nelson Steven D. ; Sipes William J. ; Hoffmaster David K.. Mems synthesized divert propulsion system. USP2001016178741.
  16. Linick James (Naples FL). Method and apparatus for radial thrust trajectory correction of a ballistic projectile. USP1997075647558.
  17. Pagliara, Philip W.; Leal, Michael A.; Jenia, Justin C.; Dalbello, Teryn; Hitner, John M.. Methods and apparatus for a tandem divert and attitude control system. USP2014088800913.
  18. Bielas, Michael S.; Schlatter, Edward C.; Facciano, Andrew B.; Theriault, Philip C.; Ebel, James A.; LaPorte, Robert J.. Mitigation of drift effects in secondary inertial measurements of an isolated detector assembly. USP2013108552350.
  19. Olden, Thomas A.; Cavalleri, Robert J.. Modular divert and attitude control system. USP2012088242422.
  20. 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.
  21. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  22. Folsom,Mark; Piper, III,Charles; Fahey,Wm. David; McGowan,Jared M.. Projectile diverter. USP2006027004423.
  23. Mark Folsom ; Charles Piper, III ; Wm. David Fahey ; Jared M. McGowan. Projectile diverter. USP2002046367735.
  24. Unterstein Klaus (Dsseldorf DEX). Projectile steering block. USP1988024726544.
  25. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
  26. 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.
  27. Machell Anthony (Stevenage GB2) Foulsham Peter G. (Stevenage GB2). Reaction control system. USP1990094955558.
  28. Davies Guy E. (Hampshire GB2). Reaction jet control system. USP1989084856734.
  29. Sturm Richard (Ottobrunn DEX). Remote control system for a rolling flying body. USP1990054928906.
  30. Goddard Charles W. (San Jose CA) Lucas John T. (Los Altos CA) Galvan Paul A. (San Jose CA). Solid-propellant-powered maneuvering system for spacecraft. USP1991115062593.
  31. Howell, W. Scott; Pruitt, Thomas M.. Spin control system for a suspended object that is to be deployed in or recovered from water. USP2012078226042.
  32. Thomas E. Harkins ; T. Gordon Brown. System and method for reducing dispersion of small rockets. USP2002026347763.
  33. 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.
  34. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral gas jets. USP1992065123611.
  35. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral nozzles. USP1991125074492.
  36. Fujita,Toshiharu; Hidaka,Shozo. Three-axis attitude control propulsion device and flying object comprising the same. USP2006097102113.
  37. Mayersak Joseph R. (Ashburn VA). Thrust maneuver system. USP1995105456429.
  38. Smith Gregory H. ; Clark Roland D.. Universal driver circuit for actuating both valves and ordnances. USP2001076267326.

이 특허를 인용한 특허 피인용횟수: 2

  1. Flynn, Dennis Joseph; Locking, Paul Martin; Johnson, Martin. Drag reduction system. USP20180710030951.
  2. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.

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