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Low mass flow reaction jet

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00    F42B-015/00   
미국특허분류(USC) 244/003.22; 244/003.15; 244/003.21; 244/051; 244/052; 244/062
출원번호 US-0287020 (2002-11-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Foster Laura R.
인용정보 피인용 횟수 : 6  인용 특허 : 20
초록
▼

A control system for a flying vehicle in an atmospheric environment, the vehicle having an aerodynamic shape including a front end and a rear end including a plurality of attitude control jet nozzles spaced outward from the vehicle near the rear end of the vehicle or a trailing edge of a vehicle part; and a generator for providing a low mass flow of a fluid through the attitude control jet nozzles to create an area of high pressure immediately forward of the nozzles and adjacent the flying vehicle, wherein the location of the attitude control jet nozzles...

대표
청구항
▼

1. A control system for a flying vehicle in an atmospheric environment, the vehicle having an aerodynamic shape including a front end and a rear end, said control system allowing the overall weight and equipment to be reduced in the vehicle, comprising:(a) a plurality of attitude control jet nozzles directed outward from the vehicle, said nozzles being located at the extreme end of the vehicle or the trailing edge of a vehicle part, said nozzles arranged in groups in lines orthogonal to the main axis of the vehicle, wherein the shape of said nozzles is s...

이 특허에 인용된 특허 (20)

  1. King ; Sr. Lloyd Herbert. Air craft wing. USP2000086109565.
  2. Metz Pierre (Paris FRX). Control device using gas jets for a guided missile. USP1984114482107.
  3. Roucoux Bertrand (Saint Jean le Blanc FRX). Control of a projectile by multi-chamber and single-nozzle impeller. USP1997085657948.
  4. Metz Pierre (Paris FRX). Gas jet steering device and method missile comprising such a device. USP1984084463921.
  5. Metz Pierre (Paris FRX). Guided projectile. USP1993085238204.
  6. Bagley Cloy J. (Fountain Valley CA). Lateral thrust assembly for missiles. USP1992075129604.
  7. Bagley Cloy J. (Fountain Valley CA). Lateral thruster for missiles. USP1990114967982.
  8. Nelson Steven D. ; Sipes William J. ; Hoffmaster David K.. Mems synthesized divert propulsion system. USP2001016178741.
  9. Schfer Berthold (Bergisch Gladbach DEX). Missile. USP1987124712748.
  10. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  11. Tubeuf Jean (Le Chesnay FR). Projectile guidance. USP1976083977629.
  12. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
  13. Robert J. Adams ; Michael B. McFarland ; Wayne V. Spate ; Arthur J. Schneider ; Michael J. Kaiserman ; Stanton L. Winetrobe. Propulsive torque motor. USP2002116478250.
  14. Sturm Richard (Ottobrunn DEX). Remote control system for a rolling flying body. USP1990054928906.
  15. Thomas E. Harkins ; T. Gordon Brown. System and method for reducing dispersion of small rockets. USP2002026347763.
  16. 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.
  17. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral gas jets. USP1992065123611.
  18. Kirschner ; Jr. Thomas J.. Thrusting apparatus. USP2001116315238.
  19. Gerhardt Heinz A. (Redondo Beach CA). Transverse thrust lift augmentation system. USP1987034648571.
  20. Smith Gregory H. ; Clark Roland D.. Universal driver circuit for actuating both valves and ordnances. USP2001076267326.

이 특허를 인용한 특허 피인용횟수: 6

  1. De Roche,Mark Stephen. Hybrid drive powered lift platform. USP2007067231997.
  2. Low, Richard; Deeds, Michael; Jean, Daniel L.; Hovland, Christopher. MEMS control surface for projectile steering. USP2009127628352.
  3. Patel, Mehul; Corke, Tom. Method of increasing the performance of aircraft, missiles, munitions and ground vehicles with plasma actuators. USP2017129834301.
  4. 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.
  5. 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.
  6. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.

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