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특허 상세정보

Adjustable range munition

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/32    F42B-010/00   
미국특허분류(USC) 244/003.22; 244/003.1; 244/003.15; 244/003.21
출원번호 US-0788816 (2010-05-27)
등록번호 US-8618455 (2013-12-31)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kane Kessler, P.C.
인용정보 피인용 횟수 : 2  인용 특허 : 36

An adjustable range munition has at least one gas vent that is selectively variable to affect the amount of force that is directed onto the projectile upon actuation of the propellant section, thereby to control the range of the munition.


1. An adjustable range munition comprising: a propellant section that is actuatable to produce gas under pressure; anda projectile releasably connected with the propellant unit;the projectile having an engagement surface that receives force of the gas under pressure to cause the projectile to release from the propellant unit and travel toward a target;the projectile having at least one gas vent that is selectively variable to affect the amount of force that is directed onto the projectile by the gas under pressure upon actuation of the propellant section...

이 특허에 인용된 특허 (36)

  1. Hibma Richard A. ; Hilscher Richard W. ; Miralles Carlos T. ; Ward Jerry D. ; Wright Blaine G.. Apparatus for defending a vehicle against an approaching threat. USP2001056231003.
  2. Metz Pierre (Paris FRX). Control device using gas jets for a guided missile. USP1984114482107.
  3. Kranz Walter (Taufkrichen DEX). Control propulsion unit, especially for exerting transverse forces on a missile. USP1990124979697.
  4. Ryan William F. (Phoenix AZ). Fluidic thruster control and method. USP1983114413795.
  5. Metz Pierre (Paris FRX). Gas jet steering device and method missile comprising such a device. USP1984084463921.
  6. Horwath, Tibor G.. Guidance seeker system with optically triggered diverter elements. USP2004116817569.
  7. Leonard John P. (Huntsville AL). Guided missile using fluidic sensing and steering. USP1976093979085.
  8. Metz Pierre (Paris FRX). Guided projectile. USP1993085238204.
  9. Minick, Alan B.; Hobart, Stephen Alan; Widman, Frederick; Kokan, Timothy S.; Massey, Frederic H.. Guided projectile. USP2011027891298.
  10. Botwin Leo (Westport CT) Simpson John A. (Southport CT). Gun-launched variable thrust ramjet projectile. USP1984014428293.
  11. Botwin Leo (Westport CT) Simpson John A. (Southport CT). Gun-launched variable thrust ramjet projectile. USP1985034502649.
  12. Grau, John C.; Fiorellini, Arthur J.; Carr, Raymond E.. Jump correcting projectile system. USP2003106629668.
  13. Bagley Cloy J. (Fountain Valley CA). Lateral thruster for missiles. USP1990114967982.
  14. Nelson Steven D. ; Sipes William J. ; Hoffmaster David K.. Mems synthesized divert propulsion system. USP2001016178741.
  15. Gundel, Bernd; Graf, Hans-Rainer; Hammer, Helmut; Thurner, Günther. Method and device for varying a flight path of a projectile by intentional tumbling of the projectile. USP2010067741588.
  16. Schfer Berthold (Bergisch Gladbach DEX). Missile. USP1987124712748.
  17. Bchele-Buecher Sigfrid (Meerbusch DEX). Missile steering device. USP1992055112007.
  18. 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.
  19. Bisping Bernhard (Ratingen DEX) Romer Rudolf (Kaarst DEX) Gerbach Klaus (Willich DEX) Wallow Peter (Dsseldorf DEX). Munitions round for barrel-type weapons. USP1984044444114.
  20. Biggers James E. ; Finn Kevin P. ; Schwartz ; II Homer H.. Neural network controller for a pulsed rocket motor tactical missile system. USP2000106138945.
  21. Keigler John Edward (Princeton NJ) Muhlfelder Ludwig (Livingston NJ) Cenker Robert Joseph (Princeton NJ). Orientation system for a spin stabilized spacecraft. USP1976083977633.
  22. Ensmenger Gary E. Pressurized gas/water rocket and launcher therefor. USP1998115839940.
  23. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  24. Folsom,Mark; Piper, III,Charles; Fahey,Wm. David; McGowan,Jared M.. Projectile diverter. USP2006027004423.
  25. Mark Folsom ; Charles Piper, III ; Wm. David Fahey ; Jared M. McGowan. Projectile diverter. USP2002046367735.
  26. Tubeuf Jean (Le Chesnay FR). Projectile guidance. USP1976083977629.
  27. Unterstein Klaus (Dsseldorf DEX). Projectile steering block. USP1988024726544.
  28. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
  29. Davies Guy E. (Hampshire GB2). Reaction jet control system. USP1989084856734.
  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. Crepin Roger (Paris FRX). Steering arrangement for projectiles of the missile kind, and projectiles fitted with this arrangement. USP1980074211378.
  32. Purcell William O. (Maitland FL). Submunition having terminal trajectory correction. USP1985014492166.
  33. Metz Pierre (Paris FRX). Terminal guidance method and a guided missile operating according to this method. USP1986024568040.
  34. Mayersak Joseph R. (Ashburn VA). Thrust maneuver system. USP1995105456429.
  35. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.
  36. Smith Gregory H. ; Clark Roland D.. Universal driver circuit for actuating both valves and ordnances. USP2001076267326.