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Fin-stabilized projectile 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F42B-010/14
출원번호 US-0820892 (2001-03-30)
우선권정보 DE-0015514 (2000-03-30)
발명자 / 주소
  • Torsten Niemeyer DE
  • Frank Guischard DE
  • Horst Fritsch DE
출원인 / 주소
  • Rheinmetall W & M GmbH DE
대리인 / 주소
    Venable
인용정보 피인용 횟수 : 25  인용 특허 : 11

초록

A fin-stabilized projectile includes a projectile body having a rear portion defining a rearwardly open cavity and a stabilizing assembly which has an axially slidable fin support in the cavity. The fin support has a retracted position in which the fin support is withdrawn into the cavity and an out

대표청구항

1. A fin-stabilized projectile comprising(a) a projectile body having a longitudinal projectile axis; (b) a rear portion including a rearwardly open cavity; and (c) a stabilizing assembly including (1) a fin support accommodated in said cavity and being axially slidable relative thereto; said fin su

이 특허에 인용된 특허 (11)

  1. Shaffer James E., Airborne vehicle having deployable wing and control surface.
  2. Wedertz Larry D. (Alta Loma CA) Vazquez Jose R. (Rancho Cucamonga CA) Schoneman Scott R. (Ontario CA), Expandable telescoped missile airframe.
  3. Rottenberg, Mark M., Fin assembly.
  4. Sadvary John W. (40 Notch Park Rd. Little Falls NJ 07424) Fung Tim C. (1241 Miriam Pl. Hillside NJ 07205), Fin deployment mechanism for missiles.
  5. Pazmany Ladislao (San Diego CA), Fin erection mechanism.
  6. Epstein Moshe (Haifa ILX) Ezri Moshe B. (Ramat Yishai ILX), Flight control device.
  7. Pollin Irvin, Lock and slide mechanism for tube launched projectiles.
  8. Ulf Holmqvist SE; Ulf Hellman SE; Stig Johnsson SE, Method and device for a fin-stabilized base-bleed shell.
  9. Kastenhuber Manfred (Rednitzhembach DEX) Eckel Alfred (Ireuchtlingen DEX) Bock Erich (Nuremberg DEX), Pivoting guidance mechanism for small-calibered projectiles.
  10. Sharrow Joseph F. (King George VA) Hardy Samuel R. (King George VA), Subassembly means.
  11. Baubry Bernard (Paris FRX), System for the opening of an unfolding tail unit for projectiles.

이 특허를 인용한 특허 (25)

  1. Geswender,Chris E.; Hinsdale,Andrew J.; Blaha,George A.; Dryer,Richard, 2-D projectile trajectory correction system and method.
  2. King, Hartley Hughes; Menna, Thomas Louis; Romero, Lawrence Steven, Aerodynamic stabilization of a projectile.
  3. King, Hartley Hughes; Menna, Thomas Louis; Romero, Lawrence Steven, Aerodynamic stabilization of a projectile.
  4. Patel, Mehul; Ng, T. Terry; Cain, Alan B.; Sowle, Zak; DiCocco, Jack, Aircraft, missile, projectile or underwater vehicle with improved control system.
  5. Patel, Mehul; Ng, T. Terry; Cain, Alan B.; Sowle, Zak; DiCocco, Jack, Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces.
  6. Patel, Mehul; Ng, T. Terry; Cain, Alan B.; Sowle, Zak; DiCocco, Jack, Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces and method of reconfiguring.
  7. Patel, Mehul; Ng, T Terry; Cain, Alan B; Sowle, Zak; DiCocco, Jack, Aircraft, missile, projectile, or underwater vehicle with reconfigurable control surfaces.
  8. Bennett, Stephen E.; Geswender, Chris E.; Greenwood, Kevin R., Boot mechanism for complex projectile base survival.
  9. Bar, Klaus; Bohl, Jurgen, Braking arrangement for a correctable-trajectory spin-stabilized artillery projectile.
  10. King, Hartley Hughes; Menna, Thomas Louis; Romero, Lawrence Steven, Deployable flare for aerodynamically stabilizing a projectile.
  11. King, Hartley Hughes; Menna, Thomas Louis; Romero, Lawrence Steven, Deployable flare for aerodynamically stabilizing a projectile.
  12. Carlyle, John Daryl; Hall, William; King, Hartley Hughes; Menna, Thomas Louis; Romero, Lawrence Steven, Deployable flare with simplified design.
  13. Dryer, Richard; Eisentraut, Rudolph Adolph; Kebschull, Martin Allen; Parine, John Christopher, Deployment mechanism for stowable fins.
  14. Martínez Valdegrama, Vicente; Lozano García, José Luis; Ramírez Blanco, Gonzalo, Device for providing electrical continuity between aeronautical components with relative movement.
  15. Tritt, Benjamin R., Fin deployment system.
  16. Johnsson, Stig; Hellman, Ulf; Holmqvist, Ulf, Fin-stabilized shell.
  17. Wik, Torsten, Method and arrangement for extending the range of fire of a fin-stabilized artillery missile.
  18. Johnsson,Stig; Hellman,Ulf; Holmqvist,Ulf, Method and arrangement for low or non-rotating artillery shells.
  19. Johnsson,Stig, Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith.
  20. Johnsson,Stig, Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith.
  21. Eisentraut, Rudolph Adolph; Kebschull, Martin Allen; Parine, John Christopher, Missile having deployment mechanism for stowable fins.
  22. August,Henry, Mortar shell ring tail and associated method.
  23. Parine, John C.; Koessler, Jeffrey H.; Gogineni, Purnachandra R.; Perez, Juan A.; Kebschull, Martin A., Single-axis fin deployment system.
  24. Olden, Thomas A.; Cavalleri, Robert; Kinsey, Jr., Lloyd E., Solid-fuel pellet thrust and control actuation system to maneuver a flight vehicle.
  25. Cohe, Patrick; Dubois, Bertrand; Moreau, Fabien, Steering section for guided munition.
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