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Integrated missile fin deployment system

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F42B-010/14
출원번호 US-0080483 (1998-05-18)
발명자 / 주소
  • Voigt Allan A.
  • Speicher John M.
출원인 / 주소
  • Versatron, Inc.
대리인 / 주소
    Bissell
인용정보 피인용 횟수 : 40  인용 특허 : 7

초록

Pairs of aerofins used for stabilization and control of missile flight are deployed through shared longitudinal slots provided in the missile body. Before launch, the pairs of aerofins, each pair comprised of a canard and a deflector, are retained in a folded position by a releasable latch mechanism

대표청구항

[ What is claimed is:] [1.] An integrated aerofin release system for a missile comprising:a missile body having a plurality of longitudinal slots formed therein;a canard associated with each longitudinal slot, said canard being pivotably mounted within said missile body and capable of rotation from

이 특허에 인용된 특허 (7)

  1. Goulding Kenneth (Stevenage GB2), Deployment and actuation mechanisms.
  2. Wedertz Larry D. (Mira Loma CA), Double swing wing self-erecting missile wing structure.
  3. Speicher John M. ; Voigt Che-Ram S. ; Perry Craig D. ; Voigt Allan A., Fin lock mechanism.
  4. Myers Glenn G. (Mission Viejo CA), Folding wing structure with a flexible cover.
  5. Niemeier Byron M. (Claremont CA), Mechanical roll rate stabilizer for a rolling missile.
  6. Ullrich Hans-Gunter,DEX, Vane control system for a guided missile.
  7. Unterstein Klaus (Duesseldorf DEX), Wing deploying system comprising an airbag.

이 특허를 인용한 특허 (40)

  1. Geswender,Chris E.; Hinsdale,Andrew J.; Blaha,George A.; Dryer,Richard, 2-D projectile trajectory correction system and method.
  2. Schroppel Werner,DEX ; Dommer Josef,DEX, Adjusting apparatus for control surfaces of a missile.
  3. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L., Asymmetrical control surface system for tube-launched air vehicles.
  4. Perry, Craig; Schroeder, Richard W.; Voigt, Allan A., Cover ejection and fin deployment system for a gun-launched projectile.
  5. Dodu,Ren?; Dion,Dominique, Deployment and drive device for projectile control surfaces.
  6. Pijaca, Thomas; Schellens, William J., Extendable and controllable flight vehicle wing/control surface assembly.
  7. Allan A. Voigt ; Che-Ram S. Voigt ; John S. Speicher ; Charles R. Ericson, Fin and cover release system.
  8. Black, Thomas A.; Reyes, David J.; Von Mayr, Robert W.; Fjerstad, Erik A.; Willems, John D., Fin buzz system and method for assisting in unlocking a missile fin lock mechanism.
  9. Osdon, Tal, Fin deployment system.
  10. Schroeder,Richard W., Fin retention and deployment mechanism.
  11. Smith,Douglas L.; Morris,Joseph P., Frictional roll control apparatus for a spinning projectile.
  12. Vasudevan, Srikanth; Suchy, Paul; Birch, Matthew C., G-hardened flow control systems for extended-range, enhanced-precision gun-fired rounds.
  13. Geswender, Chris E., Guidance control for spinning or rolling projectile.
  14. Geswender, Chris E.; Alejandro, Stevie; Vesty, Paul, Guidance control for spinning or rolling vehicle.
  15. May, Michael C.; Schroeder, Richard W.; Voigt, Allan A.; Speicher, John M.; Voigt, Che-Ram S., Gun-launched rolling projectile actuator.
  16. Lloyd, Richard M., Kinetic energy rod warhead with projectile spacing.
  17. Byrne,James Patrick; Thompson,Andrew, Method and apparatus for stowing and deploying control surfaces of a guided air vehicle.
  18. Eisentraut, Rudolph A.; Melkers, Edgar R., Method for designing a deployment mechanism.
  19. Vasudevan, Srikanth; Suchy, Paul; Birch, Matthew C., Methods for extended-range, enhanced-precision gun-fired rounds using g-hardened flow control systems.
  20. Vasudevan, Srikanth; Suchy, Paul; Birch, Matthew C., Methods for extended-range, enhanced-precision gun-fired rounds using g-hardened flow control systems.
  21. Vasudevan, Srikanth; Suchy, Paul; Birch, Matthew C., Methods for extended-range, enhanced-precision gun-fired rounds using g-hardened flow control systems.
  22. Sankovic,John; Byrne,James; Piltz,Daniel, Missile fin locking method and assembly.
  23. Perini, Richard J.; Riedel, James K.; Wantuck, Michael D., Multi-function actuator, and method of operating same.
  24. Lloyd, Richard M., Multi-point time spacing kinetic energy rod warhead and system.
  25. Elkayam, Ami; Azar, Zeev, Munition guidance system and method of assembling the same.
  26. Corder, David A; Merems, Paul A, Passive stability system for a vehicle moving through a fluid.
  27. Scott, Aaron M., Perpendicular drive mechanism for a missile control actuation system.
  28. Paulic, Antonio; Krass, Robert M., Projectile having deployable fin.
  29. Corradini, John, Projectile that includes a fin adjustment mechanism with changing backlash.
  30. Morris,Joseph P.; Smith,Douglas L., Projectile trajectory control system.
  31. Sankovic, John R., Pyrotechnic fin deployment and retention mechanism.
  32. Sankovic, John R., Pyrotechnic fin deployment and retention mechanism.
  33. Sankovic, John R., Pyrotechnic fin deployment and retention mechanism.
  34. Lutzenberger, Joerg; Kaebitz, Bernd; Kroyer, Robert, Rudder system.
  35. Geswender, Christopher E.; Dryer, Richard; Vesty, Paul, Steerable spin-stabilized projectile.
  36. Cesaroni, Anthony Joseph, Surface skimming munition.
  37. Cesaroni, Anthony Joseph, Surface skimming munition.
  38. Ericson,Charles R.; May,Michael C., Tandem motor actuator.
  39. Rogers, Thomas R., Techniques for controlling access through a slot on a projectile.
  40. Teter, Roger D.; Kudlick, Dean A.; Williams, Richard M., Three axis flap control system.
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