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특허 상세정보

Integrated missile fin deployment system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/14   
미국특허분류(USC) 244/032.8 ; 244/032.4 ; 244/049 ; 244/046
출원번호 US-0080483 (1998-05-18)
발명자 / 주소
출원인 / 주소
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 within the missile body. The deflectors are mounted in a laterally displaced position from the longitudinal slots and are constrained from sliding into alignment with the slots by the presence of the folded canards. When the canards are released by the latch ...

대표
청구항

[ 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 a folded canard position within said missile body to an extended canard position extending through said associated longitudinal slot to the exterior of said missile body;a deflector associated with each longitudinal slot, said deflector being pivotably mounted...

이 특허를 인용한 특허 피인용횟수: 40

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  4. Perry, Craig; Schroeder, Richard W.; Voigt, Allan A.. Cover ejection and fin deployment system for a gun-launched projectile. USP2005046880780.
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  6. Pijaca, Thomas; Schellens, William J.. Extendable and controllable flight vehicle wing/control surface assembly. USP2003066581871.
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  11. Smith,Douglas L.; Morris,Joseph P.. Frictional roll control apparatus for a spinning projectile. USP2008087412930.
  12. Vasudevan, Srikanth; Suchy, Paul; Birch, Matthew C.. G-hardened flow control systems for extended-range, enhanced-precision gun-fired rounds. USP2015079086258.
  13. Geswender, Chris E.. Guidance control for spinning or rolling projectile. USP2013048426788.
  14. Geswender, Chris E.; Alejandro, Stevie; Vesty, Paul. Guidance control for spinning or rolling vehicle. USP2013048410412.
  15. May, Michael C.; Schroeder, Richard W.; Voigt, Allan A.; Speicher, John M.; Voigt, Che-Ram S.. Gun-launched rolling projectile actuator. USP2004066752352.
  16. Lloyd, Richard M.. Kinetic energy rod warhead with projectile spacing. USP2009127624683.
  17. Byrne,James Patrick; Thompson,Andrew. Method and apparatus for stowing and deploying control surfaces of a guided air vehicle. USP2006097100865.
  18. Eisentraut, Rudolph A.; Melkers, Edgar R.. Method for designing a deployment mechanism. USP2005086928400.
  19. Vasudevan, Srikanth; Suchy, Paul; Birch, Matthew C.. Methods for extended-range, enhanced-precision gun-fired rounds using g-hardened flow control systems. USP2017059658040.
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  23. Perini, Richard J.; Riedel, James K.; Wantuck, Michael D.. Multi-function actuator, and method of operating same. USP2004046726147.
  24. Lloyd, Richard M.. Multi-point time spacing kinetic energy rod warhead and system. USP2013048418623.
  25. Elkayam, Ami; Azar, Zeev. Munition guidance system and method of assembling the same. USP2015109157702.
  26. Corder, David A; Merems, Paul A. Passive stability system for a vehicle moving through a fluid. USP2016089429401.
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  28. Paulic, Antonio; Krass, Robert M.. Projectile having deployable fin. USP2013058438977.
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  31. Sankovic, John R.. Pyrotechnic fin deployment and retention mechanism. USP2012128338769.
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  35. Geswender, Christopher E.; Dryer, Richard; Vesty, Paul. Steerable spin-stabilized projectile. USP2014128916810.
  36. Cesaroni, Anthony Joseph. Surface skimming munition. USP2015018939084.
  37. Cesaroni, Anthony Joseph. Surface skimming munition. USP2016099448049.
  38. Ericson,Charles R.; May,Michael C.. Tandem motor actuator. USP2007087255304.
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