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특허 상세정보

MEMS control surface for projectile steering

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01    F42B-015/00   
미국특허분류(USC) 244/003.21; 244/099.8
출원번호 UP-0268401 (2005-11-01)
등록번호 US-7628352 (2009-12-16)
발명자 / 주소
대리인 / 주소
    Zimmerman, Fredric J.
인용정보 피인용 횟수 : 2  인용 특허 : 28
초록

A projectile includes a projectile body including a flow surface; the flow surface including at least one control surface formed therein. The controls surface is formed continuous with the flow surface, and a pressure source is connected to at least one control surface. The pressure source delivers a pressure to at least one control surface to cause at least one control surface to bulge away from the flow surface.

대표
청구항

What is claimed is: 1. A projectile, comprising: a projectile body including a flow surface forming the outer skin of the projectile body; the flow surface including at least one control surface formed therein, wherein said at least one control surface is formed continuous and integrated with the flow surface, a thickness of said at least one control surface is less than a thickness of the flow surface; and a pressure source connected to said at least one control surface, the pressure source delivering pressurized fluid to said at least one control sur...

이 특허에 인용된 특허 (28)

  1. Prince, Troy; Lisy, Frederick J.; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N.. Aircraft and missile forebody flow control device and method of controlling flow. USP2004026685143.
  2. Rauckhorst ; III Richard L. (North Canton OH). Compressible nose dynamic de-icer. USP1994055314145.
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  4. Crist, James; Putt, James; Sluss, Terry. Deicer for aircraft. USP2003026520452.
  5. Lisy Frederick J. ; Schmidt Robert N.. Deployable flow control device. USP2000086105904.
  6. O'Dwyer, James Michael. Directional control of missiles. USP2005056889935.
  7. Schroeder Wayne K. (Arlington TX). Dual-control scheme for improved missle maneuverability. USP1997055631830.
  8. Hakenesch Peter,DEX. Fuselage nose for controlling aerodynamic vehicles and method of utilizing same. USP2001096283407.
  9. Dockter, Gregory E.; Hamilton, Brian K.. Geometric morphing wing. USP2005066910661.
  10. Dockter, Gregory E.; Hamilton, Brian K.. Geometric morphing wing with layers. USP2004096786457.
  11. Jay Lipeles ; R. Glenn Brosch. Guided bullet. USP2002116474593.
  12. DiChiara, Jr., Robert A.; French, Robert E.; Thatcher, Conley Siddoway; Zadorozny, Edward A.; Hogenson, Peter A.. High temperature resistant airfoil apparatus for a hypersonic space vehicle. USP2004016676077.
  13. Robert A. DiChiara, Jr. ; Robert E. French ; Conley Siddoway Thatcher ; Edward A. Zadorozny ; Peter A. Hogenson. Hot ruddervator apparatus and method for an aerospacecraft. USP2002076419189.
  14. Norbert A. Weisend, Jr.. Inflatable airfoil device. USP2002096443394.
  15. Scott Harry A. (Hawthorne CA). Integral structure and thermal protection system. USP1992105154373.
  16. John, Lawrence E.. Low mass flow reaction jet. USP2004066752351.
  17. Briscoe James A. (Doylestown OH) Putt James C. (Doylestown OH) Phillips ; II Ronald W. (Mogadore OH). Method and apparatus for deicing a leading edge. USP1989094865291.
  18. Rastegar, Jahangir S.; Pelz, Richard B.. Methods and apparatus for increasing aerodynamic performance of projectiles. USP2005086935242.
  19. Rastegar, Jahangir S.; Pelz, Richard B.. Methods and apparatus for increasing aerodynamic performance of projectiles. USP2004046727485.
  20. Millett ; Dennis A.. Pneumatic actuator system and method. USP1978024075930.
  21. Kageorge Pedro W. (Cuyahoga Falls OH). Pneumatic deicers with inextensible threads. USP1987084687159.
  22. Folsom,Mark; Piper, III,Charles; Fahey,Wm. David; McGowan,Jared M.. Projectile diverter. USP2006027004423.
  23. Mark Folsom ; Charles Piper, III ; Wm. David Fahey ; Jared M. McGowan. Projectile diverter. USP2002046367735.
  24. Robert William Hyde ; Thomas Steve Betchel ; Guy Neil Shemwell ; James Hobart Crist. Radome deicer. USP2002086439505.
  25. Pinson George T. (Huntsville AL). Resiliently deployable fairing for sealing an airframe cavity. USP1989064838502.
  26. Leffel Kevin L. (Akron OH) Putt James C. (Doylestown OH) Rauckhorst Richard L. (North Canton OH). Structural airfoil having integral expulsive system. USP1994025288355.
  27. Rauckhorst ; III Richard L. (North Canton OH). Vibrating pneumatic deicing system. USP1996105562265.
  28. Ng T. Terry. Vortex generation for control of the air flow along the surface of an airfoil. USP2001106302360.