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특허 상세정보

Three axis flap control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G06E-019/00    F42B-010/00   
미국특허분류(USC) 244/003.22; 244/003.24; 244/003.28; 244/003.29; 244/003.27
출원번호 US-0714455 (2000-11-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Swidler Berlin Shereff Friedman, LLP
인용정보 피인용 횟수 : 21  인용 특허 : 22
초록

A three axis control system employing four flaps is disclosed. The flaps are of uniform design, which decreases machining and manufacturing costs. The flaps are positioned on a vehicle orthogonally, but offset from a vehicle centerline. The system provides not only pitch and yaw control, but also bi-directional roll control with a minimum number of parts and minimal infringement of packaging envelope. The system provides quick response and increased capability for difficult maneuvers and is useable for hypersonic/supersonic applications.

대표
청구항

A three axis control system employing four flaps is disclosed. The flaps are of uniform design, which decreases machining and manufacturing costs. The flaps are positioned on a vehicle orthogonally, but offset from a vehicle centerline. The system provides not only pitch and yaw control, but also bi-directional roll control with a minimum number of parts and minimal infringement of packaging envelope. The system provides quick response and increased capability for difficult maneuvers and is useable for hypersonic/supersonic applications. blishing a direc...

이 특허에 인용된 특허 (22)

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  17. Kastenhuber Manfred (Rednitzhembach DEX) Eckel Alfred (Ireuchtlingen DEX) Bock Erich (Nuremberg DEX). Pivoting guidance mechanism for small-calibered projectiles. USP1986074600167.
  18. Minnich Violet C. (Huntsville AL). Pop-up fin. USP1976113990656.
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이 특허를 인용한 특허 피인용횟수: 21

  1. Geswender,Chris E.; Hinsdale,Andrew J.; Blaha,George A.; Dryer,Richard. 2-D projectile trajectory correction system and method. USP2007017163176.
  2. August,Henry. Aerodynamic control of a hypersonic entry vehicle. USP2007067229048.
  3. Alban, III, William H.; Johnston, Karl A.; Eiswirth, Edward A.; Morgan, David E.. Aerodynamic re-entry vehicle control with active and passive yaw flaps. USP2009117611095.
  4. 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. USP2011077977615.
  5. 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. USP2007067226015.
  6. Trosky, Bernhard; Wich, Harald; Lehmann, Lutz. Artillery rocket. USP2004026685134.
  7. Pettersson, Thomas. Brake panel for a detonator or a projectile. USP2017079702675.
  8. Olden, Thomas A.; Wrigglesworth, Walter. Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof. USP2014098826640.
  9. Fraysse, Jr., John W.. Guided fuse with variable incidence panels. USP2011098026465.
  10. Prince, Troy; Kolacinski, Richard; Patel, Mehul. Hierarchical closed-loop flow control system for aircraft, missiles and munitions. USP2013048417395.
  11. Schroeder, Wayne K.; Banks, Johnny Edward. Method and apparatus for planar actuation of a flared surface to control a vehicle. USP2004046723972.
  12. Teter, Roger D.; Dunn, Steven A.; Meyer, J. William. Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy. USP2010057721997.
  13. Teter,Roger D.; Dunn,Steven A.; Meyer,J. William. Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy. USP2007097267303.
  14. Teter, Roger D.; Dunn, Steven; Barczi, Kenneth. Methods and apparatus for driving rotational elements of a vehicle. USP2013058434712.
  15. Teter, Roger D.; Dunn, Steven; Barczi, Kenneth. Methods and apparatus for varying a trim of a vehicle. USP2013068466397.
  16. Lyman, Ward D.; Koehler, Frederick B.; Sanderson, Terry M.. Shape memory alloy micro-aero control surfaces. USP2018019879959.
  17. Olden, Thomas A.; Cavalleri, Robert; Kinsey, Jr., Lloyd E.. Solid-fuel pellet thrust and control actuation system to maneuver a flight vehicle. USP2012068193476.
  18. Tyree, Anthony K.. System and method for navigating an object. USP2013088502126.
  19. Meyer,J. W.. System and method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping. USP2007077237752.
  20. Olden, Thomas A.; Wrigglesworth, Walter. Systems and methods for composite structures with embedded interconnects. USP2014088809689.
  21. Rutan,Elbert L.. Winged spacecraft. USP2007037195207.