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특허 상세정보

Aircraft and missile forebody flow control device and method of controlling flow

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01   
미국특허분류(USC) 244/00324; 244/0760C; 244/091
출원번호 US-0800606 (2007-05-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Brian M., Kolkowski
인용정보 피인용 횟수 : 3  인용 특허 : 23
초록

A forebody flow control system and more particularly to aircraft or missile flow control systems for enhanced maneuverability and stabilization at high angles of attack. The present invention further relates to a method of operating the flow control system. In one embodiment, the present invention includes a missile or aircraft comprising an afterbody and a forebody; at least one flow effector on the missile or aircraft forebody; at least one sensor having a signal associated therewith, the at least one sensor being positioned to detect flow separation o...

대표
청구항

What is claimed: 1. A missile or aircraft comprisinga. an afterbody and a forebody;b. at least one flow effector used to assist in reattachment of airflow on the missile or aircraft forebody;c. at least one sensor having a signal associated therewith, the at least one sensor being positioned to detect flow separation or side forces on the missile or aircraft forebody; andd. a closed loop control system;

이 특허에 인용된 특허 (23)

  1. Murri Daniel G. (Grafton VA). Actuated forebody strakes. USP1990044917333.
  2. Zell Peter T. (San Jose CA). Aerodynamic surface distension system for high angle of attack forebody vortex control. USP1994075326050.
  3. DiCocco,Jack; Prince,Troy; Patel,Mehul; Ng,Tsun Ming Terry. Aircraft and missile afterbody flow control device and method of controlling flow. USP2006077070144.
  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. USP2004026685143.
  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. Ransom Stephen (Stuhr DEX) Relotius Klaus-Dieter (Bremen DEX). Apparatus for controlling the structural dynamic response of a rocket. USP1997015593110.
  7. Cheung, Ken C. K.; Sullivan, Christopher J.. Conformable skin element system for active vortex control. USP2009087578483.
  8. Lisy Frederick J. ; Schmidt Robert N.. Deployable flow control device. USP2000086105904.
  9. Peters ; Jr. Spence E. (Fort Worth TX). Flight control device to provide directional control. USP1993045201829.
  10. Lisy, Frederick J.; Modarreszadah, Mohammed; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N.; Prince, Troy. Flow control device and method of controlling flow. USP2005016837465.
  11. Schmidt Robert N. ; Shaw Greg S.. Fluid flow control devices. USP1998055755408.
  12. Hakenesch Peter,DEX. Fuselage nose for controlling aerodynamic vehicles and method of utilizing same. USP2001096283407.
  13. Peckham Derek H. (Farnham GBX). Guided missiles. USP1992085139215.
  14. Katz Richard A. (East Lyme CT). Method and system for identifying the onset of a turbulent boundary layer induced by a body moving through a fluid mediu. USP1994065319608.
  15. Meng James C. S.. Method for controlling microturbulence. USP1999045890681.
  16. Todd G. Wetzel ; Sandra F. Feldman. Optical tuft for flow separation detection. USP2002046380535.
  17. Stoy David R. (Woodland Hills CA). Separately banking maneuvering aerodynamic control surfaces, system and method. USP1994065322243.
  18. Gongwer, Calvin A.. Spherical vehicle for operation in a fluid medium. USP1983034377982.
  19. Komerath Narayanan M. ; Darden Leigh Ann ; Magill John C. ; Peterson Kevin G.. Stagnation point vortex controller. USP1998085794887.
  20. Farokhi Saeed (Lawrence KS) Taghavi Ray R. (Lawrence KS). Supersonic vortex generator. USP1997025598990.
  21. Malmuth, Norman; Fedorov, Alexander. Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow. USP2004106805325.
  22. Teter, Roger D.; Kudlick, Dean A.; Williams, Richard M.. Three axis flap control system. USP2003016502785.
  23. Rao Dhanvada M. (Hampton VA) Murri Daniel G. (Grafton VA). Yaw and pitch control of air vehicles at high angles of attack. USP1988114786009.