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특허 상세정보

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

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-021/00   
출원번호 US-0457686 (2012-04-27)
등록번호 US-9637223 (2017-05-02)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kolkowski, Brian
인용정보 피인용 횟수 : 2  인용 특허 : 16
초록

An afterbody flow control system is used for aircraft or missile flow control to provide enhanced maneuverability and stabilization. A method of operating the flow control system is also described. The missile or aircraft comprises an afterbody and a forebody; at least one activatable flow effector on the missile or aircraft afterbody; at least one sensor having a signal, the at least one sensor being positioned to detect forces or flow conditions on the missile or aircraft afterbody; and a closed loop control system; wherein the closed loop control syst...

대표
청구항

1. A missile or aircraft comprising: an afterbodya forebody andat least one sensor having an electrical signal;the missile or aircraft afterbody having a boattail andtail fins;the missile or aircraft experiencing drag during flight; andat least one electromechanical activatable flow effector or electromechanical active flow control device on the boattail or tail fins,wherein the at least one sensor is positioned to measure, estimate or predict a force or flow condition the missile or aircraft's afterbody, the at least one electromechanical activatable fl...

이 특허에 인용된 특허 (16)

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  5. Dong Yang (Cleveland Heights OH) Chizeck Howard J. (Cleveland Heights OH) Khoury James M. (Strongsville OH) Schmidt Robert N. (Cleveland OH). Extended horizon adaptive block predictive controller with an efficient prediction system. USP1995065424942.
  6. Bennett John A. (Marietta GA) Englar Robert J. (Marietta GA) Thomas Andrew S. W. (Marietta GA). Fluid flow control device. USP1988044736913.
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  8. Miller, Paul A.; Aragon, Ben P.. Method for generating surface plasma. USP2003056570333.
  9. Samad Tariq. Nonlinear-approximator-based automatic tuner. USP1998125847952.
  10. Waymeyer Walter K. (LaVerne CA) Banach Timothy P. (Chino CA). Roll damper for thrust vector controlled missile. USP1993115259569.
  11. Enloe,Carl L.; McLaughlin,Thomas E.; Jumper,Eric J.; Corke,Thomas C.. Single dielectric barrier aerodynamic plasma actuation. USP2008067380756.
  12. Bandyopadhyay Promode R.. Surface layer comprising micro-fabricated tiles for electromagnetic control of fluid turbulence in sea water. USP1998085791275.
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  14. Blackburn Ronald F. ; Warmkessel Barry M. ; Kawamoto Sonja M.. System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion. USP1998085797563.
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