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Flow control device and method for aircraft and missile forebody

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/02    F42B-010/14   
출원번호 US-0615218 (2009-11-09)
등록번호 US-9429400 (2016-08-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kolkowski, Brian
인용정보 피인용 횟수 : 5  인용 특허 : 14
초록

A forebody flow control system and more particularly an aircraft or missile flow control system for enhanced maneuverability and stabilization utilizes various types of sensors and various types of activatable flow effectors to maneuver the aircraft or missile with the help of a control system. A method of operating the flow control system is also disclosed.

대표
청구항
▼

1. A flow control system for a missile or aircraft forebody comprising a. at least one activatable micro-vortex generator;b. at least one sensor generating a signal, the at least one sensor being used to maneuver the missile or aircraft;c. an inertial measurement unit having an output; andd. a closed loop control system;wherein the closed loop control system is used for activating and deactivating the at least one micro-vortex generator based at least in part on the signal of the at least one sensor and the output of the inertial measurement unit. 2. The...

이 특허에 인용된 특허 (14)

  1. Wang, Jing; McGrath, Edward Lee; Fischetti, Thomas Joseph. Actuatable surface features for wind turbine rotor blades. USP2012058167554.
  2. 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.
  3. 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.
  4. Ransom Stephen (Stuhr DEX) Relotius Klaus-Dieter (Bremen DEX). Apparatus for controlling the structural dynamic response of a rocket. USP1997015593110.
  5. Steuer Raimar (Leinburg DEX). Artillery rocket. USP1995115467940.
  6. Sebestyen George (Weston MA) Sinclair Ronald R. (Moultonboro NH) Smith John A. (Bedford MA) Sands Timothy B. (Acton MA) Nussdorfer Theodore J. (Lexington MA). Canard control assembly for a projectile. USP1985044512537.
  7. Michael Campbell. Controllable vortex generator. USP2002086427948.
  8. Abbott Anthony Steven. GPS guided munition. USP2001056237496.
  9. Smith John A. (Bedford MA) Sinclair Ronald R. (Moultonboro NH). Guidance system for a projectile. USP1986024568039.
  10. Vig John R. ; Waugh Steven W.. Guided artillery projectile and method. USP1998075775636.
  11. Bauer Andrew B. (Orange CA). Hidden vortex generators. USP1977084039161.
  12. Leininger,J체rgen. Method for correcting the flight path of ballistically fired spin-stabilised artillery ammunition. USP2007097267298.
  13. Van Dam,Cornelis P.; Yen,Dora T.; Smith,Rosemary L.; Collins,Scott D.. Microfabricated translational stages for control of aerodynamic loading. USP2006047028954.
  14. Stoy David R. (Woodland Hills CA). Separately banking maneuvering aerodynamic control surfaces, system and method. USP1994065322243.

이 특허를 인용한 특허 피인용횟수: 5

  1. Menicovich, David; Amitay, Michael; Gallardo, Daniele. Active modular aerodynamic drag reduction system. USP2018059963175.
  2. Summers, Matthew H.; Koehler, Frederick B.; Danforth, Jeremy C.; Villarreal, James K.. Base drag reduction fairing using shape memory materials. USP20190110184762.
  3. Wood, James Richard. Missile, chemical plasm steering system, and method. USP20181010113844.
  4. Sowle, Zak; Vasudevan, Srikanth; Birch, Matthew C.. Rotational control actuation system. USP20190210203188.
  5. Hegenbart, Matthias; Eilken, Wolfgang; Paul, Erich; Stefes, Bruno; Duken, Lena. Vortex generator arrangement. USP20190210202187.

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