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Flow control device to eliminate cavity resonance 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-021/06
출원번호 US-0183812 (1997-12-19)
발명자 / 주소
  • Hebert Leonard J.
  • Miller Wendell R.
  • Nesbitt Eric H.
  • Piro Jerry
  • Sangwin Michael L.
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Christensen O'Connor Johnson Kindness PLLC
인용정보 피인용 횟수 : 27  인용 특허 : 11

초록

A flow control device and method for eliminating flow-induced cavity resonance within a closed or nearly closed end flow passage (20) having an inlet opening (30) defined between an upstream inlet edge (32) and a downstream inlet edge (34). The passage accepts exterior fluid flow (38) therein via th

대표청구항

[ The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:] [1.] A system for eliminating flow-induced cavity resonance comprising:(a) a closed or nearly closed end fluid flow passage having an inlet with an opening defined between an upstream i

이 특허에 인용된 특허 (11)

  1. Lord Thomas J. (Dayton OH), Air inlet control for aircraft or the like.
  2. Haslund Ralph L. (Mercer Island WA), Apparatus and method for providing an aero-optical interface.
  3. Maurer Otto F. (Dayton OH), Device to reduce flow induced pressure oscillations in open cavities.
  4. Raisbeck James D. (Seattle WA), Dual turning vane air inlet assembly.
  5. Lidstone Gary L. ; Clark Larry T. ; Szupkay Imre A. ; Sandquist David L., Engine noise suppression ejector nozzle.
  6. Mohn Larry W. (Edmonds WA), Flow deflector for fluid inlet.
  7. Vanderleest Siebold (Seattle WA), Scoop and inlet for auxiliary power units and method.
  8. Brown William H. (West Chester OH), Sound suppression mixer.
  9. Frantz John J. (Fairfield OH), Variable double lip quiet inlet.
  10. Osborn Melvin N. (Los Angeles CA), Variable shape, fluid flow nozzle for sound suppression.
  11. Mazzitelli Frederick (Redmond WA), Vortex generators for inlets.

이 특허를 인용한 특허 (27)

  1. Kelnhofer,Juergen; Petrac,Marcus; Buchholz,Uwe, Air discharge valve for an aircraft.
  2. Kastell, Dirk; Roering, Sebastian; Noriega, Wilson Willy Casas, Air duct for supplying ambient air in an aircraft.
  3. Alvarez, Franck; Chancerelle, Emeric; Porte, Alain; Prat, Damien, Air intake arrangement for a vehicle, in particular an aircraft.
  4. Kelnhofer,Juergen, Aircraft ram air inlet with multi-member closure flap.
  5. Stanek Michael J., Aircraft weapons bay acoustic suppression apparatus.
  6. Tretow, Paul R.; Willie, Robert Henry; Robinson, Donald Edwin, Angled inlet system for a precooler.
  7. Tretow, Paul R.; Chambers, David S.; Willie, Robert H., Auxiliary power unit inlet apparatus and methods.
  8. Mårtensson, Hans; Nilsson, Martin, Bleed structure for a bleed passage in a gas turbine engine.
  9. Mårtensson, Hans; Nilsson, Martin, Bleed structure for a bleed passage in a gas turbine engine.
  10. Laurant, Franck; Bellet, Francois; Joret, Jean-Philippe, Composite panel having a built-in duct.
  11. Dussillols, Laurent; Vuillemin, Alexandre Alfred Gaston, Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraft.
  12. Sheoran, Yogendra Y.; Michalski, Jr., Joseph W.; Asplund, Kyle D., Diffusing air inlet door assembly.
  13. Willie, Robert Henry; Tretow, Paul R., Dual inlets for a turbofan precooler.
  14. Conner,Steven L., Engine airframe J-seal damper.
  15. Bolender, Lars; Wagnon, Sébastien, Engine intake flap for being arranged on the housing of an air intake of an aircraft engine, as well as engine with such an engine intake flap and aircraft system.
  16. Zysman, Steven H., Nacelle scoop inlet.
  17. Bifulco, Anthony R., Non-metallic engine case inlet compression seal for a gas turbine engine.
  18. Tanner, Justin A.; Kang, Albert; Gentile, David P.; Facinelli, Bill; Jones, Kevin, Outflow valve having flexible bellmouth and cabin pressure control system employing the same.
  19. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V., Passive boundary layer bleed system for nacelle inlet airflow control.
  20. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V., Passive boundary layer bleed system for nacelle inlet airflow control.
  21. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V., Passive boundary layer bleed system for nacelle inlet airflow control.
  22. Bouldin, Bruce Dan; Kowal, Adam; Doras, Vincent; Robbins, Robert; Lyells, Jim, Ram door assemblies.
  23. Kelnhofer, Juergen, Relief valve for being arranged on an opening of a fuselage shell of an aircraft, fuselage part with such a relief valve and aircraft fuselage.
  24. Wayne T. Bliesner, Tailored wing assembly for an aircraft moveable slat system.
  25. Winkler, Chad M; Wright, Matthew J, Variable area flow duct employing secondary flows, and method therefor.
  26. Dussillols, Laurent Christophe; Longeville, Olivier Roland; Vuillemin, Alexandre Alfred Gaston, Variable-section flow mixer for a double-flow turbojet for a supersonic airplane.
  27. Hussain, Zahid M., Ventilation inlet.
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