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특허 상세정보

Method of controlling boundary layer flow

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-021/06    B64D-033/02    F02C-007/04    B64D-029/00   
출원번호 US-0262319 (2014-04-25)
등록번호 US-9789954 (2017-10-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Snell & Wilmer L.L.P.
인용정보 피인용 횟수 : 0  인용 특허 : 20
초록

An aircraft inlet comprising an annular air intake structure defined by an inner surface and an outer surface, a plurality of perforations formed in the outer surface of the aircraft inlet, a plenum chamber situated within the aircraft inlet and configured to receive air entering the plurality of perforations, and/or a plurality of sensors disposed about the outer surface of the aircraft inlet, each sensor associated with a region of the plurality of perforations. Each sensor may comprise a hot film anemometer. The aircraft inlet may further comprise a r...

대표
청구항

1. A nacelle inlet comprising: an annular air intake structure defined by an inner surface and an outer surface;a plurality of circumferential regions of perforations formed in the outer surface of the aircraft inlet;a plurality of plenum chambers situated within the aircraft inlet, wherein each plenum chamber of the plurality of plenum chambers is configured to receive air entering a respective circumferential region of perforations of the plurality of circumferential regions of perforations;a plurality of sensors disposed about the outer surface of the...

이 특허에 인용된 특허 (20)

  1. 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.
  2. Coffinberry George A. (West Chester OH). Aircraft gas turbine engine bleed air energy recovery apparatus. USP1992085137230.
  3. Meister, Juergen; Pfennig, Juergen. Boundary layer suction arrangement. USP2010117837155.
  4. Nelson Philip A. (Southampton GB2) Fisher Michael J. (Southampton GB2) Rioual Jean-Luc (Southampton GB2). Control of boundary layer flow. USP1993065222698.
  5. Syassen, Freerk. Device for reducing the aerodynamic drag of a leading surface of an aircraft. USP2014108864082.
  6. Anxionnaz Rene (8 ; RUE Nicolas Chuquet 75-Paris FR). Device for regulating and recovering the boundary layer over the surface of a body such as an aircraft in flight. USP1976043951360.
  7. Smith, Brian R.; Saddoughi, Seyed. Dual bimorph synthetic pulsator. USP2011067967258.
  8. Coffinberry George A. (West Chester OH). Gas turbine engine powered aircraft environmental control system and boundary layer bleed. USP1992095143329.
  9. Prince, Troy S.; Kolacinski, Richard; Patel, Mehul. Hierarchical closed-loop control system for aircraft, missiles and munitions. USP2012058190305.
  10. Lahti Daniel J. (Cincinnati OH) Yates David E. (Cincinnati OH) Mungur Parmanand (West Chester OH) Stockman Norbert O. (Batavia OH). Hybrid laminar flow nacelle. USP1991024993663.
  11. Cloft, Thomas G.; Wiley, Richard H.. Integral suction device with acoustic panel. USP2010087766280.
  12. Williams, Stewart W; Turner, Brian J. Laminar flow control system and suction panel for use therewith. USP2004066752358.
  13. Meyer,Pascal J. Laminar flow nacelle for an aircraft engine. USP2006057048230.
  14. Shatz Solomon (P.O. Box 523 Cupertino CA 94015). Movable sheet for laminar flow and deicing. USP1997015590854.
  15. Jain, Ashok K.. Nacelle flow assembly. USP2012108282037.
  16. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V.. Passive boundary layer bleed system for nacelle inlet airflow control. USP2014098844553.
  17. Patel, Mehul P.; DiCocco, Jack M; Prince, Troy. Reconfigurable porous technology for fluid flow control and method of controlling flow. USP2005036866233.
  18. Meister Juergen,DEX ; Pfennig Juergen,DEX ; Held Werner,DEX. Rudder assembly with a controlled boundary layer control for an aircraft. USP1999055899416.
  19. Hughes Kevin A. (San Diego CA) Shieh Chih F. (San Diego CA). Turbine engine nacelle laminar flow control arrangement. USP1994035297765.
  20. Gazdzinski Robert F.. Vehicular boundary layer control system and method. USP2000056068328.