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특허 상세정보

Self stabilizing sonic inlet

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/02   
미국특허분류(USC) 137/151 ; 244/53B
출원번호 US-0891244 (1978-03-29)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 26  인용 특허 : 0
초록

There is disclosed an air inlet for a turbine engine suitable for use on a short takeoff and landing (STOL), a vertical takeoff and landing (VTOL) or a conventional takeoff and landing (CTOL) type of aircraft. A critical region in which critical flow occurs under certain conditions communicates with a less critical region of lower static pressure. Air is drawn away from the critical region and reinjected into the air flow at the less critical region. In one embodiment a circumferentially extended slot is provided in the inner surface of the air inlet at ...

대표
청구항

An air inlet for an aircraft turbine engine, said inlet being an annular body having inner and outer annular surfaces with an annular lip at its foreward end and a throat downstream of said lip, the minimum diameter of said throat lying on a plane perpendicular to the axis of said inlet diffuser, the improvement comprising: a circumferential plenum chamber formed in said diffuser around said throat; a primary aperture formed in said inner annular surface downstream of the plane of said throat at the windward side of said inlet in communication with said ...

이 특허를 인용한 특허 피인용횟수: 26

  1. Rolston Stephen C.,GBX ; Ashford Edward M.,GB5. Aerodynamic low drag structure. USP1998045743488.
  2. Silkey, Joseph S.; Wilson, Christopher D.; Dyer, Richard S.. Air induction control. USP2011077975961.
  3. Boulet, Nicolas; Affortit, Sébastien. Air inlet for aircraft propulsion unit having a structure resistant to excess pressure and a process for repairing an air inlet of an aircraft propulsion unit. USP2015069061769.
  4. Chelin, Frédéric; Surply, Thierry; Bourdeau, Christophe. Air outlet system for aircraft leading edge. USP2013058434724.
  5. Porte, Alain; Chene, Gilles; Hormiere, Arnaud. Aircraft nacelle including hot air discharge means. USP2013058448901.
  6. Jaw, Link C.. Engine stall and distortion suppression system. USP2003026519943.
  7. Link C. Jaw. Engine stall and distortion suppression system. USP2002086438960.
  8. Cloft, Thomas G.; Wall, Sarah M.. Flow distribution system for inlet flow control. USP2010057708230.
  9. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014098844294.
  10. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2013018353164.
  11. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014058726632.
  12. Prasad, Dilip; Feng, Jinzhang; Sabnis, Jayant S.. Gas turbine engine inlet with noise reduction features. USP2012108286654.
  13. Winter, Michael; Jain, Ashok K.. Gas turbine engine system providing simulated boundary layer thickness increase. USP2012078209953.
  14. Leblanc, Andr?. Gas turbine inlet flow straightener. USP2005116959552.
  15. 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.
  16. Silkey, Joseph S.; Wilson, Christopher D.; Dyer, Richard S.. Inlet distortion and recovery control system. USP2009127637455.
  17. Jain, Ashok K.; Winter, Michael. Nacelle assembly having inlet airfoil for a gas turbine engine. USP2013048408491.
  18. Haas, Martin. Nacelle assembly having inlet bleed. USP2012068192147.
  19. Haas, Martin. Nacelle assembly with turbulators. USP2012058186942.
  20. Jain, Ashok K.. Nacelle flow assembly. USP2013128596573.
  21. Jain, Ashok K.. Nacelle flow assembly. USP2012108282037.
  22. Jain, Ashok K.. Nacelle flow assembly. USP2015049004399.
  23. Atassi, Oliver V.. Nacelle with porous surfaces. USP2015038974177.
  24. Harm Dorson J. (Seattle WA) Zabinsky Joseph M. (Bellevue WA). Translating lip aircraft cowling structure adapted for noise reduction. USP1991055014933.
  25. Jain, Ashok K.. Variable geometry nacelle assembly for a gas turbine engine. USP2012068205430.
  26. Jain, Ashok K.; Chaudhry, Zaffir A.. Variable shape inlet section for a nacelle assembly of a gas turbine engine. USP2013038402739.