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특허 상세정보

Method and apparatus for controlling aircraft inlet air flow

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/02   
미국특허분류(USC) 244/053.B; 137/015.1
출원번호 US-0044518 (2002-01-11)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 15  인용 특허 : 11
초록

Methods and apparatus for controlling aircraft inlet air flow. The apparatus can include an external flow surface having a forward portion, and an engine inlet positioned at least proximate to the external flow surface and aft of the forward portion. The engine inlet can have an aperture and can be coupled with an engine inlet duct to an engine location. An auxiliary flow duct can be positioned at least proximate to the external flow surface and can include a first opening and a second opening spaced apart from the first opening. The first opening can be...

대표
청구항

Methods and apparatus for controlling aircraft inlet air flow. The apparatus can include an external flow surface having a forward portion, and an engine inlet positioned at least proximate to the external flow surface and aft of the forward portion. The engine inlet can have an aperture and can be coupled with an engine inlet duct to an engine location. An auxiliary flow duct can be positioned at least proximate to the external flow surface and can include a first opening and a second opening spaced apart from the first opening. The first opening can be...

이 특허를 인용한 특허 피인용횟수: 15

  1. Mores, Sebastian; Loeser, Frank; Probst, Stefan; Matt, Michael. Aircraft with an air intake for an air breathing propulsion engine. USP2017089731831.
  2. Owens, Lewis R.; Allan, Brian G.. Boundary-layer-ingesting inlet flow control system. USP2010087784732.
  3. Cloft, Thomas G.; Wall, Sarah M.. Flow distribution system for inlet flow control. USP2010057708230.
  4. Leblanc, Andr?. Gas turbine inlet flow straightener. USP2005116959552.
  5. Ruiz, Carlos G.; Gebert, Glenn A.. Hybrid (pitot-flush) air intake system for air-breathing missiles and aircraft. USP2015069056670.
  6. Cloft, Thomas G.; Wiley, Richard H.. Integral suction device with acoustic panel. USP2010087766280.
  7. Cloft, Thomas G.; Wiley, Richard H.. Integral suction device with acoustic panel. USP2013068459597.
  8. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2005096938854.
  9. Parikh, Pradip G.. Passive removal of suction air for laminar flow control, and associated systems and methods. USP2011017866609.
  10. Chase, James D.; Garzon, German Andres. Supersonic aircraft jet engine. USP2010117837142.
  11. Surply, Thierry; Bourdeau, Christophe. Turbojet nacelle and method for controlling separation in a turbojet nacelle. USP2014028640986.
  12. Huynh, Thuy; Werner, Eric. Variable geometry flush boundary diverter. USP2018019862482.
  13. Bagnall, Adam M. Variable position intake for an aircraft mounted gas turbine engine. USP2005096945494.
  14. Bagnall,Adam M. Variable position intake for an aircraft mounted gas turbine engine. USP2006037014145.
  15. Suciu, Gabriel L.; Chandler, Jesse M.; Lord, Wesley K.. Wide fuselage aircraft with increased boundary layer ingestion. USP2017049611034.