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특허 상세정보

Gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/32   
미국특허분류(USC) 60/3907 ; 60/39092 ; 55/306 ; 417/196
출원번호 US-0157942 (1988-02-19)
우선권정보 GB-0008859 (1987-04-14)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 26  인용 특허 : 4
초록

The invention relates to turbopropeller gas turbine engines of the type which have a propeller positioned upstream of the gas generator. Intake openings supply air through intake ducts and annular intake duct to the gas generator. A separating duct removes foreign bodies from the air flowing through an outlet. The separating duct has a plurality of ejector nozzles equi-spaced in the wall of the duct. The ejector nozzles induce a flow through the separating duct to draw the foreign bodies through the separating duct. The separating duct allows the passage...

대표
청구항

A turbopropeller gas turbine engine comprising at least one propeller, a gas generator, and intake means, the at least one propeller being positioned upstream of the gas generator, the gas generator comprising a compressor and a gas generator casing, the intake means supplying air to the gas generator being positioned downstream of the at least one propeller, the intake means comprising at least one intake opening formed in the gas generator casing and an associated inlet duct extending from the intake opening to the gas generator, the intake duct includ...

이 특허를 인용한 특허 피인용횟수: 26

  1. Negulescu, Dimitrie; Mundt, Christian. Air intake system of a propeller-turbine engine. USP2004116817572.
  2. Duge, Robert T.. Air particle separator. USP2017019541003.
  3. Chamay Anthony J. ; Zelazny Isaac,KRX. Aircraft engine pitot plenum intake. USP1998035725180.
  4. Chamay Anthony J. ; Zelazny Isaac,KRX. Aircraft intake method. USP1999055906334.
  5. Addis, Mark. Aircraft propulsion systems. USP2010077752834.
  6. Brault, Michel Gilbert; Brossier, Pascal Noel. Bleed system driven in simplified manner for a turbojet or turboprop engine. USP2003096622475.
  7. Wagner, Joel H.; Magge, Shankar S.; Santeler, Keith A.. Centrifugal compressor with bleed flow splitter for a gas turbine engine. USP2015018935926.
  8. Danielson, David R.; Carvalho, Paul A.; Raes, Mark; Perkinson, Robert H.. Counter-rotating open-rotor (CROR). USP2017089718536.
  9. Talasco, Eric J.; Carvalho, Paul A.; Danielson, David R.; Perkinson, Robert H.. Counter-rotating open-rotor (CROR). USP2015069051044.
  10. Richards, Martyn. Engine. USP2011027891163.
  11. Youssef, Nashed. Gas turbine aircraft engine with power variability. USP2012058181442.
  12. Chanez, Philippe Gerard; Mabboux, Gaetan Jean; Minot, Philippe Gilles; Vincent, Thomas Alain Christian; Yvon, Didier Jean-Louis. Gas turbine engine air intake in a nacelle. USP2015079091207.
  13. Urban, Justin R.; Bifulco, Anthony R.. Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events. USP2018029890711.
  14. Suciu, Gabriel L.; Epstein, Alan H.; Lord, Wesley K.; Chandler, Jesse M.. Gas turbine engine with cooling scheme for drive gear system and pitch control. USP2018039909504.
  15. Bouchard,Guy; Szlanta,Zenon; Mitrovic,Lazar. Hybrid inlet. USP2006016990798.
  16. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Low noise aeroengine inlet system. USP2018059957889.
  17. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Low noise aeroengine inlet system. USP2018049951690.
  18. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Low noise aeroengine inlet system. USP20180810054050.
  19. Hall Edward J. ; Meade Joseph P.. Method for reducing turboprop noise. USP1999105961067.
  20. Snyder, Philip H.; Vittal, Baily. Particle separator. USP2003016508052.
  21. Martel, Alain C.; Gekht, Eugene. Particle separator and separating method for gas turbine engine. USP2012018092145.
  22. Philip H. Snyder. Particle separator for a gas turbine engine. USP2002126499285.
  23. Snyder, Philip H.. Particle separator for a turbine engine. USP2004036698180.
  24. Kumar, Anurag; Pritchard, Byron Andrew; Tan, Chiong Siew. System for extracting matter through variable bleed valves in turbines. USP2017049623354.
  25. Van Der Woude, Matthijs. Turboprop engine with an apparatus for the generation of a cooling airflow. USP2012108276392.
  26. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Variable geometry inlet system. USP20190310221764.