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특허 상세정보

Methods and apparatus for operating gas turbine engines

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/34    F02K-001/00    F02K-001/40   
미국특허분류(USC) 060/204; 060/262; 060/264; 181/213; 181/220; 239/265.17
출원번호 US-0810142 (2004-03-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Armstrong Teasdale LLP
인용정보 피인용 횟수 : 20  인용 특허 : 13
초록이 없습니다.
대표청구항이 없습니다

이 특허를 인용한 특허 피인용횟수: 20

  1. Huber, Jerome; Bonnet, Jean Paul; Gomes, Luis; Maury, Remy. Aircraft jet engine comprising a system for reducing the noise generated by the ejection of the gases. USP2015109151244.
  2. Feuillard,Philippe; Hemeury,Philippe; Gerri,Christian. Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle. USP2008127469529.
  3. Bodard, Guillaume; Vuillemin, Alexandre Alfred Gaston. Device for reducing the noise emitted by the jet of an aircraft propulsion engine. USP2016089422887.
  4. Huber, Jerome; Bonnet, Jean-Paul; Delville, Joel; Jordan, Peter; Strekowski, Francois. Device with plane jets for reducing the noise generated by an aircraft engine. USP2012038132756.
  5. Morvant, Romuald. Exhaust cone. USP2015069062610.
  6. Alhatim, Omair M.. Exhaust nozzle of a gas turbine engine. USP2016039297334.
  7. Mengle, Vinod G.. Jet engine nozzle exit configurations and associated systems and methods. USP2011067966824.
  8. Mengle, Vinod G.. Jet engine nozzle exit configurations and associated systems and methods. USP2013088511090.
  9. Mengle, Vinod G.; Thomas, Russell H.. Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods. USP2012048157207.
  10. Chase, James D.; Garzon, German Andres. Jet nozzle plug with varying, non-circular cross sections. USP2013028371124.
  11. Oishi, Tsutomu; Oba, Yoshinori. Noise reducing device and jet propulsion system. USP2014128904795.
  12. Tanaka, Nozomi; Kusuda, Shinya; Oishi, Tsutomu; Oba, Yoshinori. Noise reduction system. USP2016129528468.
  13. Tanaka, Nozomi; Kusuda, Shinya; Oishi, Tsutomu; Oba, Yoshinori. Noise reduction system with chamber. USP2014088813907.
  14. Reba, Ramons Andris; Wake, Brian Ernest; Narayanan, Satish; Maeder, Thierry. Serrated nozzle trailing edge for exhaust noise suppression. USP2009067543452.
  15. Alhatim, Omair M.. System of support thrust from wasted exhaust. USP2018019879636.
  16. Birch, Stanley F.; Secundov, Alexander N.; Lyubimov, Dmitriy A.; Khritov, Konstantin M.; Maslov, Vladimir P.; Mironov, Aleksey K.. Systems and methods for passively directing aircraft engine nozzle flows. USP2011017870722.
  17. Birch, Stanley F.; Secundov, Alexander N.; Lyubimov, Dmitriy A.; Khritov, Konstantin M.; Maslov, Vladimir P.; Mironov, Aleksey K.. Systems and methods for passively directing aircraft engine nozzle flows. USP2012058166768.
  18. Alkislar, Mehmet B.; Butler, George W.; Reed, David H.. Systems and methods for reducing noise from jet engine exhaust. USP2011067966826.
  19. Beutin,Bruno; Dos Santos,Nelson; Fert,Jeremy; Lacorre,Fabienne; Picard,Jean Louis. Turbojet having a large bypass ratio. USP2008107430852.
  20. Thomas, Russell H.; Kinzie, Kevin W.. Wet active chevron nozzle for controllable jet noise reduction. USP2011098015819.