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특허 상세정보

Outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/28   
미국특허분류(USC) 060/231; 060/770; 239/265.17
출원번호 US-0577506 (2005-11-01)
등록번호 US-8327617 (2012-12-11)
우선권정보 SE-0402715 (2004-11-05); SE-0402951 (2004-12-02)
국제출원번호 PCT/SE2005/001646 (2005-11-01)
§371/§102 date 20070419 (20070419)
국제공개번호 WO2006/049568 (2006-05-11)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    WRB-IP LLP
인용정보 피인용 횟수 : 0  인용 특허 : 14
초록

An outlet nozzle for a jet engine has a gas intake and a gas outlet, at least one opening being provided through the nozzle boundary wall for the injection of a fluid into the nozzle in a direction perpendicular to one plane, for the purpose of controlling the direction of a gas flow from the jet engine so that vectoring occurs substantially tangentially in this plane. A first opening configuration is provided through the nozzle boundary wall on a first side of the nozzle center line and a second opening configuration is provided through the nozzle bound...

대표
청구항

1. An outlet nozzle for a jet engine, comprising a gas intake and a gas outlet, at least one opening being provided through a nozzle boundary-wall for injection of a fluid into the nozzle in a direction perpendicular to one plane to control a direction of a gas flow from the jet engine so that vectoring occurs substantially tangentially in the plane, wherein a first opening configuration is provided through the nozzle boundary wall on a first side of a nozzle center line and a second opening configuration is provided through the nozzle boundary wall on a...

이 특허에 인용된 특허 (14)

  1. Lee, Douglas; Anderson, J. Thomas; Hershberger, Brian K.. Apparatus and method for controlling primary fluid flow using secondary fluid flow injection. USP2004016679048.
  2. Fitzgerald Robert E. (New Britain CT). Control vanes for thrust vector control nozzle. USP1988074754927.
  3. Jenkins Julian L. (Arlington TX) Wood Tommie L. (Arlington TX) Brand Albert G. (North Richland Hills TX). Engine exhaust gas deflection system. USP1995075435489.
  4. Avenell, Christopher Stuart. Fluid vectoring nozzle. USP2010027658337.
  5. John Michael Koshoffer. Fluidic nozzle control system. USP2002016336319.
  6. Mueller John H.. Fluidic throat exhaust nozzle. USP1999125996936.
  7. Vaughan ; III ; John C.. Jet engine tail pipe flow deflector. USP1978014069977.
  8. Kranz Walter (Taufkirchen DEX) Tillmann Heinz (Ottobrunn DEX). Jet engine with a thrust vector control. USP1982094351479.
  9. Catt Jeffrey Alan ; Miller Daniel Nicholas. Method and apparatus of asymmetric injection at the subsonic portion of a nozzle flow. USP2000096112513.
  10. Miller, Daniel N.; Yagle, Patrick J.; Ginn, Kerry B.; Hamstra, Jeffrey W.. Method and apparatus of asymmetric injection into subsonic flow of a high aspect ratio/complex geometry nozzle. USP2005116962044.
  11. Sondee Daniel C. ; Kelton Michael W.. Single variable flap exhaust nozzle. USP1998115833139.
  12. Johnson,James Edward. Thrust vectoring missile turbojet. USP2009037509797.
  13. Thayer Edward B.. Vectoring nozzle using injected high pressure air. USP1998015706650.
  14. Blozy,Jack T.; Willard,Charles M.; Messersmith,Nathan L.; Velazquez,Miquel A.. Yaw vectoring for exhaust nozzle. USP2009017481038.