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특허 상세정보

Device for controlling propulsive jet mixing for aircraft jet engines

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/00   
미국특허분류(USC) 060/770; 239/265.19; 060/228
출원번호 US-0801265 (2004-03-16)
우선권정보 FR-01 12113(2001-09-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    DLA Piper US LLP
인용정보 피인용 횟수 : 6  인용 특허 : 28
초록이 없습니다.
대표청구항이 없습니다

이 특허에 인용된 특허 (28)

  1. Dorris ; III John ; Smith David Michael ; Parekh David Espineli ; Kibens Valdis. Apparatus and methods for active flow control of a nozzle exhaust plume. USP2001106308898.
  2. Speir Donald W. (Cincinnati OH) McHugh Donald P. (Cincinnati OH). Articulated plug nozzle. USP1977084043508.
  3. John F. Brausch ; Bangalore A. Janardan ; John W. Barter, IV ; Gregory E. Hoff. Chevron exhaust nozzle for a gas turbine engine. USP2002036360528.
  4. Hebert, Leonard J.. Convergent/divergent segmented exhaust nozzle. USP2003126658839.
  5. Nesbitt, Eric H.; Butler, George W.; Reed, David H.. Deployable segmented exhaust nozzle for a jet engine. USP2004046718752.
  6. Lair, Jean-Pierre. Duplex mixer exhaust nozzle. USP2004096786038.
  7. Giffin ; III Rollin G. (Cincinnati OH) Wolf Jeremiah P. (Cincinnati OH) Hilse Mark A. (Middletown OH). Exhaust assembly for a high speed civil transport aircraft engine. USP1992105154052.
  8. Birch, Nigel T; Webster, John R. Gas turbine engine exhaust nozzle having a noise attenuation device driven by shape memory material actuators. USP2004116813877.
  9. Steven H. Zysman ; Wesley K. Lord ; Gregory A. Kohlenberg. Gas turbine engine jet noise suppressor. USP2002126487848.
  10. Horgan John J. (Wethersfield CT). Gas turbine outlet arrangement. USP1987094696159.
  11. Luffy Ronald J. (Maineville OH) Taylor ; Jr. John B. (Cincinnati OH) Sutherland William V. (Milford OH) Stine Frederick J. (Mainville OH) Crowley James A. (Midlothian VA) Mann David E. (West Chester . Method and apparatus for boosting ram airflow to an ejection nozzle. USP1995075435127.
  12. Speller Kevin E.. Method and apparatus for vectoring thrust employing electrodes generating voltages greater than the dielectric breakdow. USP1998055752381.
  13. Catt Jeffrey Alan ; Miller Daniel Nicholas. Method and apparatus of asymmetric injection at the subsonic portion of a nozzle flow. USP2000096112513.
  14. Glezer Ari ; Smith Barton L. ; Trautman Mark A.. Modifications of fluid flow about bodies and surfaces with synthetic jet actuators. USP1999095957413.
  15. Koff ; Bernard L. ; Budinger ; Raymond E. ; Johnson ; James E.. Modulating bypass variable cycle turbofan engine. USP1978034080785.
  16. Dusa Donald J. (Cincinnati OH). Multiple bypass-duct turbofan with annular flow plug nozzle and method of operating same. USP1977094050242.
  17. Klees Garry W. (Mercer Island WA) Lidstone Gary L. (Federal Way WA) Sloan Mark L. (Renton WA). Nozzle system and method for supersonic jet engine. USP1993065222359.
  18. Martens, Steven. Shelf truncated chevron exhaust nozzle for reduction of exhaust noise and infrared (IR) signature. USP2003036532729.
  19. Ellis Stanley H. (Palm Beach Gardens FL). Small gas turbofan engine with regenerating diffuser. USP1982114357796.
  20. Janardan, Bangalore Ananthamurthy; Brausch, John Francis. Stub airfoil exhaust nozzle. USP2003016502383.
  21. Klees Garry W. (Mercer Island WA). Supersonic jet engine and method of operating the same. USP1981104294068.
  22. Glezer Ari ; Allen Mark G. ; Coe David J. ; Smith Barton L. ; Trautman Mark A. ; Wiltse John W.. Synthetic jet actuator and applications thereof. USP1998065758823.
  23. Mathews Douglas C. ; Low John K. C.. Tabbed nozzle for jet noise suppression. USP2001116314721.
  24. Dusa Donald J. (Cincinnati OH) Kuchar Andrew P. (West Chester OH) Faust Guy K. (West Chester OH). Turbofan mixed flow exhaust system. USP1986064592201.
  25. Thomas William W. (Cincinnati OH) Sprunger Elmore V. (Cincinnati OH). Two-spool variable cycle engine. USP1977084043121.
  26. Rey, Nancy M.; Miller, Robin Mihekun; Tillman, Thomas G.; Rukus, Robert M.; Kettle, John L.. Variable area nozzle for gas turbine engines driven by shape memory alloy actuators. USP2004056735936.
  27. Giffin ; III Rollin G. (Cincinnati OH). Variable specific thrust turbofan engine. USP1993115261227.
  28. McAndrews Glenn (Lebanon OH). Variable vane valve in a gas turbine. USP1993025184459.