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Shelf truncated chevron exhaust nozzle for reduction of exhaust noise and infrared (IR) signature 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B63H-011/00
출원번호 US-0871263 (2001-05-31)
발명자 / 주소
  • Martens, Steven
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Herkamp, Nathan D.Conte, Francis L.
인용정보 피인용 횟수 : 46  인용 특허 : 4

초록

An exhaust nozzle includes an annular exhaust duct for discharging exhaust from an aft end thereof. Circumferentially adjoining chevrons extend from the duct aft end around only an arcuate portion thereof leaving a plain arcuate shelf between terminal ones of the chevrons. Each of the chevrons has a

대표청구항

An exhaust nozzle includes an annular exhaust duct for discharging exhaust from an aft end thereof. Circumferentially adjoining chevrons extend from the duct aft end around only an arcuate portion thereof leaving a plain arcuate shelf between terminal ones of the chevrons. Each of the chevrons has a

이 특허에 인용된 특허 (4)

  1. John F. Brausch ; Bangalore A. Janardan ; John W. Barter, IV ; Gregory E. Hoff, Chevron exhaust nozzle for a gas turbine engine.
  2. Larson Richard S. (Rocky Hill CT) Packman Allan B. (West Hartford CT), Gas turbine noise suppressor.
  3. Gilbertson Frederick L. (Toronto CAX) Garland Douglas B. (Toronto CAX) Whittley Donald C. (Toronto CAX), Nozzle structure with notches.
  4. Mathews Douglas C. ; Low John K. C., Tabbed nozzle for jet noise suppression.

이 특허를 인용한 특허 (46)

  1. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C., Aircraft configuration.
  2. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.; Lan, Justin, Aircraft configuration.
  3. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C., Airplane configuration.
  4. Viswanathan,Krishnamurthy, Apparatus and method for reduction jet noise from single jets.
  5. Viswanathan, Krishnamurthy, Apparatus and method for reduction of jet noise from single jets.
  6. Viswanathan, Krishnamurthy, Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flaws.
  7. Viswanathan,Krishnamurthy, Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flows.
  8. Narayanan, Satish; Simonich, John; Schlinker, Robert Hans, Asymmetric serrated nozzle for exhaust noise reduction.
  9. Anderson,Morris G.; Gerrard,John C.; Ruiz,Ron G.; Mitchell,Robert D., Compact mixer with trimmable open centerbody.
  10. Hebert, Leonard J., Convergent/divergent segmented exhaust nozzle.
  11. Nesbitt, Eric H.; Butler, George W.; Reed, David H., Deployable segmented exhaust nozzle for a jet engine.
  12. Bonnet,Jean Paul; Delville,Joel; Collin,Erwan; Tensi,Jean; Moreau,Eric; Touchard,Gerard, Device for controlling propulsive jet mixing for aircraft jet engines.
  13. Gupta,Anurag, Device for reducing jet engine exhaust noise using oscillating jets.
  14. Core, Robert A., Dilating fan duct nozzle.
  15. Gutmark, Ephraim Jeff; Martens, Steven (nmn), Duplex tab exhaust nozzle.
  16. Uhm, Jong Ho; Johnson, Thomas Edward, Fuel nozzle assembly for use in turbine engines and methods of assembling same.
  17. Huzzard Cunningham, Mark, Gas turbine engine exhaust mixer including circumferentially spaced-apart radial rows of tabs extending downstream on the radial walls, crests and troughs.
  18. Webster, John R, Gas turbine engine exhaust nozzle.
  19. Birch,Nigel T; Webster,John R, Gas turbine engine exhaust nozzle having a noise attenuation device driven by shape memory material actuators.
  20. Shmilovich, Arvin; Yadlin, Yoram; Smith, David M.; Clark, Roger W., Integrated engine exhaust systems and methods for drag and thermal stress reduction.
  21. Shmilovich, Arvin; Yadlin, Yoram; Smith, David M.; Clark, Roger W., Integrated engine exhaust systems and methods for drag and thermal stress reduction.
  22. Anderson, Morris G.; Jan, David K.; Zurmehly, George E.; Halfmann, Steve H.; Zollars, Christopher E., Integrated support and mixer for turbo machinery.
  23. Suchezky, Mark E.; Simpkins, Lisa M., Jet engine exhaust nozzle and associated system and method of use.
  24. Mengle, Vinod G., Jet engine nozzle exit configurations and associated systems and methods.
  25. Mengle, Vinod G., Jet engine nozzle exit configurations and associated systems and methods.
  26. Mengle, Vinod G.; Thomas, Russell H., Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods.
  27. Oba, Yoshinori; Oishi, Tsutomu, Jet flow discharge nozzle and jet engine.
  28. Nesbitt, Eric H.; Yee, Mark; Elkoby, Ronen; Hebert, Leonard J.; Alston, Thomas E., Jet nozzle having noise attenuating shield and method therefor.
  29. Gutmark,Ephraim Jeff; Callender,Bryan W.; Martens,Steven, Method and apparatus for operating gas turbine engines.
  30. Porte, Alain, Method for attenuating the noise of a turbofan.
  31. Gowda,Srinivasa Range; Early,Kevin Sean; Martens,Steven, Methods and apparatus for operating gas turbine engines.
  32. Gutmark,Ephraim Jeff; Martens,Steven, Methods and apparatus for operating gas turbine engines.
  33. Mengle, Vinod Govind, Noise-reducing engine nozzle system.
  34. Rose, Marco; Spieweg, Rene, Nozzle with guiding devices.
  35. Rose, Marco; Spieweg, Rene, Nozzle with guiding devices.
  36. Dun, Roy, Scarf nozzle for a jet engine and method of using the same.
  37. Reba, Ramons Andris; Wake, Brian Ernest; Narayanan, Satish; Maeder, Thierry, Serrated nozzle trailing edge for exhaust noise suppression.
  38. Blodgett,Keith Edward James; Early,Kevin Sean; Martens,Steven; Bailey,William Andrew; Price,Kenneth Daniel, Sinuous chevron exhaust nozzle.
  39. Renggli,Bernard James, Split shroud exhaust nozzle.
  40. 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.
  41. 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.
  42. Alkislar, Mehmet B.; Butler, George W.; Reed, David H., Systems and methods for reducing noise from jet engine exhaust.
  43. Au, Dax; Bigot, Pascal Moise Michel; Briend, Pierre; Loheac, Pierre Philippe Marie, Turbomachine nozzle cover provided with triangular patterns having a point of inflexion for reducing jet noise.
  44. Au, Dax; Bigot, Pascal Moise Michel; Briend, Pierre; Loheac, Pierre Philippe Marie, Turbomachine nozzle cover provided with triangular patterns having pairs of vertices for reducing jet noise.
  45. Quarin, Benedetta; Zeggai, Kamel, Turbomachine nozzle cowl having patterns with lateral fins for reducing jet noise.
  46. Arnold,Steven M.; Penney,Nicholas, Variable area nozzle including a plurality of convexly vanes with a crowned contour, in a vane to vane sealing arrangement and with nonuniform lengths.
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