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Contoured thrust reverser and lobed nozzle noise suppressor for gas turbine engines 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-001/00
출원번호 US-0491683 (2000-01-26)
발명자 / 주소
  • Presz
  • Jr. Walter M.
  • Reynolds Gary
출원인 / 주소
  • Stage III Technologies, L.C.
대리인 / 주소
    Holland, Esq.
인용정보 피인용 횟수 : 26  인용 특허 : 16

초록

A contoured thrust reverser and lobed nozzle noise suppressor is meant for use with gas turbine engines that have conventional post-exit thrust reversers and that require only moderate levels of noise suppression. The contoured thrust reverser and lobed nozzle noise suppressor comprises a convention

대표청구항

[ Having thus described the invention, what is claimed is:] [1.]1. A gas turbine engine having an attached thrust reverser and noise suppressor comprising:a. a lobed nozzle attached to an aft end of an engine tailpipe frame, wherein the lobed nozzle is shaped to mix ambient air external to the frame

이 특허에 인용된 특허 (16)

  1. Timms Richard H. (San Diego County CA), Aircraft thrust reverser mechanism.
  2. Presz ; Jr. Walter M. ; Reynolds Gary, Alternating lobed mixer/ejector concept suppressor.
  3. Fage Etienne,FRX, Bypass jet engine with confluent nozzle, rotating members which control the bypass air flow and a thrust reverser which.
  4. Giraud Pierre (45 ; rue de Lisbonne 75008 Paris FRX), Double flow turbine engine equipped with a central mixing nozzle and a thrust reverse.
  5. Fournier Alain M.,FRX, Electro/hydraulic system for a 2 door thrust reverser.
  6. Standish Robert R. (Gazeran FRX), Forward mounted pivoting door reverser with efflux control device.
  7. Moe Jeffrey W. ; Cariola Roy E. ; Lymons Dennis E., Pivoting door type thrust reverser with deployable members for efflux control and flow separation.
  8. Fage ; Etienne, Single-skin thrust reverser for aircraft jet engines.
  9. Meyer Pascal J.,FRX, Specially configured deflection edge thrust reverser for jet engine.
  10. Clarke James A. (E. Northport NY), Syntactic film for thrust reverser blocker doors.
  11. Mutch Henry (Chula Vista CA), Target thrust reverser.
  12. Peters Fred H. ; Jannetta Thomas J., Thrust reverser door side fillers.
  13. Lebrun Bertrand (Vincennes FRX) Lecossais Eric (Virville FRX) Lemay Henriette S. (Le Havre FRX) Metezeau Fabrice (Le Havre FRX) Valleroy Laurent G. (Le Havre FRX), Thrust reverser with aerodynamically cooled baffle.
  14. Metezeau Emile Fabrice Henri,FRX ; Portal Marcel Jean-Fabrice,FRX, Thrust reverser with improved forward thrust efficiency.
  15. Porte Alain,FRX, Turbofan with thrust reversal doors not submitted to bypass air in their inactive position.
  16. Presz ; Jr. Walter M., Two-stage mixer ejector suppressor.

이 특허를 인용한 특허 (26)

  1. Kernemp, Irwin; Langridge, Jonathan; Pascal, Sébastien; Guillois, Denis; Clere, Gérard; Chapelain, Loïc, Afterbody for a turbojet engine comprising a nozzle provided with a thrust reverser system that incorporates a crown of noise-reducing chevrons.
  2. Andre,Joan; Andrieu,Laurent, Aircraft provided with thrust reversers.
  3. Ryan, Michael E.; Dixon, J. David; Klein, Patrick M., Enclosed volume exhaust diffuser apparatus, system, and method.
  4. Malandra, Anthony J.; Orosa, John A., Exhaust diffuser including flow mixing ramp for a gas turbine engine.
  5. Janakiraman, Arun; Feng, Shiming, Exhaust gas aspirator.
  6. Suciu, Gabriel L.; Merry, Brian D.; Penda, Allan R.; Dye, Christopher M.; Bhatt, Jay, Fan case thrust reverser.
  7. Presz, Jr., Walter M.; Werle, Michael J.; Kennedy, III, Thomas J.; Keeley, William Scott; Dold, Robert H., Fluid turbine.
  8. Yan, Guorong; Cunningham, Mark; Di Paola, Franco, Gas turbine engine ejector.
  9. Lane,Michael T, Hot-fillable blow molded container with pinch-grip vacuum panels.
  10. Anderson, Morris G.; Jan, David K.; Zurmehly, George E.; Halfmann, Steve H.; Zollars, Christopher E., Integrated support and mixer for turbo machinery.
  11. Anderson, Jack H., Jet nozzle mixer.
  12. Anderson,Jack H., Jet nozzle mixer.
  13. Clerc,James C.; Cramer,James A.; Dixon,J. David; Ntone,Francois; Klein,Patrick M., Lobed exhaust diffuser apparatus, system, and method.
  14. Presz, Jr., Walter M.; Werle, Michael J.; Kennedy, III, Thomas J.; Keeley, William Scott, Nacelle configurations for a shrouded wind turbine.
  15. Davidson, Debbie; Engeham, Duncan; Uban, Piotr; Elsey, David; Liu, Z. Gerald; Pawson, Kenneth; Smith, Paul; Capel, Ken; Critchley, Andrew; Sarcona, David; Goss, James, Reductant decomposition system.
  16. Davidson, Debbie; Engeham, Duncan; Urban, Piotr; Elsey, David; Liu, Z. Gerald; Pawson, Ken; Smith, Paul; Capel, Ken; Critchley, Andrew; Sarcona, David; Goss, James R, Reductant decomposition system.
  17. Presz, Jr., Walter M.; Werle, Michael J.; Kennedy, III, Thomas J.; Keeley, William Scott, Segmented wind turbine.
  18. Caruel, Pierre; Vauchel, Guy Bernard, Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut.
  19. Durocher, Eric; Lefebvre, Guy, Turbine exhaust case mixer of gas turbine with variable thickness.
  20. Presz, Jr., Walter M.; Werle, Michael J., Turbine with mixers and ejectors.
  21. Presz, Jr., Walter M.; Werle, Michael J., Turbine with mixers and ejectors.
  22. Bardagi, Thierry; Dravet, Alain; Doussinault, Marc, Turbomachine nozzle with noise reduction.
  23. Presz, Jr., Walter M.; Werle, Michael J., Water turbines with mixers and ejectors.
  24. Presz, Jr., Walter M.; Werle, Michael J., Wind turbine with mixers and ejectors.
  25. Presz, Jr., Walter M.; Werle, Michael J., Wind turbine with mixers and ejectors.
  26. Presz, Jr., Walter M.; Werle, Michael J., Wind turbine with mixers and ejectors.
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