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Method and device for reducing the noise of turbo-machines 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F04D-029/66
출원번호 US-0849407 (1977-11-07)
우선권정보 FR-0034066 (1976-11-05)
발명자 / 주소
  • Raffy Pierre M. (Saint-Germain Laxis FRX) Andre Pierre A. (Paris FRX) Girault Jean-Pierre Y. B. (Dammarie les Lys FRX) Richter Gerhard (Boissise le Roi FRX) Thevenin Jean-Claude P. H. P. (Saint-Maur-
출원인 / 주소
  • Societe Nationale d\Etude et de Construction de Moteurs d\Aviation (Paris FRX 03)
인용정보 피인용 횟수 : 43  인용 특허 : 3

초록

A device for reducing the noise generated by the blades of at least one ring of rotor blades in a turbo-machine by the production of a counter-noise of opposed phase. This is achieved by injection of jets of fluid under pressure through orifices borne by the rotor located near to the periphery of th

대표청구항

A turbo-machine which comprises: at least one ring of circumferentially spaced, radially oriented rotor blades, the inner edges of which are attached to a rotor shaft; a rotatable cylindrical screen positioned around said rotor blades and integrally connected to their outer edges; and means for redu

이 특허에 인용된 특허 (3)

  1. Swinbanks Malcolm Alexander (Glasgow SC), Active control of sound waves.
  2. Mattei Jean (Saint-Mande FR) Simon Bernard (Clamart FR) Vuong nee Adlerberg Ingrid (Bures-sur-Yvette FR), Axial-flow fan with by-pass pipe or pipes.
  3. Hoff Richard W. (Newington CT), Turbine vane cooling.

이 특허를 인용한 특허 (43)

  1. Andersson Anders O. (Seattle WA), Active control of tone noise in engine ducts.
  2. Gordon Bruce J. (Cincinnati OH), Aircraft pylon.
  3. Gysling Daniel L. ; Feulner Matthew R. ; Eveker Kevin M., Apparatus and method of active flutter control.
  4. Ryan, William Richard; Berksoy, Sanem, Automatic combustion control for a gas turbine.
  5. Ryan, William Richard; Berksoy, Sanem, Automatic combustion control for a gas turbine.
  6. Warzyszynski, Mariusz; Webster, Jonathan, Conditioning method of gas turbine engine components for aerodynamic noise reduction.
  7. Farstad, Jerry E., Engine assembly, acoustical liner and associated method of fabrication.
  8. Tse, Man-Chun; LeBlanc, Andr?, Fan and compressor noise attenuation.
  9. Burdisso Ricardo A. ; Smith Jerome P., Fan noise reduction from turbofan engines using adaptive Herschel-Quincke tubes.
  10. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
  11. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
  12. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
  13. Winter, Michael; Jain, Ashok K., Gas turbine engine system providing simulated boundary layer thickness increase.
  14. Parker, David; Ryan, William Richard, Gas turbine with flexible combustion sensor connection.
  15. Caeti, Ryan B.; Kalkhoran, Iraj M., High-speed jet noise reduction via fluidic injection.
  16. Bowers,John L.; Hariram,Sham S.; Patel,Jayant D.; Sikand,Sharanpal S., Hingeless flapper valve for flow control.
  17. Rice Edward J. ; Walker Bruce E. ; Hersh Alan S., Hybrid mode-scattering/sound-absorbing segmented liner system and method.
  18. Richardson, Giles Anthony; MacManus, David; Sheaf, Christopher Thomas John, Intake liner for a gas turbine engine.
  19. Bolis,Giacomo; Hagstr��m,Gustav; Hoffmann,J��rgen; Wasmuth,Thorsten, Method and apparatus for achieving power augmentation in gas turbine using wet compression.
  20. Bolis, Giacomo; Hagström, Gustav; Hoffman, Jürgen; Wasmuth, Thorsten, Method and apparatus for achieving power augmentation in gas turbines using wet compression.
  21. Bolis,Giacomo; Hagstr��m,Gustav; Hoffmann,J��rgen; Wasmuth,Thorsten, Method and apparatus for achieving power augmentation in gas turbines using wet compression.
  22. Bolis,Giacomo; Hagstr��m,Gustav; Hoffmann,J��rgen; Wasmuth,Thorsten, Method and apparatus for achieving power augmentation in gas turbines using wet compression.
  23. Polifke Wolfgang,CHX ; Paschereit Christian Oliver,CHX ; Dobbeling Klaus,CHX, Method and device for minimizing thermoacoustic vibrations in gas-turbine combustion chambers.
  24. Andre Pierre A. (Paris FRX) Thevenin Jean-Claude P. H. P. (Saint.-Maur-des-Fosses FRX) Girault Jean-Pierre Y. B. (Dammarie les Lys FRX) Richter Gerhard (Boissise le Roi FRX), Method and device for reducing the noise of turbo-machines.
  25. Mani, Ramani; Graziosi, Paolo, Method and system for reduction of jet engine noise.
  26. Weiner Harvey I. ; Demers Christopher G., Method of assembling a rotary machine.
  27. Hoffmann, Juergen; Matz, Charles Raymond, Method of controlling the injection of liquid into an inflow duct of a prime mover or driven machine.
  28. Jacobs Loyd D. (Bellevue WA) Shivashankara Belur N. (Bellevue WA), Mounting assembly for unducted prop engine and method.
  29. Haas, Martin, Nacelle assembly having inlet bleed.
  30. Haas, Martin, Nacelle assembly with turbulators.
  31. Jain, Ashok K., Nacelle flow assembly.
  32. Jain, Ashok K., Nacelle flow assembly.
  33. Jain, Ashok K., Nacelle flow assembly.
  34. Ivers, Douglas E., Noise controlled turbine engine with aircraft engine adaptive noise control tubes.
  35. D'Angelo, John P., Noise reduction tubes.
  36. Antoine, Angelique Helene; Bouty, Eric Jean-Louis; Thomas, Alain Alphonse Leopold, Process and device for attenuating the noise made in a turbomachine by rotor/stator interaction.
  37. Weiner Harvey I. ; Demers Christopher G., Rotary machine.
  38. May Daryl N. ; Chapkis Robert L., Rotating machinery noise control device.
  39. Karam, Michael Abraham, Rotor noise suppression.
  40. Brough Anthony D. (Hamilton OH), System and method for actively controlling pressure pulses in a gas turbine engine combustor.
  41. Jain, Ashok K.; Winter, Michael, Variable contour nacelle assembly for a gas turbine engine.
  42. Jain, Ashok K.; Winter, Michael, Variable contraction ratio nacelle assembly for a gas turbine engine.
  43. Jain, Ashok K.; Chaudhry, Zaffir A., Variable shape inlet section for a nacelle assembly of a gas turbine engine.
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