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High admittance acoustic liner 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-033/02
  • B64D-033/00
출원번호 US-0878806 (2004-06-28)
등록번호 US-7337875 (2008-03-04)
발명자 / 주소
  • Proscia,William
  • Jones,Christopher D.
  • Patrick,William P.
출원인 / 주소
  • United Technologies Corporation
인용정보 피인용 횟수 : 22  인용 특허 : 20

초록

A cooled acoustic liner useful in a fluid handling duct includes a resonator chamber 52 with a neck 56, a face sheet 86, and a coolant plenum 80 residing between the face sheet and the chamber. Coolant bypasses the resonator chamber, rather than flowing through it, resulting in better acoustic admit

대표청구항

We claim: 1. A gas turbine engine acoustic liner for attenuating noise generated by working fluid flowing through said gas turbine engine at a noise source, comprising: a resonator including a chamber having an opening; a face sheet between the chamber and the working fluid, said chamber opening re

이 특허에 인용된 특허 (20)

  1. Autie Pascal J. M. (Paris FRX) Avignon Philippe P. (Combs-la-Ville FRX) Camusso Dominique P. (Evry FRX) Forestier Alexandre (Melun FRX) Ulryck Gilles (Ballancourt FRX), Acoustic panel for sound insulating linings of gas ducts.
  2. Rolston Stephen C.,GBX ; Ashford Edward M.,GB5, Aerodynamic low drag structure.
  3. Porte, Alain; Batard, Herv?, Aircraft engine pod with acoustic attenuation.
  4. Parente Charles A., Combined acoustic and anti-ice engine inlet liner.
  5. Wiseman Albert D. (Wilmington OH), Engine noise suppression kit for the nacelles of a jet aircraft.
  6. Arcas Noe ; Hutto Frederick M. ; Parente Charles A., Extended reaction acoustic liner for jet engines and the like.
  7. Dear Terrence A. (Elkton MD) Ingard Karl U. (Kittery Point ME), Fluid distribution system having noise reduction mechanism.
  8. Tindell Runyon H. ; Parente Charles A., Low drag inlet design using injected duct flow.
  9. Breer, Marlin D.; Olsen, Ronald F.; Kunze, Jr., Robert K.; Riedel, Brian L., Method and apparatus for aircraft inlet ice protection.
  10. Clarke James A. ; Kunze ; Jr. Robert K., Method of forming acoustic attenuation chambers using laser processing of multi-layered polymer films.
  11. Chapman John F. (Solihull GB2), Multi-layer acoustic linings.
  12. Batey John G. (Cordova TN) Burrets Park W. (Memphis TN) Grewe William F. (Memphis TN) Whitestone Bruce G. (Germantown TN) Yerger Mark D. (Collierville TN), Noise reduction kit for jet turbine engines.
  13. Anderson Robert E. (Huntington Station NY) Parente Charles A. (Oyster Bay NY), One-piece engine inlet acoustic barrel.
  14. Bar Alfredo (Pavia ITX), Reciprocating hermetic motor compressor with a thermetically insulatable non-rotatable muffler.
  15. Bellucci,Valter; Flohr,Peter; Paschereit,Christian Oliver; Schuermans,Bruno; Tabacco,Daniele, Reheat combustion system for a gas turbine.
  16. Andrews John S. (Barry EN), Silencer for ventilation ducts.
  17. Snyder Stephen (West Hills CA), Sound attenuation system for jet aircraft engines.
  18. Dean ; III Lee W. (South Glastonbury CT) Peracchio Aldo A. (South Windsor CT), Sound suppressor liners.
  19. Nash ; Dudley O. ; Holowach ; Joseph, Sound-suppressing structure with thermal relief.
  20. Harper Harold M. (Brooklyn MI) Schmitz ; III Raymond J. (Tecumseh MI) Kandpal Tara C. (Tecumseh MI), Suction muffler.

이 특허를 인용한 특허 (22)

  1. Wang, Shanwu; Han, Fei; Mueller, Mark Anthony, Acoustic damping device for use in gas turbine engine.
  2. Alonso-Miralles, Jose S., Acoustic panel assembly with a folding chamber.
  3. Ali, Amr, Acoustic treatment in an unducted area of a geared turbomachine.
  4. Ali, Amr, Acoustic treatment in geared turbomachine.
  5. Huber, Andreas; Noiray, Nicolas; Schuermans, Bruno; Benz, Urs, Combustion device for a gas turbine.
  6. Huber, Andreas; Noiray, Nicolas; Schuermans, Bruno; Benz, Urs, Combustion device for a gas turbine configured to suppress thermo-acoustical pulsations.
  7. Schnell, Alexander; Noiray, Nicolas; Reinert, Felix; Lauffer, Diane; Schuermans, Bruno, Combustion device of a gas turbine including a plurality of passages and chambers defining helmholtz resonators.
  8. Huber, Andreas; Noiray, Nicolas; Benz, Urs; Reinert, Felix; Lauffer, Diane, Combustion device with a layered wall structure for a gas turbine.
  9. Farstad, Jerry E., Engine assembly, acoustical liner and associated method of fabrication.
  10. Corr, Robert; Sykes, Peter; Struck, Bruno; Thomas, Kenneth G.; Braeutigam, Richard; Gauce, Danny; Krichever, Alexander; Phi, Vu; Caron, Timothy, Gas turbine combustor with mounting for Helmholtz resonators.
  11. Moon, Francis R.; Kupratis, Daniel Bernard, Gas turbine engine with reverse-flow core having a bypass flow splitter.
  12. Bouchard, Richard; Pietrobon, John; Durocher, Eric, Gas turbine exhaust case.
  13. Bouchard, Richard; Girard, Gaetan; Pronovost, Christian, Gas turbine exhaust case with acoustic panels.
  14. Cunha, Francisco J.; Snyder, Timothy S., Impingement cooling for turbofan exhaust assembly.
  15. Liu, Zheji, Multi-degree of freedom resonator array.
  16. Mattia, Stephen H., Noise attenuating acoustic panel.
  17. Cai, Xiaobing, Sound absorber.
  18. Todorovic, Predrag, Sound absorber for a gas turbine exhaust cone, and method for the production thereof.
  19. Ichihashi, Fumitaka, Stepped acoustic structures with multiple degrees of freedom.
  20. Bouchard, Richard; Trottier, Daniel; Girard, Gaetan, Strut mounting arrangement for gas turbine exhaust case.
  21. Baarck, Jenny N.; Krayenvenger, Daren; Proscia, William; Jones, Christopher D., Turbine engine tailcone resonator.
  22. Bouteiller, Xavier; Blin, Laurent Albert, Turbojet engine nacelle.
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