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특허 상세정보

Acoustic resonator with impingement cooling tubes

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G10K-011/02    G10K-011/00   
미국특허분류(USC) 181/293; 181/210; 181/211; 181/213; 181/292
출원번호 US-0339721 (2006-01-25)
등록번호 US-7413053 (2008-08-19)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 30  인용 특허 : 20
초록

Aspects of the invention are directed to an acoustic resonator with improved impingement cooling effectiveness. The resonator includes a plate with an inside face and an outside face. A plurality of passages extend through the plate. The resonator includes a side wall that extends from and about the plate. A plurality of cooling tubes are attached to the resonator plate such that an inner passage of each cooling tube is in fluid communication with a respective passage in the resonator plate. The resonator can be secured to a surface of a turbine engine c...

대표
청구항

What is claimed is: 1. An acoustic resonator comprising: a resonator plate having an outside face, an inside face, and a plurality of passages extending through the resonator plate from the inside face to the outside face; at least one side wall extending from and about the resonator plate; and a plurality of cooling tubes extending front the inside face of the resonator plate, the cooling tubes having a first end, a second end and an inner passage, wherein the first end of each cooling tube is operatively connected to the resonator plate such that the ...

이 특허에 인용된 특허 (20)

  1. Pandalai Raghavan P. (Cincinnati OH) Carter Bruce A. (West Chester OH) Hehmann Horst W. W. (Cincinnati OH). Acoustic damper for a gas turbine engine combustor. USP1997115685157.
  2. Proscia,William; Jones,Christopher D.. Acoustic liner with bypass cooling. USP2007127311175.
  3. Jakob Keller CH; Georg Keller CH; Vera Keller CH. Combustion chamber for a gas turbine. USP2002036351947.
  4. Lewis George D. (North Palm Beach FL) Garrison Gary D. (Jupiter FL). Combustion instability reduction device having swirling flow. USP1976083974647.
  5. Hellat, Jaan; Tschirren, Stefan; Stuber, Peter; Paschereit, Christian Oliver. Damper arrangement for reducing combustion-chamber pulsations. USP2003046546729.
  6. Huck Andr (Saint Just FRX) Kernilis Alain (Paris FRX) Druart Jean-Paul (Notre Dame de L\Isle FRX) Dorville Georges (Rouen FRX). Damping system for high frequency combustion instabilities in a combustion chamber. USP1994105353598.
  7. Szecsi Laszlo (Karlsruhe DEX). Device for cooling a superconductive resonator and method of making the device. USP1981074277765.
  8. Gulati Anil (Cincinnati OH) Dean Anthony John (Scotia NY) Holmes David Graham (Schenectady NY) Voorhees Eayre Bruce (Sloansville NY). Dynamics free low emissions gas turbine combustor. USP1997075644918.
  9. Kudernatsch, Gunter. Exhaust gas system with helmholtz resonator. USP2004036705428.
  10. Aigner Manfred (Wettingen CHX) Urech Raphael (Hallwil CHX) Wetter Hugo (Buchs CHX). Gas turbine combustion chamber with scavenged Helmholtz resonators. USP1994125373695.
  11. Mandai, Shigemi; Suenaga, Kiyoshi; Aoyama, Kuniaki; Ikeda, Kazufumi; Tanaka, Katsunori. Gas turbine combustor. USP2005016837051.
  12. Suenaga, Kiyoshi; Mandai, Shigemi; Ono, Masaki; Tanaka, Katsunori. Gas turbine combustor, gas turbine, and jet engine. USP2005126973790.
  13. Hofler Thomas J.. Heat driven acoustic power source coupled to an electric generator. USP1999125996345.
  14. Newton Jefferson F. (Seattle WA) Martin Thomas D. (Bellevue WA) Westre Willard N. (Bellevue WA) Carbery David J. (Vashon Island WA) Ikegami Roy (Seattle WA). Lightweight honeycomb panel structure. USP1995085445861.
  15. Early Brian J. (Trumbull CT) Reens Daniel J. (Ridgefield CT) Karnoff Robert S. (Monroe CT). Method and apparatus for evaporative cooling of air leading to a gas turbine engine. USP1995115463873.
  16. Sattinger, Stanley S.; Darling, Douglas Dean; Holbert, Roy Kyle; Kepes, William E.. Modular resonators for suppressing combustion instabilities in gas turbine power plants. USP2003036530221.
  17. Kraft Robert E. ; Syed Asif A.. Rigid sandwich panel acoustic treatment. USP2001026182787.
  18. Takewa Hiroyuki (Kaizuka JPX) Torii Yutaka (Kadoma JPX). Sound absorber. USP1996045512715.
  19. Nash ; Dudley O. ; Holowach ; Joseph. Sound-suppressing structure with thermal relief. USP1978084106587.
  20. Eisinger Frantisek L. (Demarest NJ). Vibration of systems comprised of hot and cold components. USP1996025489202.

이 특허를 인용한 특허 피인용횟수: 30

  1. Alexander, Jonathan H.; Slama, David F.. Acoustic composite. USP2013028381872.
  2. Matsuyama, Keisuke; Nakamura, Sosuke. Acoustic damper, combustor and gas turbine. USP2016049316156.
  3. Portillo Bilbao, Juan Enrique; Rajaram, Rajesh; You, Danning; Spence, Kevin M.. Acoustic damping system for a combustor of a gas turbine engine. USP2016079400108.
  4. Kim, Kwanwoo; Han, Fei; Jain, Praveen; Narra, Venkat; Bethke, Sven Georg. Acoustic resonator located at flow sleeve of gas turbine combustor. USP2016099447971.
  5. Vincent, Thomas Alain Christian. Central body for a turbojet exhaust channel, turbojet. USP2011027886543.
  6. Bouty, Eric Jean-Louis; Dravet, Alain; Le Docte, Thierry Jacques Albert; Riou, Georges Jean Xavier; Vincent, Thomas Alain Christian. Central body of a turbojet nozzle. USP2011027891195.
  7. Huber, Andreas; Noiray, Nicolas; Schuermans, Bruno; Benz, Urs. Combustion device for a gas turbine. USP2018019857079.
  8. Huber, Andreas; Noiray, Nicolas; Schuermans, Bruno; Benz, Urs. Combustion device for a gas turbine configured to suppress thermo-acoustical pulsations. USP2015038991185.
  9. Huber, Andreas; Noiray, Nicolas; Benz, Urs; Reinert, Felix; Lauffer, Diane. Combustion device with a layered wall structure for a gas turbine. USP2015038978382.
  10. Tiwary, Abhijeet; Ramier, Stephen A.; Fox, Timothy A.; Bertoncello, James; Williams, Steven. Combustor resonator section with an internal thermal barrier coating and method of fabricating the same. USP2016079395082.
  11. Schilp, Reinhard. Cooling chamber for upstream weld of damping resonator on turbine component. USP2016089410484.
  12. Bothien, Mirko Ruben; Noiray, Nicolas; Schuermans, Bruno. Damper for gas turbine. USP20190410260745.
  13. Tonon, Devis; Bothien, Mirko Ruben; Genin, Franklin Marie; Pennell, Douglas Anthony. Damper with bent neck for gas turbine. USP20180710036327.
  14. Lee, Ching-Pang; You, Danning; Schilp, Reinhard; Prakash, Chander. Damping resonator with impingement cooling. USP2017019546558.
  15. Farstad, Jerry E.. Engine assembly, acoustical liner and associated method of fabrication. USP2011017870929.
  16. Johnson, Clifford E.. Flow control through a resonator system of gas turbine combustor. USP2013048413443.
  17. Stoia, Lucas John; Bailey, Donald Mark; Bethke, Sven Georg; Bobba, Mohan Krishna. Fuel nozzle assembly with resonator. USP20181210145561.
  18. Ikeda, Kazufumi; Mandai, Shigemi; Kawata, Yutaka; Aoyama, Kuniaki; Ono, Masaki; Tanaka, Katsunori. Gas turbine combustor and a gas turbine equipped therewith. USP2010117832211.
  19. Eroglu, Adnan; Freitag, Ewald; Rüdel, Uwe; Benz, Urs; Huber, Andreas. Gas turbine combustor including an acoustic damper device. USP2014018635874.
  20. Bothien, Mirko Ruben; Noiray, Nicolas; Schuermans, Bruno. Gas turbine damper with inner neck extending into separate cavities. USP2018029897314.
  21. Magni, Fulvio; Von Planta, Martin Andrea; Grimm, Frank; Nowak, Dariusz; Schaerer, Mischa. Helmholtz damper for a combustor of a gas turbine and a method for installing the helmholtz damper. USP2015028943825.
  22. Kim, Kwanwoo; Yoon, Changjin; Herbon, John Thomas. High frequency acoustic damper for combustor liners. USP20190210197275.
  23. Theuer, Andre; Palys, Dariusz Oliwiusz; Imfeld, Jost. Method and apparatus for gas turbine combustor inner cap and high frequency acoustic dampers. USP20190310220474.
  24. Kirby, Stuart J.. Noise reduction device. USP2012128336316.
  25. Johnson, Clifford E.; Bland, Robert J.; Gambacorta, Domenico; Wasif, Samer P.. Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber. USP2012048146364.
  26. Schilp, Reinhard; Sutcu, Muzaffer. Resonator system with enhanced combustor liner cooling. USP2014058720204.
  27. You, Danning; Schiavo, Anthony L.; Crane, John M.; Prade, Bernd; Krebs, Werner. Resonators with interchangeable metering tubes for gas turbine engines. USP2018069988958.
  28. Kitamura, Yoshiharu. Soundproofing plate and soundproofing device permitting air flow. USP2014058714304.
  29. Kitamura, Yoshiharu. Soundproofing plate which does not obstruct airflow. USP2014118893851.
  30. Melton, Patrick Benedict; Westmoreland, James Harold. Systems and methods for dampening combustor dynamics in a micromixer. USP2015119188342.