$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Modular resonators for suppressing combustion instabilities in gas turbine power plants 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/24
출원번호 US-0667409 (2000-09-21)
발명자 / 주소
  • Sattinger, Stanley S.
  • Darling, Douglas Dean
  • Holbert, Roy Kyle
  • Kepes, William E.
출원인 / 주소
  • Siemens Westinghouse Power Corporation
인용정보 피인용 횟수 : 54  인용 특허 : 7

초록

A resonator module for a combustion turbine power plant, where the combustion turbine power plant defines a flow path. The resonator module includes a first member, an a second member. The first member has a size substantially smaller than the diameter of said flow path and a plurality of openings t

대표청구항

1. A resonator module in combination with a combustion turbine power plant, wherein said combustion turbine power plant has a compressor assembly, a combustor assembly, a turbine assembly, and a transition section between said combustor assembly and said turbine assembly which define a flow path, sa

이 특허에 인용된 특허 (7)

  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.
  2. Pla Frederic G. (Clifton Park NY), Active noise control using an array of plate radiators and acoustic resonators.
  3. Motsinger Russell E. (Cincinnati OH) Vdoviak John W. (Marblehead MA), Closed cavity noise suppressor.
  4. Aigner Manfred (Wettingen CHX) Urech Raphael (Hallwil CHX) Wetter Hugo (Buchs CHX), Gas turbine combustion chamber with scavenged Helmholtz resonators.
  5. Cowan Samuel J. (Seattle WA) Gerend Robert P. (Bellevue WA) Ramsay James W. (Bellevue WA) Shivashankara Belur N. (Renton WA), Gas turbine engine combustion noise suppressor.
  6. Fuchs Helmut,DEX ; Hunecke Joerg,DEX ; Zha Xueqin,DEX, Plate resonator.
  7. Forestier Alexandre (Vaux le Penil FRX) Pluquet Alain A. (Melun FRX) Rosa Roger A. (Morangis FRX) Tabet Mansour (Melun FRX) Teysseyre Pierre M. (Juvisy sur Orge FRX), Soundproofing for a gas pipe, in particular for the fan jet of a turbojet, and equipment for its fabrication.

이 특허를 인용한 특허 (54)

  1. Chiou, Song; Yu, Jia; Hubert, Claude; Layland, Michael, Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers.
  2. Portillo Bilbao, Juan Enrique; Rajaram, Rajesh; You, Danning; Spence, Kevin M., Acoustic damping system for a combustor of a gas turbine engine.
  3. Ishida, Masahiro; Matsuda, Naoki, Acoustic device and electronic device and image forming apparatus incorporating same.
  4. Wasif,Samer P.; Johnson,Clifford E., Acoustic resonator with impingement cooling tubes.
  5. Sattinger,Stanley S., Acoustically stiffened gas-turbine fuel nozzle.
  6. Gilcreest, Mark D.; Sleath, Trevor G.; Gelzer, Daniel F.; Windels, Merlin C., Acoustically treated exhaust centerbody for jet engines and associated methods.
  7. Rajaram, Rajesh; Ritland, David M., Attenuation of combustion dynamics using a Herschel-Quincke filter.
  8. Vincent, Thomas Alain Christian, Central body for a turbojet exhaust channel, turbojet.
  9. 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.
  10. Young,Kenneth James; Steinbach,Klaus Stefan; Herzog,Volker; Dupere,Iain David Jeffrey; Geary,Alan Philip; Gerendas,Miklos, Combustion chamber for gas turbine engine.
  11. Melton, Patrick Benedict; Belsom, Keith Cletus; Stoia, Lucas John, Combustor.
  12. Johnson, Clifford E.; Lepers, Joachim; Wasif, Samer P., Combustor assembly including one or more resonator assemblies and process for forming same.
  13. 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.
  14. Bobba, Mohan Krishna; Kim, Kwanwoo; Melton, Patrick Benedict; Antoniono, Carolyn Ashley, Combustor resonator with non-uniform resonator passages.
  15. Alkabie, Hisham; Morenko, Oleg; McCaldon, Kian, Combustor with improved swirl.
  16. Mandai, Shigemi; Kawata, Yutaka; Maekawa, Atsushi; Tanaka, Katsunori; Nishimura, Masaharu; Tomimoto, Soichiro, Combustor, a gas turbine, and a jet engine.
  17. Schilp, Reinhard, Cooling chamber for upstream weld of damping resonator on turbine component.
  18. Schuermans, Bruno; Bothien, Mirko Ruben, Damper for combustion oscillation damping in a gas turbine.
  19. Lee, Ching-Pang; You, Danning; Schilp, Reinhard; Prakash, Chander, Damping resonator with impingement cooling.
  20. Bothien, Mirko Ruben; Jorgensen, Stephen W.; Pennell, Douglas, Damping system for combustor.
  21. Farstad, Jerry E., Engine assembly, acoustical liner and associated method of fabrication.
  22. Johnson, Clifford E., Flow control through a resonator system of gas turbine combustor.
  23. Gambacorta, Domenico; Johnson, Clifford E., Forward-section resonator for high frequency dynamic damping.
  24. Stoia, Lucas John; Bailey, Donald Mark; Bethke, Sven Georg; Bobba, Mohan Krishna, Fuel nozzle assembly with resonator.
  25. Olsen, Andrew J.; Austrem, Ivar; Yildirim, M. Serkan; Liu, Zheji, Gas turbine combustion acoustic damping system.
  26. Akamatsu, Shinji; Kishida, Hiroaki; Sato, Kenji; Tokuyama, Kentaro; Matsuyama, Keisuke; Takashima, Takayoshi, Gas turbine combustor.
  27. Akamatsu, Shinji; Kishida, Hiroaki; Sato, Kenji; Tokuyama, Kentaro; Matsuyama, Keisuke; Takashima, Takayoshi, Gas turbine combustor.
  28. Akamatsu, Shinji; Kishida, Hiroaki; Sato, Kenji; Tokuyama, Kentaro; Matsuyama, Keisuke; Takashima, Takayoshi, Gas turbine combustor.
  29. Ikeda,Kazufumi; Ishiguro,Tatsuo; Tanaka,Katsunori; Tanimura,Satoshi, Gas turbine combustor.
  30. Mandai, Shigemi; Suenaga, Kiyoshi; Aoyama, Kuniaki; Ikeda, Kazufumi; Tanaka, Katsunori, Gas turbine combustor.
  31. Ikeda, Kazufumi; Mandai, Shigemi; Kawata, Yutaka; Aoyama, Kuniaki; Ono, Masaki; Tanaka, Katsunori, Gas turbine combustor and a gas turbine equipped therewith.
  32. Ohnishi, Keizo; Ikeda, Kazufumi; Ono, Masaki; Nishimura, Masaharu; Tanaka, Katsunori, Gas turbine combustor having an acoustic energy absorbing wall.
  33. Eroglu, Adnan; Freitag, Ewald; Rüdel, Uwe; Benz, Urs; Huber, Andreas, Gas turbine combustor including an acoustic damper device.
  34. 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.
  35. Suenaga, Kiyoshi; Mandai, Shigemi; Ono, Masaki; Tanaka, Katsunori, Gas turbine combustor, gas turbine, and jet engine.
  36. Suenaga, Kiyoshi; Mandai, Shigemi; Ono, Masaki; Tanaka, Katsunori, Gas turbine combustor, gas turbine, and jet engine.
  37. Matsuyama, Keisuke; Miyauchi, Kotaro, Gas turbine having a combustion oscillation suppressing device.
  38. Bland,Robert; Ryan,William, High frequency dynamics resonator assembly.
  39. Johnson, Thomas Edward; Ziminsky, Willy Steve; York, William David; Stevenson, Christian Xavier, Injector with integrated resonator.
  40. Nemet, Anton; Kokanovic, Stanka, Method for automatic closed-loop control of one or more combustion temperatures in a gas turbine installation and method for determination of the water content in the working fluid of a gas turbine installation.
  41. Alkabie, Hisham, Noise reducing combustor.
  42. Alkabie, Hisham, Noise reducing combustor.
  43. Johnson, Clifford E.; Bland, Robert J.; Gambacorta, Domenico; Wasif, Samer P., Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber.
  44. Nishimura,Masaharu; Ono,Masaki; Ohnishi,Keizo; Tanaka,Katsunori, Outer casing covering gas turbine combustor.
  45. Chiou, Song; Yu, Jia; Hubert, Claude; Layland, Michael, Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure.
  46. Davis, Jr., Lewis Berkley; Han, Fei; Srinivasan, Shiva; Singh, Kapil Kumar; Kim, Kwanwoo; Narra, Venkateswarlu, Resonator assembly for mitigating dynamics in gas turbines.
  47. Johnson, Clifford E.; Wasif, Samer P., Resonator device at junction of combustor and combustion chamber.
  48. Tobik,Steven E.; Sattinger,Stanley S.; Ohri,Rajeev; Koenig,Michael H., Resonator performance by local reduction of component thickness.
  49. Schilp, Reinhard; Sutcu, Muzaffer, Resonator system with enhanced combustor liner cooling.
  50. Stoia, Lucas John; DiCintio, Richard Martin; Melton, Patrick Benedict; Romig, Bryan Wesley; Slobodyanskiy, Ilya Aleksandrovich, System and method for a multi-wall turbine combustor.
  51. Nguyen, Quoc Hoai; Kim, Kwanwoo; Epperson, Whitney; Pastecki, Patrick Edward; Mueller, Mark Anthony, System and method for tuning resonators.
  52. Kim, Kwanwoo; Narra, Venkateswarlu; Jain, Praveen Kumar Babulal; Bethke, Sven Georg, System for damping oscillations in a turbine combustor.
  53. Pollarolo, Giacomo, System for damping thermo-acoustic instability in a combustor device for a gas turbine.
  54. Kodukulla, Sridhar Venkat; Chila, Ronald James; Crothers, Sarah Lori; Rao, Shreekrishna Jayakumar; Srinivasan, Shivakumar, Turbomachine combustor assembly including a vortex modification system.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로