$\require{mediawiki-texvc}$

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.

High frequency dynamics resonator assembly 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/24
출원번호 US-0644563 (2003-08-15)
발명자 / 주소
  • Bland,Robert
  • Ryan,William
출원인 / 주소
  • Siemens Power Generation,Inc.
인용정보 피인용 횟수 : 23  인용 특허 : 12

초록

Aspects of the invention relate to resonator assemblies for use in non-uniform flow environments. The resonator assemblies include one or more features, such as a box or a scoop, for substantially equalizing the pressure on the resonator. In the box configuration, a box is attached on top of the res

대표청구항

What is claimed is: 1. A resonator assembly comprising: a turbine engine component having a plurality of opening therein; a resonator body including a plate having a plurality of openings therein and at least one side wall extending from and about the entire periphery of the plate, the at least one

이 특허에 인용된 특허 (12)

  1. Liu, Zheji, Acoustic liner and a fluid pressurizing device and method utilizing same.
  2. Handscomb Paul,GBX, Apparatus for and method of attenuating acoustic energy.
  3. Motsinger Russell E. (Cincinnati OH) Vdoviak John W. (Marblehead MA), Closed cavity noise suppressor.
  4. Moeller Scott Michael, Combustion turbine modular cooling panel.
  5. Blaser Dwight A. (Sterling Heights MI) Goding David J. (Willow Springs IL), Compact exhaust silencer for diesel locomotives.
  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.
  7. Ross David F. (Scottsdale AZ) Royalty Charles M. (Tempe AZ), Dual flow turbine engine muffler.
  8. Sams Gary W. ; Inman Merle B., Gas burner system providing reduced noise levels.
  9. Stief Reinhard (Weinheim DEX) Schork Roger (Morlenbach DEX) Muller-Broll Gerhard (Rimbach DEX) Jost Thomas (Weinheim DEX) Mattutat Manfred (Ladenburg DEX) Schmitt Klaus-Dieter (Gorxheimertal DEX), Housing Lining.
  10. Sattinger, Stanley S.; Darling, Douglas Dean; Holbert, Roy Kyle; Kepes, William E., Modular resonators for suppressing combustion instabilities in gas turbine power plants.
  11. Hoch Rene G. (La Rochette FRX) Jubelin Bernard J. L. (Cesson FRX) Sarlat Pierre M. A. (Fontainebleau FRX) Thomas Pierre (La Houssaye en Brie FRX), Resonant cavity devices for reducing noise within a duct in the presence of a gaseous fluid.
  12. Lyon Craig A. (Mesa AZ) Ross David F. (Scottsdale AZ) Sheoran Yogendra (Scottsdale AZ), Turbine engine noise suppression apparatus and methods.

이 특허를 인용한 특허 (23)

  1. Huber, Andreas; Noiray, Nicolas; Schuermans, Bruno; Benz, Urs, Combustion device for a gas turbine.
  2. Huber, Andreas; Noiray, Nicolas; Schuermans, Bruno; Benz, Urs, Combustion device for a gas turbine configured to suppress thermo-acoustical pulsations.
  3. 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.
  4. Johnson, Clifford E.; Lepers, Joachim; Wasif, Samer P., Combustor assembly including one or more resonator assemblies and process for forming same.
  5. Bobba, Mohan Krishna; Kim, Kwanwoo; Melton, Patrick Benedict; Antoniono, Carolyn Ashley, Combustor resonator with non-uniform resonator passages.
  6. Hellie, Mark Donald; Arruda, Anthony C.; Shaw, Christopher Edward; Sparks, Joshua, Compact low frequency resonator.
  7. Schilp, Reinhard, Cooling chamber for upstream weld of damping resonator on turbine component.
  8. Schuermans, Bruno; Bothien, Mirko Ruben, Damper for combustion oscillation damping in a gas turbine.
  9. Ito, Takanori; Matsuyama, Keisuke; Ikeda, Kazufumi; Tanimura, Satoshi; Akamatsu, Shinji, Damping device and gas turbine combustor.
  10. Johnson, Clifford E., Flow control through a resonator system of gas turbine combustor.
  11. Liu, Zheji; Kuzdzal, Mark Joseph, Fluid-carrying conduit and method with noise attenuation.
  12. Ikeda, Kazufumi; Mandai, Shigemi; Kawata, Yutaka; Aoyama, Kuniaki; Ono, Masaki; Tanaka, Katsunori, Gas turbine combustor and a gas turbine equipped therewith.
  13. 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.
  14. Brown, William S.; Walczuk, Thomas M.; Noble, Rodney; Dodd, Frederick, Low velocity injector manifold for hypergolic rocket engine.
  15. Theuer, Andre; Palys, Dariusz Oliwiusz; Imfeld, Jost, Method and apparatus for gas turbine combustor inner cap and high frequency acoustic dampers.
  16. Liu, Zheji, Multi-degree of freedom resonator array.
  17. Johnson, Clifford E.; Bland, Robert J.; Gambacorta, Domenico; Wasif, Samer P., Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber.
  18. Norris,James W.; Nordeen,Craig A.; Twelves, Jr.,Wendell V., Pulsed combustion engine.
  19. Davis, Jr., Lewis Berkley; Han, Fei; Srinivasan, Shiva; Singh, Kapil Kumar; Kim, Kwanwoo; Narra, Venkateswarlu, Resonator assembly for mitigating dynamics in gas turbines.
  20. Johnson, Clifford E.; Wasif, Samer P., Resonator device at junction of combustor and combustion chamber.
  21. Schilp, Reinhard; Sutcu, Muzaffer, Resonator system with enhanced combustor liner cooling.
  22. Kim, Kwanwoo; Narra, Venkateswarlu; Jain, Praveen Kumar Babulal; Bethke, Sven Georg, System for damping oscillations in a turbine combustor.
  23. Szwedowicz, Jaroslaw Leszek; Irmisch, Stefan, Thermally loaded, cooled component.
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