$\require{mediawiki-texvc}$

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.

Slanted cavity resonator 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • G10K-011/04
  • F02K-001/26
  • B64D-033/06
출원번호 US-0673398 (1976-04-05)
발명자 / 주소
  • Tseo Gudin (San Diego CA)
출원인 / 주소
  • Rohr Industries, Incorporated (Chula Vista CA 02)
인용정보 피인용 횟수 : 36  인용 특허 : 0

초록

A combination fan jet engine nozzle plug and muffler. The combination comprises a nozzle plug structure formed from a plurality of inwardly slanted spaced apart elements. The elements form outwardly open and inwardly closed cavities. The cavities\openings are covered by porous skin material attached

대표청구항

A combination engine plug and muffler for a fan jet aircraft engine comprising: a central plug structure formed of a plurality of inward slanting, spaced apart elements, said elements fixedly attached to a center member positioned co-axial with the center line of said engine and fixedly attached the

이 특허를 인용한 특허 (36)

  1. Cicon Dennis E. (Manchester CT), Acoustic treated exhaust plug for turbine engine.
  2. Mercat, Florent, Acoustic treatment device for turbine and combustion noises.
  3. Wynosky Thomas A. (Madison CT), Acoustical turbine engine tail pipe plug.
  4. Gilcreest, Mark D.; Sleath, Trevor G.; Gelzer, Daniel F.; Windels, Merlin C., Acoustically treated exhaust centerbody for jet engines and associated methods.
  5. Peter Joseph E. (Cincinnati OH), Anti-icing noise-suppressing vortex tube assembly.
  6. Matta Ram K. (Loveland OH) Clapper William S. (West Chester OH), Apparatus for suppressing internally generated gas turbine engine low frequency noise.
  7. Nguyen, Phuong H.; Sikora, Joseph A.; Campbell, Thomas A., Automatic control systems for aircraft auxiliary power units, and associated methods.
  8. Nguyen, Phuong H.; Sikora, Joseph A.; Campbell, Thomas A., Automatic control systems for aircraft auxiliary power units, and associated methods.
  9. Nguyen,Phuong H.; Sikora,Joseph A.; Campbell,Thomas A., Automatic control systems for aircraft auxiliary power units, and associated methods.
  10. Ward, Stephen H., Boot for repair of chevron on nacelle.
  11. Vincent, Thomas Alain Christian, Central body for a turbojet exhaust channel, turbojet.
  12. 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.
  13. Smith, James E.; Pertl, Franz A., Compact electromagnetic plasma ignition device.
  14. Campbell, Thomas A.; Chambers, David S.; Willie, Robert H.; Rust, Charles W., Dual flow APU inlet and associated systems and methods.
  15. Campbell,Thomas A.; Chambers,David S.; Willie,Robert H.; Rust,Charles W., Dual flow APU inlet and associated systems and methods.
  16. Spencer, Michael J.; Lowery, Andrew D.; Smith, James E., Dual signal coaxial cavity resonator plasma generation.
  17. Morvant, Romuald, Exhaust cone.
  18. Blanchard, Stephane Pierre Guillaume; Cameriano, Laurent Bernard; Dakowski, Mathieu; Page, Alain Pierre, Exhaust cone for channeling a stream of gas downstream from a turbine.
  19. Honma, Shiro; Tanimoto, Jun; Maruyama, Takashi; Takasugi, Yuji; Yoshida, Tatsuya, Exhaust system for combustion engine.
  20. Mecuson, Gautier; Conete, Eric, Exhaust with an acoustic attenuation system.
  21. Todorovic, Predrag, Gas turbine exhaust cone.
  22. Todorovic, Predrag, Gas-turbine exhaust cone.
  23. Todorovic, Predrag, Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall element.
  24. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin, Independent power generation in aircraft.
  25. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin, Independent power generation in aircraft.
  26. Campbell,Thomas A.; Voll,William A.; Diamond,John A., Integrated axially varying engine muffler, and associated methods and systems.
  27. Chiou, Song; Yu, Jia; Hubert, Claude; Layland, Michael; Kwan, Hwa-Wan, Linear acoustic liner.
  28. Gutmark,Ephraim Jeff; Callender,Bryan W.; Martens,Steven, Method and apparatus for operating gas turbine engines.
  29. Todorovic, Predrag, Method for the production of a sound absorber, especially for a gas turbine exhaust cone.
  30. Gutmark,Ephraim Jeff; Martens,Steven, Methods and apparatus for operating gas turbine engines.
  31. Streib Richard A. (Ellington CT), Muffler plug for gas turbine power plant.
  32. Smith, James E.; Pertl, Franz A., Quarter wave coaxial cavity igniter for combustion engines.
  33. Yu, Jia; Chien, Eugene W., Sound-absorbing exhaust nozzle center plug.
  34. Zielinski, Edward; Bernier, Alan T.; Knechtel, Kent W.; Campbell, Thomas A.; White, Jeffrey J.; Ralston, Mark D., Systems and methods for starting aircraft engines.
  35. Lwasa, Ronald M.; Chow, Allen D., Thermally compliant APU exhaust duct arrangements and associated systems and methods.
  36. Karimi, Kamiar J.; Liu, Shengyi; Liffring, Mark E.; Helton, Steven B.; Fu, Sheau-Wei (Johnny), Vehicle electrical power management and distribution.
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