$\require{mediawiki-texvc}$

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.

Active noise control using noise source having adaptive resonant frequency tuning through variable ring loading 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-025/00
출원번호 US-0143603 (1993-11-01)
발명자 / 주소
  • Pla Frederic G. (Schenectady NY) Rajiyah Harindra (Clifton Park NY) Renshaw Anthony A. (Albany NY) Hedeen Robert A. (Clifton Park NY)
출원인 / 주소
  • General Electric Company (Schenectady NY 02)
인용정보 피인용 횟수 : 36  인용 특허 : 0

초록

A noise source for an aircraft engine active noise cancellation system in which the resonant frequency of noise radiating structure is tuned to permit noise cancellation over a wide range of frequencies. The resonant frequency of the noise radiating structure is tuned by a plurality of drivers arran

대표청구항

An apparatus for minimizing noise emanating from an aircraft engine which has an outer shroud and a fan, said apparatus comprising: means for inducing vibrations coupled to said outer shroud; means for applying a variable force to said outer shroud; means for producing a blade passage frequency sign

이 특허를 인용한 특허 (36)

  1. Welsh William A. ; Yoerkie ; Jr. Charles A., Active noise control system for a defined volume.
  2. Welsh William A. ; Yoerkie ; Jr. Charles A., Active noise control system for a helicopter gearbox mount.
  3. Patrick William P., Active noise control using phased-array active resonators.
  4. Rossetti Dino J. ; Ivers Douglas E. ; Norris Mark A. ; Heath Michael C. ; Southward Steve C., Active structural control system and method including active vibration absorbers (AVAS).
  5. Ross Colin F. (Great Shelford GBX) Langley Andrew J. (Welwyn GBX), Active vibration control system for aircraft.
  6. Kraft Robert E. (Cincinnati OH) Syed Asif A. (Loveland OH), Actively controlled acoustic treatment panel.
  7. Thomas, John E., Appliance incorporating sound cancellation system.
  8. Breitbach, Harald; Gerner, Christian; Sachau, Delf, Device and method for reducing sound of a noise source in narrow frequency ranges.
  9. Berkhoff, Arthur Perry, Device for actively reducing sound transmission, and panel comprising such device.
  10. Obosu,Charles Borromeo; Chitti,Mallikarjuna Sarma, Extended venturi fan ring.
  11. Okada Takayuki,JPX, Fan noise canceller.
  12. Okada Takayuki,JPX, Fan noise canceller.
  13. Olsen,Ronald F.; Breer,Marlin D., Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods.
  14. Busekros, Armin; Kramer, Thomas; Fischer, Jochem; Hoffmann, Juergen, Gas turbine air intake manifold controllably changing a mechnical rigidity of the walls of said intake manifold.
  15. Bouchard, Richard; Pietrobon, John; Durocher, Eric, Gas turbine exhaust case.
  16. Chelin, Frédéric; Leconte, Cedric; Montetagaud, Fabienne, Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle.
  17. Breer, Marlin D.; Olsen, Ronald F.; Kunze, Jr., Robert K.; Riedel, Brian L., Method and apparatus for aircraft inlet ice protection.
  18. Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel, Method and apparatus for aircraft inlet ice protection.
  19. Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel, Method and apparatus for aircraft inlet ice protection.
  20. Hilbert Gary R. ; Pearson David D. ; Crawley Edward F., Method and apparatus for damping vibration in turbomachine components.
  21. Shah, Anil D.; Gupta, Alankar, Method and apparatus for detecting conditions conducive to ice formation.
  22. Shah,Anil D.; Gupta,Alankar, Method and apparatus for detecting conditions conducive to ice formation.
  23. Friddell,Stephen D.; Prichard,Alan K., Method and apparatus for liquid containment, such as for aircraft fuel vessels.
  24. Travis Matt H. (Fall City WA), Method and apparatus for minimizing aircraft cabin noise.
  25. Jones, Kennie H; Nark, Douglas M.; Jones, Michael G.; Parrott, Tony L.; Lodding, Kenneth N., Method of adjusting acoustic impedances for impedance-tunable acoustic segments.
  26. Gautier, Jr., Stanford Joseph; Mezenner, Rabah; Long, Randy, Methods and apparatus for manufacturing semiconductor devices.
  27. Zwinger, Steven F.; Gross, Kenny C.; Urmanov, Aleksey M., Mitigating mechanical vibrations caused by a fan in a computer system.
  28. Atassi, Oliver V., Nacelle with porous surfaces.
  29. Van Nostrand William C. ; Parente Charles A. ; Arcas Noe, Noise absorption system having active acoustic liner.
  30. Lee Seungbae,KRX, Noise killing system of fans.
  31. Porte, Alain, Process for de-icing by forced circulation of a fluid, an air intake cowling of a reaction motor and device for practicing the same.
  32. Kentaro Nakamura JP, Resonator-integrated fan shroud and resonator-integrated fan shroud with air intake duct.
  33. May Daryl N. ; Chapkis Robert L., Rotating machinery noise control device.
  34. Welsh, William A., System for active noise reduction.
  35. Nicgorski, Dana, Systems and methods for avoiding resonances excited by rotating components.
  36. Cheng C. Raymond ; McIntosh Jason D. ; Zuroski Michael T. ; Eriksson Larry J., Tunable acoustic 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