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Electric heater for integration into an aircraft acoustic panel 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • E04B-001/86
출원번호 US-0585533 (2012-08-14)
등록번호 US-8919494 (2014-12-30)
발명자 / 주소
  • Burkett, Brian Bobby
  • Botura, Galdemir Cezar
  • Hubert, Claude Marc
  • Sweet, David Bert
  • Zecca, Joseph Christopher
  • Olson, Timothy Robert
출원인 / 주소
  • Rohr, Inc.
대리인 / 주소
    Cantor Colburn LLP
인용정보 피인용 횟수 : 4  인용 특허 : 29

초록

An electric heater (40) for integration into an acoustic panel (20) having sound-penetrating pores (30) communicating with a sound-canceling medium. The heater (40) includes an electrically conductive layer (53) with resistance-setting apertures (63) filled with sealant (73). Openings (83), which co

대표청구항

1. An electric heater for integration into an acoustic panel having sound-penetrating pores; said electric heater comprising: an electrically conductive layer,resistance-setting apertures extending through the conductive layer,sealant filling at least some of the resistance-setting apertures, andsou

이 특허에 인용된 특허 (29)

  1. Chene, Gilles; Gantie, Fabrice; Porte, Alain, Acoustic coating for an aircraft incorporating a frost treatment system by joule effect.
  2. Layland, Michael John; Brown, Keith Towers; Hubert, Claude Marc; Christy, Daniel P., Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein.
  3. Hogeboom William H. ; Bielak Gerald W., Aircraft engine acoustic liner.
  4. Hogeboom William H. ; Bielak Gerald W., Aircraft engine acoustic liner and method of making same.
  5. Botura, Galdemir C.; Flosdorf, David C., Aircraft engine nacelle ice protection system.
  6. Layland, Michael John; Brown, Keith T., Aircraft engine nacelle inlet having access opening for electrical ice protection system.
  7. Layland, Michael John; Brown, Keith T., Aircraft engine nacelle inlet having access opening for electrical ice protection system.
  8. Layland,Michael John; Brown,Keith Towers, Aircraft engine nacelle inlet having access opening for electrical ice protection system.
  9. Layland, Michael John; Brown, Keith Towers, Aircraft engine nacelle inlet having electrical ice protection system.
  10. Jeffrey W. Moe, Aircraft wing and method for reducing airframe-generated noise.
  11. Adee James M. (San Diego CA), Buried element deicer.
  12. Frustie, Valerie; Duprieu, Bernard; Gantie, Fabrice, Coating for acoustic treatment integrating the function of frost treatment with hot air.
  13. Hubert,Claude M.; Christy,Daniel P., Composite ice protection heater and method of producing same.
  14. Rose Philip M. (Chula vista CA), Encapsulated bulk absorber acoustic treatments for aircraft engine application.
  15. Arcas Noe ; Hutto Frederick M. ; Parente Charles A., Extended reaction acoustic liner for jet engines and the like.
  16. Arcas Noe ; Hutto Frederick M. ; Parente Charles A., Extended reaction acoustic liner for jet engines and the like.
  17. Rose Philip M. (Chula Vista CA) Yu Jia (San Diego CA), Honeycomb noise attenuation structure.
  18. Zecca, Joseph Christopher; Botura, Galdemir Cezar; Burkett, Brian Bobby; Hubert, Claude Marc; Layland, Michael John; Olson, Timothy Robert; Roman, James Michael, Ice protection system for a multi-segment aircraft component.
  19. Cloft, Thomas G.; Prihar, Ron I.; Lussier, Darin S., Integrated inlet fan case.
  20. Blackner Anthony M., Jet engine and method for reducing jet engine noise by reducing nacelle boundary layer thickness.
  21. Moe, Jeffrey W.; Wunsch, John J.; Sperling, Michael S., Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip.
  22. Müller, Ulrich, Method for the manufacture of a light-weight sheet.
  23. Parente Charles A. (Oyster Bay NY), Method of making an acoustic attenuating liner.
  24. Hom Felix (La Mesa CA), Method of manufacturing a honeycomb noise attenuation structure and the structure resulting therefrom.
  25. Rose Philip M. (Chula Vista CA) Riel Frank J. (San Diego CA), Method of manufacturing double layer attenuation panel with two layers of linear type material.
  26. Robert Samuel Wilson IE; Richard Parkes IE; Mark Braniff IE, Noise attenuation panel.
  27. Buge,Michel; Porte,Alain; Poignonec,Jean Marc, Process for making a panel with a protected acoustic damping layer.
  28. Cook Billy G. (Chula Vista CA), Sound attenuating structural honeycomb sandwich material.
  29. Taylor Maurice Ian (Allestree EN), Sound attenuating structure.

이 특허를 인용한 특허 (4)

  1. Lumbab, Alex C.; Leisten, Bradley Scott, Aircraft engine nacelle bulkheads and methods of assembling the same.
  2. Lumbab, Alex C.; Leisten, Bradley Scott, Lipskin for a nacelle and methods of making the same.
  3. Lumbab, Alex C.; Leisten, Bradley Scott, Methods and apparatus for noise attenuation in an engine nacelle.
  4. Lumbab, Alex C.; Lan, Justin Honshune; Leisten, Bradley Scott, Noise attenuating lipskin assembly and methods of assembling the same.
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