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Continuously wound filament structure for use in noise attenuation element 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B32B-003/12
출원번호 US-0687905 (1984-12-31)
발명자 / 주소
  • Chee Wan T. (Bellevue WA) Quigley George W. (Bellevue WA)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 27  인용 특허 : 5

초록

An engine inlet sound diffusion structure for use with a turbofan engine is constructed of nonmetallic composite materials. An inner perforated skin of the diffuser is made up of continuously wound composite material filaments. A honeycomb core is sandwiched between the inner porous skin and a nonpo

대표청구항

An acoustic treatment structure for use in the inlet of a turbofan engine formed by the process of filament winding an inner porous skin over a mandrel shaped to substantially conform to the inner shape of the turbofan inlet, said mandrel having pins protruding from the surface thereof, said pins be

이 특허에 인용된 특허 (5)

  1. Rhodes Marvin D. (Yorktown VA) Mikulas ; Jr. Martin M. (Williamsburg VA), Composite sandwich lattice structure.
  2. Trainor James T. (Huntington CT) Covaleski Stanley F. (Milford CT), Laminated aramid fiber friction members.
  3. Holmes Richard N. (Laguna Beach CA), Lock core panel.
  4. Hilliard ; Lonnie George ; Verzemnieks ; Juris, Low non-linearity factor sound attenuating laminate.
  5. Smith Bruce W. (Nipomo CA), Stiffened structural laminate and method of molding laminate with stiffener beads.

이 특허를 인용한 특허 (27)

  1. Lorch Frederick A. ; Sharp Gordon P. ; Succi George, Acoustic resonator.
  2. McGrath Ralph D., Acoustical diffuser assembly and method of installation.
  3. Porte Alain,FRX ; Andre Robert,FRX ; Batard Herve,FRX, Acoustically resistive layer, process for production of this layer and absorbent acoustic panel provided with at least one such layer, as well as its process for production.
  4. Hethcock, James D.; Nunn, Kenneth E.; Oldroyd, Paul, Composite core and method of making same.
  5. Obeshaw, Dale Francis, Contoured crushable composite structural members and methods for making the same.
  6. Obeshaw, Dale Francis, Contoured metal structural members and methods for making the same.
  7. Journade, Frederic; Lafont, Laurent, Engine assembly for aircraft with sliding nacelle.
  8. Welch John M. ; Popp Thomas D. ; Wikstrom Robert F. ; Stratton Terry W. ; Kitt Brian R., Engine nacelle acoustic panel with integral wedge fairings and an integral forward ring.
  9. Welch John M. ; Benton William E. ; Lobsinger Michael R., Engine nacelle outer cowl panel with integral track fairings.
  10. Hull H. Robert (San Leandro CA), Formable honeycomb panel.
  11. Mathon, Richard; Patrigeon, Olivier, Former for fabricating a composite material casing for a gas turbine.
  12. Welch John M. ; Popp Thomas D. ; Baca Leonard L., Method for forming a composite acoustic panel.
  13. Le Borgne, Benedicte Marie; Camus, Erwan; Schneider, Julien, Method for manufacturing a turbine-engine fan casing having an acoustic coating.
  14. Porte, Alain; Batard, Hervé, Method for producing a panel comprising an adapted acoustically resistive layer and panel so obtained.
  15. Francis W. Moore, Method for transferring heat in an aircraft engine thrust reverser.
  16. Herup Eric ; Huybrechts Steven ; Griffin Steven ; Tsai Stephen, Method of making composite chambercore sandwich-type structure with inherent acoustic attenuation.
  17. Vermilyea, Mark Ernest; Kirkpatrick, Bowden; Shoemaker, Philip Alexander; Vernes, Terrence Paul, Method of manufacture of composite laminates, an assembly therefor, and related articles.
  18. Obeshaw, Dale Francis, Modified contoured crushable structural members and methods for making the same.
  19. Kowal, Adam; Hein, Jeff M.; Wilcox, David E., Monolithic acoustically-treated composite structures and methods for fabricating the same.
  20. Kowal, Adam; Hein, Jeffrey; Wilcox, David E., Monolithic acoustically-treated composite structures and methods for fabricating the same.
  21. Diamond, John Anthony, No-septum acoustic sandwich panel, and apparatus and method for suppressing noise in a nozzle.
  22. Moore Francis W., Non-metallic thermally conductive honeycomb thrust reverser inner wall.
  23. Fran.cedilla.ois Monget FR; Patrick Decraecker FR, Process for depositing by winding on a support several rovings simultaneously of pre-impregnated fibers, device for practicing the same, and structure of a composite material thus obtained.
  24. Gumz Dale M., Protective liner for freezers.
  25. Welch John M. ; Popp Thomas D. ; Wikstrom Robert F. ; Stratton Terry W. ; Kitt Brian R., Reinforcing structure for engine nacelle acoustic panel.
  26. Obeshaw, Dale Francis, Shaped contoured crushable structural members and methods for making the same.
  27. Moore Francis W., Thrust reverser inner wall.
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