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특허 상세정보

Acoustic mechanical retainer

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/40    B64C-001/00    B64C-001/12    B64C-001/06    B64D-033/02    B64D-033/00    F02K-001/82    F02K-001/00   
미국특허분류(USC) 181/210; 181/214; 244/001.N; 244/131; 244/132
출원번호 US-0112946 (2005-04-22)
등록번호 US-7296656 (2007-11-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds
인용정보 피인용 횟수 : 10  인용 특허 : 11
초록

A fan case assembly includes a noise attenuation layer that is covered by a face sheet. The face sheet includes a first plurality of openings. The noise attenuation layer includes a plurality of individual cells that are in communication with at least one of the first plurality of openings. Noise energy is communicated through the first plurality of openings into the individual cells and dissipated to reduce noise emissions. A seam in the face sheet is covered to protect the underlying noise attenuation layer from damage by a retainer. The retainer is b...

대표
청구항

What is claimed is: 1. A liner assembly for a duct comprising: a noise attenuation layer; a face sheet covering said noise attenuation layer including a first plurality of openings and a seam; and a retainer covering said seam including a second plurality of openings for communicating sound energy through said retainer and said face sheet to said noise attenuation layer, wherein said second plurality of openings extend through said retainer and a portion of said face sheet underlying said retainer. 2. A liner assembly for a duct comprising: a noise a...

이 특허에 인용된 특허 (11)

  1. Porte, Alain; Pascal, Nathalie; Thezelais, Sylvain; Rambaud, Eric. Acoustically resistive layer for an acoustical attenuation panel, panel using such a layer. USP2004086772857.
  2. Hart-Smith Leonard J. (Long Beach CA). Aircraft skin lap splice. USP1994035297760.
  3. Stretton, Richard G; Udall, Kenneth F. Cowl structure for a gas turbine engine. USP2005056892526.
  4. Wollaston Tim,GBX ; Pedwell Richard,GBX ; Bush Paul,GBX. Friction welding metal components. USP2001126328261.
  5. Wilkinson Wilfred H. (Turnditch GB2). Metal cavitated sandwich structures. USP1979074161231.
  6. Anderson Robert E. (Huntington Station NY) Parente Charles A. (Oyster Bay NY). One-piece engine inlet acoustic barrel. USP1996125581054.
  7. Buge, Michel; Porte, Alain; Poignonec, Jean-Marc. Process for making a panel with a protected acoustic damping layer and acoustic panel as made. USP2004116820337.
  8. Dublineau, Pascal; Buge, Michel; Porte, Alain. Process for the production of holes particularly micro-perforations in a composite material, device for its practice and sound damping layer constituted by said material. USP2005086923931.
  9. Shuttleworth Richard G. (South Windsor CT) Snyder Gene R. (Vernon CT). Sound absorbing structure. USP1981104293053.
  10. Porte, Alain. Tubular acoustic attenuation piece for an aircraft jet engine air intake. USP2004076761245.
  11. Readnour Jack L. (Ft. Mitchell KY) Wright Jack D. (Mason OH). Variable contour annular air inlet for an aircraft engine nacelle. USP1991035000399.