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특허 상세정보

Duct liner acoustic splice

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-0112642 (2005-04-22)
등록번호 US-7296655 (2007-11-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds
인용정보 피인용 횟수 : 6  인용 특허 : 11

A duct liner assembly includes a noise attenuation layer for absorbing noise energy that is covered by a face sheet. The face sheet includes a seam that is covered by an acoustically active splice. The acoustically active splice includes a plurality of acoustic regions that provide for communication of noise energy to the noise attenuation layer to minimize creation of acoustically dead areas.


What is claimed is: 1. A liner assembly for a duct comprising: a noise attenuation layer; a face sheet over said noise attenuation layer, said face sheet including a plurality of openings and a seam; and a splice for covering said seam, wherein said splice includes an acoustic region open to said plurality of openings within said face sheet, wherein said acoustic region comprises an open area defined by surrounding portions of said splice. 2. The assembly as recited in claim 1, wherein said splice includes a center portion covering said seam and said...

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.