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특허 상세정보

System for joining acoustic cellular panel sections in edge-to-edge relation

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/00   
미국특허분류(USC) 181/213; 181/210; 181/214; 181/292; 029/52501; 029/52511
출원번호 US-0959156 (2010-12-02)
등록번호 US8028797 (2011-09-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Womble Carlyle Sandridge & Rice, PLLC
인용정보 피인용 횟수 : 5  인용 특허 : 16
초록

The invention includes a joint assembly for connecting first and second longitudinal edges of portions of an acoustic barrel or panel having an open cell core, a perforated inner skin, and an outer skin. The joint assembly includes at least one strip covering a plurality of openings in walls of cells along the first and second longitudinal edges. The strip is separate from the inner and outer skins. A plate includes a first portion connected to the outer skin proximate to the first longitudinal edge, and a second portion connected to the outer skin proxi...

대표
청구항

What is claimed is: 1. A method of maximizing the available acoustic area of an engine nacelle inner barrel having an acoustic cellular core, a perforated inner skin, an outer skin, and at least one longitudinal seam extending between opposing edges of the acoustic cellular core, the method comprising:(a) providing an acoustic cellular core having a first cut edge and a second cut edge;(b) covering the first cut edge of the cellular core such that substantially all of the cells along the first cut edge remain substantially unobstructed;(c) covering the s...

이 특허에 인용된 특허 (16)

  1. Sanicki,Scott; Costa,Mark W.. Acoustic mechanical retainer. USP2007117296656.
  2. Porte, Alain; Pascal, Nathalie; Thezelais, Sylvain; Rambaud, Eric. Acoustically resistive layer for an acoustical attenuation panel, panel using such a layer. USP2004086772857.
  3. Porte, Alain; Batard, Herv?. Aircraft engine pod with acoustic attenuation. USP2005056896099.
  4. Harrison, Geoffrey E.. Annular acoustic panel. USP2005076920958.
  5. Dhoore Louis G. (Seattle WA) Schultz William H. (Bellevue WA). Combination bulk absorber-honeycomb acoustic panels. USP1980114235303.
  6. Porte, Alain; Lalane, Jacques. Device for connecting two tubular pieces of an aircraft turbine engine. USP2005026857669.
  7. Franklin Alonzo W. ; O'Neill Timothy M.. Method and apparatus for honeycomb core splicing. USP2000016017413.
  8. Strandgaard Christian,DKX. Method of manufacturing a sandwich board and a sound insulating structure. USP2001096290021.
  9. Alan R Maguire GB. Nacelle assembly for a gas turbine engine. USP2002036360989.
  10. Porte Alain,FRX ; Andre Robert,FRX. Noise reducing connection assembly for aircraft turbine housings. USP2000096123170.
  11. Anderson Robert E. (Huntington Station NY) Parente Charles A. (Oyster Bay NY). One-piece engine inlet acoustic barrel. USP1996125581054.
  12. Anderson Robert Elon ; Parente Charles A.. One-piece engine inlet acoustic barrel. USP1998065768778.
  13. Jessup Jerry R. ; Perez ; Sr. Richard. Structural bonding process with encapsulated foaming adhesive. USP1999085938875.
  14. Douglas, Alan Richard. System for joining acoustic cellular panel sections in edge-to-edge relation. USP2011017866440.
  15. Porte, Alain. Tubular acoustic attenuation piece for an aircraft jet engine air intake. USP2004076761245.
  16. Costa, Mark W.; Brown, Charles; Foose, Andrew S.. Zero acoustic splice fan case liner. USP2010097797809.