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특허 상세정보

Fire protection space for aircraft passengers provided with the aid of fuselage skin of fibre-metal laminates

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/10    B64C-001/12    B64C-001/40    A62C-003/08   
미국특허분류(USC) 244/121;
출원번호 US-0595227 (2008-04-14)
등록번호 US-8899523 (2014-12-02)
우선권정보 DE-10 2007 018 753 (2007-04-20)
국제출원번호 PCT/EP2008/054500 (2008-04-14)
§371/§102 date 20100419 (20100419)
국제공개번호 WO2008/128920 (2008-10-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Fenwick & West LLP
인용정보 피인용 횟수 : 0  인용 특허 : 13
초록

This invention provides a fuselage of an aircraft or space vehicle with a fuselage section having an outer skin, wherein at least the outer skin of the fuselage section consists of a glass-fiber reinforced aluminum laminate to form a safety zone for passengers in the event of a fire.

대표
청구항

1. An aircraft or space vehicle comprising a fuselage, wherein the fuselage comprises: a fuselage section forming a safety zone for passengers in the event of a fire, having: an outer skin that includes skin panels having sheet ends, wherein the skin panels consist completely of high static strength glass-fibre reinforced aluminium laminate;stringers and ribs in the safety zone, the stringers provided in a longitudinal direction of the aircraft or space vehicle for longitudinal stiffening and the ribs provided in a transverse direction of the aircraft or...

이 특허에 인용된 특허 (13)

  1. Fay Ralph Michael ; Wulliman Rebecca Sue ; Stacy James Walter ; Townsend Jeffrey Canon ; Volenec Steven N.. Burn through resistant systems for transportation, especially aircraft. USP2001116322022.
  2. Fay, Ralph Michael; Wulliman, Rebecca Sue; Stacy, James Walter; Townsend, Jeffrey Canon; Volenec, Steven N.. Burn through resistant systems for transportation, especially aircraft. USP2003056565040.
  3. Ehrstrom,Jean Christophe; Warner,Timothy. Composite laminated aluminum-glass fiber sandwich panels. USP2006087087317.
  4. Sherman S. Smith. Fire-blocking insulation blanket. USP2002036358591.
  5. Wrenn P. Holman ; Robert W. Dost ; Ernest E. Williams, Jr. ; John A. Wilson ; Raymond H. Horstman. Flow-efficient, static pressure-shielding, fire-resistant decompression panel assembly. USP2002086435455.
  6. Anast, Peter Z.. Light weight and high strength fuselage. USP2003116648273.
  7. Palm, Frank. Metal fiber-reinforced composite material as well as a method for its production. USP2005036861156.
  8. Roebroeks, Gerardus Hubertus Joannes Joseph. Method for making a laminate and laminate obtainable by said method. USP2004056736919.
  9. Andreas Kielies DE; Rolf Beck DE; Guenter Doehle DE. Method of manufacturing a profile member of a hybrid composite material. USP2002106460240.
  10. Stulc,Jeffrey F.; Chan,Wallace C.; Clapp,Brian C.; Rolfes,Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2008027325771.
  11. Assler,Herwig; Schmidt,Hans Juergen. Splicing for interconnected thin-walled metal structures. USP2006047021856.
  12. Liguore, Salvatore L.; Montgomery, Joshua M.. Systems and methods for reducing noise in aircraft fuselages and other structures. USP2010117837147.
  13. Westre Willard N. ; Allen-Lilly Heather C. ; Ayers Donald J. ; Cregger Samuel E. ; Evans David W. ; Grande Donald L. ; Hoffman Daniel J. ; Rogalski Mark E. ; Rothschilds Robert J.. Titanium-polymer hybrid laminates. USP2000096114050.