The aircraft fuselage of burn-through resistant

The aircraft fuselage of burn-through resistant

  • CN 101,977,810 B
  • Filed: 03/17/2009
  • Issued: 04/20/2016
  • Est. Priority Date: 03/28/2008
  • Status: Active Grant
First Claim
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1. an aircraft fuselage (12), comprising:

  • at least one being arranged in described aircraft fuselage (12) has the space of floor (14);

    And ventral rectifying device (26),Wherein, described floor (14) comprise one or more floor panel (16),It is characterized in that, described ventral rectifying device (26) and described floor panel (16) during at least four minutes in resist outside burning towards described space from described aircraft fuselage (12), andWherein, described aircraft fuselage (12) to be in below described floor (14) and the region being in the top of described ventral rectifying device (26) does not comprise burn-through resistant isolation layer.

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