Aircraft firewall

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Reexamination Certificate

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Reexamination Certificate

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07819359

ABSTRACT:
The present invention relates to an aircraft firewall (12) separating first and second compartments (1and2) of the aircraft, the first compartment (1) containing a plurality of elements. The firewall (12) is provided with a first wall (3) inserted in the structure (5) of the aircraft and having a first surface (3′) facing the first compartment (1), and the firewall (12) is provided with regulator elements (4, 13) for maintaining the maximum temperature of the first surface (3′) of the first wall (3) at a predetermined temperature value lower than the self-combustion temperature of the elements.

REFERENCES:
patent: 2986878 (1961-06-01), Townsend
patent: 4177693 (1979-12-01), Ivanko et al.
patent: 4291530 (1981-09-01), Ballard
patent: 7090165 (2006-08-01), Jones et al.
patent: 2004/0093850 (2004-05-01), Horii et al.
patent: 0 893 589 (1999-01-01), None
patent: 1 150 590 (1958-01-01), None
patent: 2 855 497 (2004-12-01), None
patent: 1 212 109 (1970-11-01), None
patent: 2 317 825 (1998-04-01), None
patent: 03/033345 (2003-04-01), None

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