FIELD: transport.
SUBSTANCE: in fire development, air flows may originate to facilitate fire propagation between aircraft cargo compartment and skin. In compliance with first version, anti-fire barrier is arranged in aforesaid area, i.e. between cargo compartment and skin made up of panel resistant to burn-through. Said barrier is designed to form vent channel to allow a fast reduction in passenger cabin pressure in normal flight conditions and prevention of surface puncture in case of fire. Such anti-fire barrier may be arranged in whatever position in intermediate wall space of said area.
EFFECT: anti-fire protection of aircraft fuselage that inhibits fire propagation.
13 cl, 8 dwg
Title | Year | Author | Number |
---|---|---|---|
PANEL STRUCTURE FOR INNER LINING OF AIRCRAFT PASSENGER CABIN | 2005 |
|
RU2387575C2 |
SET TO INSULATE AIRCRAFT AIRFRAME INNER SURFACE | 2005 |
|
RU2373109C2 |
INSULATION STRUCTURE OF INSIDE INSULATION OF VEHICLE | 2005 |
|
RU2373108C2 |
HULL | 2005 |
|
RU2384462C2 |
ANTI-BURNING-PROOF AIRCRAFT FUSELAGE | 2009 |
|
RU2502634C2 |
LIGHT TWIN-ENGINED MULTI-PURPOSE AIRCRAFT | 1994 |
|
RU2112704C1 |
PRESSURE REDUCTION ELONGATED GATE CONFIGURATION | 2006 |
|
RU2423288C2 |
TWIN-ENGINE MULTI-PURPOSE AIRCRAFT "CHOLOD-1" (VERSIONS) | 2005 |
|
RU2297368C1 |
INSULATING MAT FOR SOUND INSULATION OF AIRPLANE FUSELAGE STRUCTURE AND FASTENING ELEMENT FOR IT | 2007 |
|
RU2429162C2 |
ISOLATION SYSTEM | 2005 |
|
RU2356760C2 |
Authors
Dates
2011-03-20—Published
2007-04-26—Filed