Embodiments of the present invention relate generally to fuel tanks for aviation, and particularly to construction of rigid tank walls that have been found useful in absorbing energy of a magnitude expected during a crash. In some aspects, the rigid tank wall construction includes particular materials, such as a thermoplastic resin matrix. In some aspects, the rigid tank wall construction includes a particular arrangement of reinforcing fibers, such as a twill weave pattern.
AVIATION FUEL TANK WITH RIGID WALL FOR CRASH ENERGY ABSORPTION
2015-10-01
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AVIATION FUEL TANK WITH RIGID WALL FOR CRASH ENERGY ABSORPTION
European Patent Office | 2015
|AVIATION FUEL TANK WITH RIGID WALL FOR CRASH ENERGY ABSORPTION
European Patent Office | 2020
|AVIATION FUEL TANK WITH RIGID WALL FOR CRASH ENERGY ABSORPTION
European Patent Office | 2019
|AVIATION FUEL TANK WITH RIGID WALL FOR CRASH ENERGY ABSORPTION
European Patent Office | 2018
|Aviation fuel tank with rigid wall for crash energy absorption
European Patent Office | 2016
|