Patent ID: 9340296
Filing Date: 2016-05-17
CPC Classification: B64D,Y02T,Y10T

Claim Text:
1. A fuel storage device for an aircraft, comprising: at least one main reservoir, the at least one main reservoir being designed to contain a first batch of fuel; at least one feed line for supplying at least one propulsion engine of the aircraft with the first batch of fuel contained in the at least one main reservoir; at least one auxiliary reservoir designed to contain a second batch of fuel separate from the first batch of fuel, the at least one auxiliary reservoir being connected to the at least one main reservoir, an intake line for bringing the second batch of fuel contained in the at least one auxiliary reservoir to a combustion chamber of the aircraft independent of the at least one propulsion engine of the aircraft, and a transfer pump for transferring the first batch of fuel to the at least one auxiliary reservoir.