A fuel system for an aircraft includes a fuel collector downstream of a boost pump and upstream of an engine fuel pump. Said fuel collector (is mounted in a fuel tank and of an open bowl shape so as to collect fuel therein permitting fuel to continuously overflow therefrom. The system further comprises an inverted fuel collector extending over said fuel collector.
FUEL FEED SYSTEM
KRAFTSTOFFZUFÜHRSYSTEM
SYSTÈME D'ALIMENTATION EN CARBURANT
2018-09-12
Patent
Electronic Resource
English