A fuel control system for an aircraft engine, comprises a fuel feed conduit including an inlet end and an outlet end. A fuel metering mechanism is disposed in the fuel feed conduit between the inlet end and the outlet end operable to regulate flow through the fuel feed conduit. A position feedback sensor is operatively connected to the fuel metering mechanism and operable to generate a signal indicative of a position of the fuel metering mechanism.
CONTROLLING GASEOUS FUEL FLOW
CONTROLE DU FLUX DE CARBURANT GAZEUX
27.01.2023
Patent
Elektronische Ressource
Englisch
GASEOUS FUEL SUPPLY SYSTEM AND METHOD FOR OPERATING THE GASEOUS FUEL SUPPLY SYSTEM
Europäisches Patentamt | 2021
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