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
2023-01-27
Patent
Elektronische Ressource
Englisch
GASEOUS FUEL SUPPLY SYSTEM AND METHOD FOR OPERATING THE GASEOUS FUEL SUPPLY SYSTEM
Europäisches Patentamt | 2021
|GASEOUS FUEL SUPPLY SYSTEM AND METHOD FOR OPERATING THE GASEOUS FUEL SUPPLY SYSTEM
Europäisches Patentamt | 2021