The controller is operable to control a flow rate of a fuel supplied to the gas turbine engine responsive to a power demand on the auxiliary power unit, and also to restrict an inlet air flow into the gas turbine engine, so as to maintain an air pressure inside the aircraft cabin within a pre-determined range.
AUXILLARY POWER UNIT ASSEMBLY AND A METHOD OF USING THE SAME
09.02.2017
Patent
Elektronische Ressource
Englisch
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