Method and system for regulating power in the event of at least one aircraft engine failure
AssigneeTurbomeca
InventorJean-Michel Presse
Life of this patent
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AssigneeTurbomeca
InventorJean-Michel Presse
Estimating the term…
A method to optimize resources needed to continue flight if at least one main engine is lost, by relieving a propulsion system that has remained operative of all or some of non-propulsive energy demands, by additional generation of non-propulsive power, operating continuously. The method uses a GPP unit that operates constantly in flight while taking up some of nominal total non-propulsive power of the aircraft, to supply increased non-propulsive power almost instantaneously, based on at least three respective emergency regimes at a time of engine failure. A control and monitoring function of the GPP calculates elapsed time for each emergency regime, and informs a data processing unit thereof, while emitting an alarm if operating periods allocated to each emergency regime are exceeded, and the emergency function adjusts non-propulsive power demands made by the aircraft between main engines and the unit GPP either automatically or on orders of a pilot.
A method for regulating power in event of failure of at least one aircraft engine including a central digital data processing unit providing an emergency function capable of triggering an emergency signal, the method comprising:
Dependencies are inferred from the claim text.