Patent ID: 9476360
Filing Date: 2016-10-25
CPC Classification: B64C,B64D,F02C,F05D

Claim Text:
1. A method of automatically regulating a power plant of an aircraft having a turbine engine, the engine being operable in an idling mode of operation and having a gas generator and a free turbine, the method comprising: during a selection step (STPO); selecting that the engine be operated in the idling mode of operation; during a regulation step (STP wherein operating the engine in compliance with the idling mode of operation during the regulation step (STP during the regulation step (STP determining an electricity generation target (ITOT) that the power plant is to deliver in order to satisfy a second one of the operational and hierarchically ordered conditions; and when the power plant cannot deliver the electricity generation target while the gas generator is operating at the first original gas generator speed of rotation level (Ng