Method of supplying power to actuators associated with an aircraft landing gear

摘要

The method involves supplying electrical energy to actuators e.g. electromechanical braking actuators, by a local power supply (26) in a nominal operation mode, where the local power supply is provided with electrical local generators driven by rotation of steering wheels (2) carried by an auxiliary landing gear (1) of an aircraft. Additional energy or total energy is provided to the actuators by a main power supply (100) when delivery of the energy by the local power supply is not sufficient, in an additional operation mode.