Method for generating hydraulic power in an aircraft, use of a hybrid power control unit and drive system
A method for generating hydraulic power in an aircraft, the aircraft having a drive system comprising at least one transmission shaft connected to a power control unit, the power control unit having an electric motor and a hydraulic displacement machine connected to a differential gear unit for driving a common output shaft. The method includes switching the hydraulic displacement machine into a pump mode, arresting the output shaft, rotating the electric motor such that the hydraulic displacement machine is driven due to the arrested output shaft and supplying the fluid flow into a hydraulic system. A drive system of an aircraft may thereby be used for either moving control surfaces or for generating hydraulic power in an aircraft. This hydraulic power may be used to cover hydraulic load peaks during aircraft operation or to power hydraulic devices without the need of additional hydraulic power generation components.
1. A method for generating hydraulic power in an aircraft, the aircraft having a drive system comprising at least one transmission shaft connected to a hybrid power control unit, the power control unit having an electric motor and a hydraulic displacement machine connected to a differential gear unit for driving a common output shaft, the method comprising:
arresting the output shaft;
rotating the electric motor such that the hydraulic displacement machine is driven due to the arrested output shaft; and
supplying the fluid flow into a hydraulic system of said aircraft.
2. The method of claim 1 , wherein arresting the output shaft comprises arresting at least one first brake connected to the at least one transmission shaft.
3. The method of claim 2 , wherein the at least one first brake is at least one wing tip brake.
4. The method of claim 1 , wherein rotating the electric motor includes releasing a second brake at the hydraulic displacement machine and a third brake at the electric motor.
5. The method of claim 4 , wherein the second brake is a pressure-off brake and wherein releasing the second brake includes driving a brake release unit coupled with the pressure-off brake to release the pressure-off brake in case the corresponding hydraulic system is not pressurized.
6. The method of claim 1 , wherein a control unit controls at least one of the speed of the electric motor and a displacement of the hydraulic displacement machine for adjusting a resulting hydraulic pressure or flow rate.