Hub-mounted electric blade pitch control
An electromechanical blade pitch control system includes a propeller hub, a blade having an adjustable pitch angle, and a blade bearing hub operably coupled to the blade. The system includes a linear actuator operably coupled to the blade bearing hub and a rotary actuator operably coupled to the linear actuator via a planetary gear system. The system is configured such that the blade bearing hub, linear actuator, and rotary actuator are housed within the propeller hub, and further configured such that actuation of the linear actuator results in a change in a pitch angle of the blade.
1. An electromechanical blade pitch control system, comprising: a propeller hub; a blade having an adjustable pitch angle; a blade bearing hub operably coupled to the blade; a linear actuator operably coupled to the blade bearing hub; and a rotary actuator operably coupled to the linear actuator via a planetary gear system; wherein the blade bearing hub, linear actuator, and rotary actuator are housed within the propeller hub; and wherein actuation of the linear actuator results in a change in a pitch angle of the blade; wherein the rotary actuator includes an electric motor; wherein the rotary actuator further includes a resolver configured to provide positional feedback on the electric motor; and a slip ring assembly connected to and in data communication with the rotary actuator, the slip ring assembly comprising: a signal brush block connected to and in data communication with the resolver; and a power brush block connected to and in data communication with the electric motor.
2. The system of claim 1 , wherein the linear actuator is a ball screw having a ball nut configured to translate linearly along an axis of rotation of the ball screw in response to rotation of the ball screw, the ball nut being operably coupled to the blade bearing hub.
3. The system of claim 1 , wherein the rotary actuator includes a power-off brake upstream of the linear actuator.
4. The system of claim 1 , wherein the rotary actuator is arranged fore of the blade.
5. The system of claim 1 , further comprising an electronic controller connected to and in data communication with the slip ring assembly, the controller being configured to receive an input from a pilot input device and effectuate the rotary actuator in response to the input from the pilot input device.
6. The system of claim 1 , wherein a loss of power to the blade pitch control system biases the blade towards a feathering blade pitch angle.
7. An electromechanical blade pitch control system, comprising: a propeller hub; a blade having adjustable pitch angle; a blade bearing hub operatively coupled to the blade; a ball screw having a ball nut, the ball nut being configured to translate linearly in response to rotational movement of the ball screw, the ball nut being operably coupled to the blade bearing hub; an electric motor; and a planetary gear system which transfers rotational motion from the electric motor to the ball screw, wherein: the blade bearing hub, the ball screw, the ball nut, and the electric motor are housed within the propeller hub; the electric motor is arranged fore of the blade; and, rotating the ball screw results in a change in a pitch angle of the blade; a resolver configured to provide positional feedback on the electric motor; and a slip ring assembly comprising: a signal brush block connected to and in data communication with the resolver via at least one signal line; and a power brush block connected to and in data communication with the electric motor via at least one power line.
8. The system of claim 7 , further comprising a power-off brake upstream of the ball screw, the ball nut, and the blade bearing hub.
9. The system of claim 7 , further comprising an electronic controller comprising a processor and non-transitory computer memory and being configured to effectuate the electric motor in response to an input.
10. The system of claim 9 , wherein the input is generated by a pilot input device connected to and in data communication with the controller, the pilot input device being selected from the group consisting of: a lever, a button, a pedal, a throttle, a joystick, a yoke, a control wheel, a center stick, a sidestick, and a touchscreen.
11. The system of claim 9 , further comprising at least one sensor in data communication with the controller, the sensor being configured to determine an incidence pitch of the blade.