초록 ▼

An electromechanical inlet guide vane actuation system includes one or more electric motor driven actuators that are used to appropriately position the inlet guide vanes in a gas turbine engine. The actuation system includes a control circuit that supplies guide vane actuation control signals in res

An electromechanical inlet guide vane actuation system includes one or more electric motor driven actuators that are used to appropriately position the inlet guide vanes in a gas turbine engine. The actuation system includes a control circuit that supplies guide vane actuation control signals in response to guide vane position command signals it receives. The guide vane actuation control signals are supplied to one or more electric motors, which position actuators, and thus the inlet guide vanes, to the commanded position.

대표청구항 ▼

We claim: 1. A variable inlet guide vane actuation system, comprising a control circuit including a primary channel and a secondary channel, each channel adapted to receive one or more guide vane position control signals and operable, in response thereto, to selectively supply guide vane actuation

We claim: 1. A variable inlet guide vane actuation system, comprising a control circuit including a primary channel and a secondary channel, each channel adapted to receive one or more guide vane position control signals and operable, in response thereto, to selectively supply guide vane actuation control signals; a primary electric motor coupled to receive the guide vane actuation control signals from the primary channel and operable, in response thereto, to supply a drive force; a secondary electric motor coupled to receive the guide vane actuation control signals from the secondary channel and operable, in response thereto, to supply a drive force; and an actuator assembly coupled to the primary and secondary electric motors and configured, upon receipt of the drive force therefrom, to selectively move between a closed position and an open position. 2. The system of claim 1, wherein the control circuit is configured such that when the primary channel is active the secondary channel is inactive, and vice-versa. 3. The system of claim 2, the actuator assembly comprises: a differential gear assembly coupled between the primary and secondary electric motors. 4. The system of claim 1, wherein each actuator is adapted to couple to a gas turbine engine unison ring. 5. The system of claim 1, further comprising: an actuator position sensor coupled to the actuator assembly and configured to supply position signals representative of actuator assembly position. 6. The system of claim 1, further comprising: a primary brake assembly coupled to the primary electric motor and configured to selectively (i) engage the primary electric motor, whereby the primary electric motor is prevented from supplying the drive force and (ii) disengage the primary electric motor, whereby the primary electric motor is allowed to supply the drive force; and a secondary brake assembly coupled to the secondary electric motor and configured to selectively (i) engage the secondary electric motor, whereby the secondary electric motor is prevented from supplying the drive force and (ii) disengage the secondary electric motor, whereby the secondary electric motor is allowed to supply the drive force. 7. The system of claim 6, wherein: the primary and secondary channels are further operable, in response to the guide vane position control signals, to selectively supply primary and secondary brake control signals, respectively; and the primary and secondary brake assemblies are coupled to receive the primary and secondary brake control signals, respectively, and are respectively operable, in response thereto, to selectively engage and disengage, respectively, the primary and secondary electric motors. 8. The system of claim 7, wherein the primary and secondary brake assemblies are configured to engage the primary and secondary electric motor, respectively, at least when the brake assembly is de-energized. 9. The system of claim 1, further comprising: a primary rotational position sensor coupled to the primary electric motor and configured to supply one or more signals representative of a rotational position of the primary electric motor; and a secondary rotational position sensor coupled to the secondary electric motor and configured to supply one or more signals representative of a rotational position of the secondary electric motor. 10. The system of claim 9, wherein: the primary channel (i) is coupled to receive the primary motor rotational position signals from the primary rotational position sensor and (ii) is configured to supply the guide vane actuation control signals based at least in part on the primary motor rotational position signals; and the secondary channel (i) is coupled to receive the secondary motor rotational position signals from the secondary rotational position sensor and (ii) is configured to supply the guide vane actuation control signals based at least in part on the secondary motor rotational position signals. 11. The system of claim 1, wherein the primary and secondary electric motors are each brushless DC motors. 12. The system of claim 1, wherein the primary and secondary electric motors are each AC induction motors. 13. A gas turbine engine system, comprising: an engine case; a turbine mounted at least partially within the engine case and having a plurality of moveable inlet guide vanes; a hardened unison ring rotationally coupled between the engine case and each of the inlet guide vanes; and a guide vane actuation control system including: a control circuit including a primary channel and a secondary channel, each channel adapted to receive one or more guide vane position control signals and operable, in response thereto, to supply guide vane actuation control signals, a primary electric motor coupled to receive the guide vane actuation control signals from the primary channel and operable, in response thereto, to supply a drive force, a secondary electric motor coupled to receive the guide vane actuation control signals from the secondary channel and operable, in response thereto, to supply a drive force, and an actuator assembly coupled between the primary and secondary electric motors and the unison ring, the actuator assembly configured, upon receipt of the drive force therefrom, to selectively rotate the unison ring in either a first or a second direction, to thereby selectively move the inlet guide vanes between a closed position and an open position, respectively.