초록 ▼

A system and method are provided to selectively control lubricant supply flow to one or more rotating machines in an aircraft when the rotating machines are windmilling. A controller determines if the rotating machines are windmilling. When the rotating machines are windmilling, the controller at le

A system and method are provided to selectively control lubricant supply flow to one or more rotating machines in an aircraft when the rotating machines are windmilling. A controller determines if the rotating machines are windmilling. When the rotating machines are windmilling, the controller at least selectively energizes an electric motor driven lubrication pump, to thereby supply lubricant to the windmilling turbomachine.

대표청구항 ▼

1. An aircraft lubrication supply system, comprising: an electric motor operable, upon being energized from a power source, to rotate and supply a drive force;a pump coupled to receive the drive force from the electric motor and operable, upon receipt thereof, to supply lubricant to a rotating machi

1. An aircraft lubrication supply system, comprising: an electric motor operable, upon being energized from a power source, to rotate and supply a drive force;a pump coupled to receive the drive force from the electric motor and operable, upon receipt thereof, to supply lubricant to a rotating machine;a rotational speed sensor operable to sense rotational speed of the rotating machine and to supply a rotational speed signal representative thereof; anda controller adapted to receive one or more signals indicating that the rotating machine is operating in a windmill operational condition and coupled to receive the rotational speed signal from the rotational speed sensor, the controller operable, in response to the one or more signals and to the rotational speed signal, to: (i) determine that the rotating machine is operating in the windmill condition,(ii) determine when the rotational speed exceeds a predetermined value, and(iii) at least selectively energize the electric motor from the power source when (a) the rotating machine is operating in the windmill operational condition and (b) the rotational speed exceeds the predetermined value. 2. The system of claim 1, further comprising: a ram air turbine selectively movable between a stowed position and a deployed position;wherein the one or more signals include a signal that indicates the ram air turbine is in the deployed position. 3. The system of claim 2, wherein: the ram air turbine is configured, when in the deployed position, to receive a flow of ram air and, in response thereto, to generate electrical power; andthe power source from which the motor is energized is the ram air turbine. 4. The system of claim 1, wherein the controller is further operable to: determine an amount of time that the rotational speed exceeds the predetermined speed value; andat least selectively energize the electric motor from the power source at least when (a) the rotating machine is operating in the windmill operational condition, (b) the rotational speed exceeds the predetermined value, and (c) the rotational speed exceeds the predetermined value a predetermined amount of time. 5. The system of claim 4, wherein the controller comprises a timer configured to determine the amount of time that the turbomachine rotational speed exceeds the predetermined speed value. 6. The system of claim 1, further comprising: one or more pressure sensors disposed downstream of the pump, the one or more pressure sensors configured to sense fluid pressure and supply a pressure feedback signal representative thereof to the controller. 7. The system of claim 6, wherein the controller is configured to implement a closed-loop pressure control law that uses the pressure feedback signal. 8. The system of claim 1, further comprising: a motor rotational speed sensor configured to sense motor rotational speed and supply a speed feedback signal representative thereof to the controller. 9. The system of claim 8, wherein the controller implements a closed-loop speed control law that uses the speed feedback signal. 10. The system of claim 1, wherein the controller is further adapted to receive one or more signals representative of aircraft operating conditions. 11. An aircraft lubrication supply system, comprising: a ram air turbine selectively movable between a stowed position and a deployed position, the ram air turbine configured, when in the deployed position, to receive a flow of ram air;a turbomachine disposed to receive a portion of the flow of ram air when the ram air turbine is in the deployed position;a rotational speed sensor coupled to, and operable to supply a rotational speed signal representative of, turbomachine rotational speed;an electric motor operable, upon being energized from a power source, to rotate and supply a drive force;a pump coupled to receive the drive force from the electric motor and operable, upon receipt thereof, to supply lubricant to the turbomachine;a controller adapted to receive a signal representative of ram air turbine position and coupled to receive the rotational speed signal, the controller operable, in response to these signals, to; (i) determine at least when the ram air turbine is in the deployed position,(ii) determine when the turbomachine rotational speed exceeds a predetermined value, and(iii) at least selectively energize the electric motor from the power source at least (a) when the ram air turbine is determined to be in the deployed position and (b) the turbomachine rotational speed exceeds the predetermined value. 12. The system of claim 11, wherein the controller is further operable to: determine an amount of time that the turbomachine rotational speed exceeds the predetermined speed value; andat least selectively energize the electric motor from the power source at least when (a) the ram air turbine is in the deployed position, (b) the turbomachine rotational speed exceeds the predetermined value, and (c) the turbomachine rotational speed exceeds the predetermined value a predetermined amount of time. 13. The system of claim 12, wherein the controller includes a timer configured to determine the amount of time that the turbomachine rotational speed exceeds the predetermined speed value. 14. The system of claim 11, wherein: the ram air turbine is configured, when in the deployed position, to receive a flow of ram air and, in response thereto, to generate electrical power; andthe power source from which the electric motor is energized is the ram air turbine.