Aircraft engine cowl door movement control system and method

Patent metadata

Field	Value
Publication number	US-9701414-B2
Application number	US-201314063247-A
Country	US
Kind code	B2
Filing date	Oct 25, 2013
Priority date	Sep 16, 2013
Publication date	Jul 11, 2017
Grant date	Jul 11, 2017

Abstract

A system and method are provided for controlling the movement of an aircraft engine cowl door between an open position and a closed position. The system includes an electric motor, at least one actuator, and an electrically operated brake. The actuator is coupled to the motor and is operable to move the cowl door between the closed and the open position. The electrically operated brake is coupled to the electric motor and the at least one actuator and is configured, upon being energized, to supply a unidirectional resisting torque load to the electric motor that does not prevent motor rotation.

First claim

What is claimed is:

1. A system for controlling movement of an aircraft engine cowl door between an open position and a closed position, comprising:
an electric motor configured, upon being energized, to generate a torque;
at least one actuator coupled to the motor and operable to move the cowl door between the closed and the open position;
an electrically operated brake coupled between the electric motor and the at least one actuator to thereby transfer the torque generated by the electric motor to the actuator, the electrically operated brake configured, upon being energized, to supply a resisting torque load to the electric motor that does not prevent motor rotation;
a power source configured to supply electric power; and
a controller coupled to the power source, to the electric motor, and to the electrically operated brake, the controller including a cowl position control switch and configured to (i) controllably energize the electric motor and (ii) controllably energize the electrically operated brake,
wherein:
the cowl position control switch has an OPEN position, a CLOSE position, and a HOLD position,
in the OPEN position, the cowl position control switch electrically couples the motor to the power source and electrically isolates the electrically operated brake from the power source;
in the CLOSE position, the cowl position control switch electrically couples both the motor and the electrically operated brake to the power source; and
in the HOLD position, the cowl position control switch electrically isolates both the motor and the electrically operated brake from the power source.

2. The system of claim 1 , further comprising:
a second electrically operated brake coupled to the electric motor and configured to selectively supply a braking torque to the motor that prevents motor rotation.

3. The system of claim 1 , wherein the actuator comprises:
a rotationally mounted ball screw shaft, the ball screw shaft coupled to receive torque supplied by the electric motor and configured, upon receipt thereof, to rotate; and
a ball nut rotationally supported on the ball screw shaft, the ball nut configured to translate in response to rotation of the ball screw shaft.

4. The system of claim 1 wherein:
the controller is further configured to controllably supply current to the electrically operated brake, the current having a current magnitude; and
the electrically operated brake is configured, upon receipt of the current, to supply the resisting torque load at a magnitude that is proportional to the current magnitude.

5. The system of claim 1 , further comprising:
an open limit switch disposed at least proximate the actuator, the open limit switch configured to sense when the actuator is in a fully extended position and, in response thereto, to supply a signal representative thereof; and
a close limit switch disposed at least proximate the actuator, the close limit switch configured to sense when the actuator is in a fully retracted position and, in response thereto, to supply a signal representative thereof.

6. The system of claim 1 , wherein the electrically operated brake comprises a hysteresis brake.

7. The system of claim 1 , further comprising:
a gear box coupled between the electrically operated brake and the at least one actuator; and
a manual drive coupled to the gear box.

8. A system for controlling movement of an aircraft engine cowl door between an open position and a closed position, comprising:
an electric motor configured, upon being energized, to generate a torque;
at least one actuator coupled to the motor and operable to move the cowl door between the closed and the open position;
a first electrically operated brake coupled to the electric motor and configured to selectively supply a braking torque to the motor that prevents motor rotation;
a second electrically operated brake coupled between the electric motor and the at least one actuator to thereby transfer the torque generated by the electric motor to the actuator, the second electrically operated brake configured, upon being energized, to supply a resisting torque load to the electric motor that does not prevent motor rotation;
a power source configured to supply electric power;
a controller coupled to the power source, to the electric motor, to the first electrically operated brake, and to the second electrically operated brake, the controller including a cowl position control switch having an OPEN position, a CLOSE position, and a HOLD position, the controller configured to:
controllably energize the electric motor,
controllably energize the first electrically operated brake, and
controllably energize the second electrically operated brake,

wherein:
in the OPEN position, the cowl position control switch electrically couples both the motor and the first electrically operated brake to the power source, and electrically isolates the second electrically operated brake from the power source,
in the CLOSE position, the cowl position control switch electrically couples both the motor and the second electrically operated brake to the power source, and electrically isolates the first electrically operated brake from the power source, and
in the HOLD position, the cowl position control switch electrically isolates the motor, the first electrically operated brake, and the second electrically operated brake from the power source.

9. The system of claim 8 , wherein:
the controller is further configured to controllably supply current to the second electrically operated brake, the current having a current magnitude; and
the second electrically operated brake is configured, upon receipt of the current, to supply the resisting torque load at a magnitude that is proportional to the current magnitude.

10. The system of claim 8 , further comprising:
an open limit switch disposed at least proximate the actuator, the open limit switch configured to sense when the actuator is in a fully extended position and, in response thereto, to supply a signal representative thereof; and
a close limit switch disposed at least proximate the actuator, the close limit switch configured to sense when the actuator is in a fully retracted position and, in response thereto, to supply a signal representative thereof.

11. The system of claim 8 , wherein the actuator comprises:
a rotationally mounted ball screw shaft, the ball screw shaft coupled to receive torque supplied by the electric motor and configured, upon receipt thereof, to rotate; and
a ball nut rotationally supported on the ball screw shaft, the ball nut configured to translate in response to rotation of the ball screw shaft.

12. The system of claim 8 , wherein the second electrically operated brake comprises a hysteresis brake.

13. The system of claim 8 further comprising:
a gear box coupled between the electrically operated brake and the at least one actuator; and
a manual drive coupled to the gear box.

Assignees

• Honeywell Int Inc

Inventors

• Vaughan Ron
• Fizer Leroy Allen
• Wawrzynek James
• Chakkera Kevin K
• Salam Mohamed A
• Warr William
• Birn Stephen

Classifications

• B64D29/06 Primary

  Attaching of nacelles, fairings or cowlings · CPC title

• F16H25/2204

  with balls · CPC title