Thrust reverser system

Patent metadata

Field	Value
Publication number	US-9482180-B2
Application number	US-201213480299-A
Country	US
Kind code	B2
Filing date	May 24, 2012
Priority date	May 24, 2012
Publication date	Nov 1, 2016
Grant date	Nov 1, 2016

Abstract

A method and apparatus comprising a sleeve, at least one linear electric motor connected to the sleeve, and a controller. The sleeve is configured to move between a first position and a second position. The sleeve exposes a cascade when in the second position. The at least one linear electric motor is configured to move the sleeve between the first position and the second position. The controller is configured to control operation of the at least one linear electric motor to move the sleeve between the first position and the second position.

First claim

What is claimed is:

1. An apparatus comprising:
a sleeve configured to move between a first position and a second position, wherein the sleeve exposes a cascade when in the second position;
at least one linear electric motor directly connected to the sleeve and configured to move the sleeve between the first position and the second position, wherein the at least one linear electric motor comprises: a coil system disposed within a base connected to an engine structure, a member connected to the sleeve, and a magnet system connected to the member and configured to interact with the coil system to linearly move the member relative to the base to cause the sleeve to move between the first position and the second position;
a controller configured to control operation of the at least one linear electric motor to move the sleeve between the first position and the second position; and
a load cell, disposed within the base, configured to send load information to the controller, wherein the controller is further configured to use the load information to maintain a desired load on the at least one linear electric motor.

2. The apparatus of claim 1 , wherein the controller is configured to control operation of the at least one linear electric motor to move the sleeve between the first position and the second position with a desired number of speeds.

3. The apparatus of claim 1 further comprising:
a sensor system configured to measure a position of the sleeve.

4. The apparatus of claim 1 , wherein the controller is configured to synchronize the at least one linear electric motor to move the sleeve.

5. The apparatus of claim 1 , wherein the controller is configured to compensate for a linear electric motor in the at least one linear electric motor that is not functioning as commanded.

6. The apparatus of claim 5 , wherein the controller is further configured to control operation of a group of remaining linear electric motors in the at least one linear electric motor to move the sleeve between the first position and the second position taking into account load changes caused by the linear electric motor to maintain a load on the group of remaining linear electric motors below a selected load.

7. The apparatus of claim 5 , wherein the controller causes the linear electric motor to operate in a mode in which the member that is connected to the sleeve floats such that the linear electric motor does not actively move.

8. The apparatus of claim 1 , wherein the controller is configured to stop the sleeve in at least one of the first position and the second position.

9. The apparatus of claim 1 , wherein the controller is configured to reduce a speed of the at least one linear electric motor while moving the sleeve between the first position and the second position to maintain a load on the at least one linear electric motor caused by moving the sleeve below a selected threshold.

10. The apparatus of claim 1 , wherein the at least one linear electric motor is directly connected to only one sleeve.

11. A thrust reverser system comprising:
a sleeve configured to move between a first position and a second position, wherein the sleeve exposes a cascade when in the second position;
at least one linear electric motor having a coil system disposed within a base connected directly to an engine structure, a member connected directly to the sleeve, and a magnet system connected to the member and configured to interact with the coil system to linearly move the member relative to the base to cause the sleeve to move between the first position and the second position; and
a load cell, disposed within the base, configured to send load information to a controller, wherein the controller is configured to use the load information to maintain a desired load on the at least one linear electric motor.

12. The thrust reverser system of claim 11 further comprising:
a plurality of linear electric motors having a base connected to an engine structure; and
the member directly connected to the sleeve and configured to move the sleeve between the first position and the second position.

13. The thrust reverser system of claim 11 further comprising:
a sensor system configured to detect a load on the at least one linear electric motor while moving the sleeve and measure a position of the sleeve; and
the controller configured to control operation of the at least one linear electric motor to move the sleeve between the first position and the second position and control a speed at which the at least one linear electric motor moves the sleeve to maintain a load on the at least one linear electric motor below a selected load.

14. The thrust reverser system of claim 11 , wherein the controller is configured to stop the sleeve in at least one of the first position and the second position.

15. The thrust reverser system of claim 11 , wherein the controller is further configured to compensate for a linear electric motor in the at least one linear electric motor not functioning as commanded.

16. A method for operating a thrust reverser system for an aircraft, the method comprising:
moving a sleeve on an engine in the thrust reverser system from a first position to a second position using a linear electric motor directly connected to the sleeve and to a structure of the engine, wherein the moving of the sleeve to a second position exposes a cascade such that exhaust gasses generated by the engine pass through the cascade;
wherein the at least one linear electric motor comprises:
a base;
a coil system associated with the base;
a member connected to the sleeve;
a magnet system associated with the member and configured to interact with the coil system to linearly move the member relative to the base to cause the sleeve to move between the first position and the second position; and

a load cell, disposed within the base, configured to send load information to a controller, wherein the controller is configured to use the load information to maintain a desired load on the at least one linear electric motor.

17. The method of claim 16 further comprising:
moving the sleeve from the first position to the second position using a plurality of linear electric motors.

18. The method of claim 16 further comprising:
determining whether a load on a plurality of linear electric motors is greater than a selected load; and
adjusting a speed of the plurality of linear electric motors to reduce the load on the plurality of linear electric motors when the load is equal to or greater than the selected load.

19. The method of claim 18 , wherein the selected load is one that is greater than a desired load for the plurality of linear electric motors.

20. The method of claim 16 , wherein operation of the linear electric motor is controlled by the controller.

21. The method of claim 17 , wherein moving the sleeve on the engine in the thrust reverser system from the first position to the second position using the plurality of linear electric motors connected to the sleeve comprises:
sending a command to the plurality of linear electric motors to move the sleeve in a direction from the first position towards the second position;
monitoring a position of the sleeve; and
halting operation of the plurality of linear electric motors to halt movement of the sleeve when the second position is reached.

Assignees

• Bol Eric D
• Boeing Co

Inventors

• Bol Eric D

Classifications

• F02K1/72 Primary

  the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow · CPC title

• F05D2250/41

  with one degree of freedom · CPC title

• F01D17/24

  electrical · CPC title

• F05D2270/62

  Electrical actuators · CPC title

• F02K1/763

  with actuating systems or actuating devices; Arrangement of actuators for thrust reversers · CPC title