No-back brake creep inhibitor

Patent metadata

Field	Value
Publication number	US-10443696-B1
Application number	US-201615227624-A
Country	US
Kind code	B1
Filing date	Aug 3, 2016
Priority date	Aug 3, 2016
Publication date	Oct 15, 2019
Grant date	Oct 15, 2019

Abstract

A system for inhibiting no-back brake device creep includes a motor, a ballscrew assembly coupled to the motor, a no-back brake device coupled to the ballscrew assembly, and at least one damper coupled to the ballscrew assembly. The damper varies a damping characteristic based on an operational state of the motor.

First claim

What is claimed is:

1. A system for inhibiting no-back brake device creep, comprising:
a motor;
a ballscrew assembly coupled to the motor;
a no-back brake device coupled to the ballscrew assembly; and
at least one damper coupled to the ballscrew assembly, the at least one damper configured to vary a damping characteristic based on an operational state of the motor, wherein the at least one damper comprises a magnetorheological damper; and
a control system coupled to the motor and the at least one damper, wherein the control system controls operation of the motor and the at least one damper such that when the motor is engaged, the at least one damper provides a relatively lower viscous drag to the ballscrew assembly, and when the motor is not engaged, the at least one damper provides a relatively higher viscous drag to the ballscrew assembly.

2. The system of claim 1 , wherein the at least one damper automatically varies the damping characteristic based on the operational state of the motor.

3. The system of claim 1 , wherein the damping characteristic comprises an amount of viscous drag provided by the at least one damper.

4. The system of claim 1 , wherein the at least one damper comprises a rotary damper.

5. The system of claim 1 , wherein the operational state of the motor comprises at least one of an active mode wherein the motor is configured to rotate the ballscrew assembly and an inactive mode.

6. The system of claim 1 , wherein the at least one damper and the motor are coupled to the ballscrew assembly via a gear train assembly.

7. The system of claim 1 , wherein when the motor is not engaged, the no-back brake device is configured to prevent movement of the ballscrew assembly, and the at least one damper is configured to prevent creep-related movement of the ballscrew assembly due to vibrational forces acting upon the ballscrew assembly.

8. A system for inhibiting no-back brake device creep, comprising:
a motor;
a ballscrew assembly coupled to the motor;
a no-back brake device coupled to the ballscrew assembly;
at least one damper coupled to the ballscrew assembly; and
a control module comprising a processor coupled with a non-transitory processor-readable medium storing processor executable code for causing the processor to:
monitor a state of the motor; and
vary a damping characteristic of the at least one damper based on the state of the motor such that when the motor is engaged, the at least one damper provides a relatively lower viscous drag, and when the motor is not engaged, the at least one damper provides a relatively higher viscous drag.

9. The system of claim 8 , wherein the state of the motor comprises at least one of an active mode wherein the motor is configured to rotate the ballscrew assembly and an inactive mode.

10. The system of claim 8 , wherein the at least one damper comprises a magnetorheological damper.

11. The system of claim 10 , wherein the at least one damper comprises a rotary damper.

12. The system of claim 8 , wherein the at least one damper and the motor are coupled to the ballscrew assembly via a gear train assembly.

13. The system of claim 8 , wherein the damping characteristic comprises an amount of viscous drag provided by the at least one damper.

14. A system for inhibiting no-back brake device creep for a no back brake device usable with an actuator to control an aircraft stabilizer, comprising:
a ballscrew assembly configured to be coupled to the aircraft stabilizer;
a motor coupled to the ballscrew assembly such that operation of the motor enables adjustment of a position of the aircraft stabilizer;
a no-back brake device coupled to the ballscrew assembly;
a magnetorheological damper coupled to the ballscrew assembly; and
a control module configured to vary a damping characteristic of the magnetorheological damper based on a state of the motor such that when the motor is engaged, the magnetorheological damper provides a relatively lower viscous drag to the ballscrew assembly, and when the motor is not engaged, the magnetorheological damper provides a relatively higher viscous drag.

Assignees

• Rockwell Collins Inc

Inventors

• Latif Rana Kamran
• Webster Mark A
• Kohuth Kerry R

Classifications

• F16H25/2454 Primary

  Brakes; Rotational locks · CPC title

• F16H25/2204

  with balls · CPC title

• B64C13/28

  mechanical · CPC title

• F16F15/002

  characterised by the control method or circuitry (control of mechanical oscillations per se G05D19/00) · CPC title

• F16F9/535 Primary

  Magnetorheological [MR] fluid dampers (springs comprising magnetorheological [MR] elastomers F16F1/361) · CPC title