Braking assembly

• US 20030051950A1
• Filed: 09/11/2002
• Published: 03/20/2003
• Est. Priority Date: 09/15/2001
• Status: Abandoned Application

• Current Assignee: Goodrich Actuation Systems Limited (Goodrich Ltd.)
• Original Assignee: Goodrich Actuation Systems Limited (Goodrich Ltd.)
• Inventors: Harvey, John Herbert
• Application Number:
  US10/241,563
• Publication Number:
  US 20030051950A1
• Time in Patent Office: Days
• US Class Current: 188/134
• CPC Class Codes: F16D 59/02 spring-loaded and adapted to be released by mechanical, fluid, or electromagnetic means

Abstract

A no-back braking assembly for a rotary actuator includes a rotatable input shaft, a rotatable output shaft, wherein said output shaft is co-axial with said input shaft, and a braking arrangement operably coupled with said output shaft. The braking arrangement comprises first and second braking members and biasing means, and a torque transfer device mounted between said shafts for transferring torque applied to said input shaft to said output shaft. The first and second braking members are relatively moveable between a first position in which they are in mutual engagement and in which rotation of said output shaft is braked, and a second position in which they are mutually spaced and in which said output shaft is capable of relatively free rotation, the biasing arrangement being arranged to urge the braking members into their first position. The torque transfer means is arranged to overcome said biasing arrangement, whereby to urge said first and second braking members into their second position upon application of torque above a predetermined threshold to said input shaft, and to cause rotation of said output shaft.

Claims

1. A no-back braking assembly for a rotary actuator, the braking assembly comprising:

a rotatable input shaft;

a rotatable output shaft, said output shaft being co-axial with said input shaft;

a braking arrangement operably coupled with said output shaft, said braking arrangement comprising first and second braking members and a biasing arrangement; and

a torque transfer device mounted between said shafts for transferring torque applied to said input shaft to said output shaft,

wherein said first and second braking members are relatively moveable between a first position in which they are in mutual engagement and in which rotation of said output shaft is braked, and a second position in which they are mutually spaced and in which said output shaft is capable of relatively free rotation, the biasing arrangement being arranged to urge the braking members into their first position,

and wherein said torque transfer device is arranged to overcome said biasing arrangement, whereby to urge said first and second braking members into their second position upon application of torque above a predetermined threshold to said input shaft, and to cause rotation of said output shaft.

2. A no-back braking assembly according to claim 1, wherein the output shaft (14) forms a drive input to a screw-type actuator.

3. A no-back braking assembly according to claim 1, wherein the output shaft forms a drive input to a rotary gearbox actuator.

4. A no-back braking assembly according to claim 2, wherein the braking assembly includes the actuator.

5. A no-back braking assembly according to claim 4, whereby the actuator is arranged to drive a flight control surface of an aircraft.

6. A no-back braking assembly according to claim 1, wherein said biasing arrangement comprises a resiliently deformable member.

7. A no-back braking assembly according to claim 6, wherein said biasing member is a disc spring or a coil spring.

8. A no-back braking assembly according to claim 1, wherein said braking members are relatively moveable between their first and second positions in a direction substantially parallel to the rotational axis of said input and output shafts.

9. A no-back braking assembly according to claim 1, wherein said first braking member is fixedly secured to a first housing portion, said relative movement between said first and second positions being entirely due to movement of said second braking member.

10. A no-back braking assembly according to claim 1, wherein said second braking member is carried by said output shaft, the engagement between the output shaft and the braking member being such that relative rotation between the second braking member and the output shaft is prevented.

11. A no-back braking assembly according to claim 1, wherein said torque transfer device comprises a ball/ramp mechanism.

12. A no-back braking assembly according to claim 11, wherein said ball ramp mechanism comprises a channel formed by a recess in an end of the input shaft and an aligned corresponding recess in the second braking member, a ball being retained within the channel.

13. A no-back braking assembly according to claim 12, wherein a plurality of such channels and balls are provided.

14. An actuator for driving a flight control surface of an aircraft including a no-back braking assembly having a rotatable input shaft, and a rotatable output shaft which is coaxial with said input shaft, a brake arrangement coupled with said output shaft and having first and second braking members and a biasing arrangement, and a torque transfer device mounted between said input and output shafts for transferring torque applied to said input shaft to said output shaft, wherein said first and second braking members are relatively movable between a first position in which they are in mutual engagement and in which rotation of said output shaft is braked, and a second position in which they are mutually spaced and in which said output shaft is capable of relatively free rotation, whereby the biasing arrangement is arranged to urge the braking members into their first position, and wherein said torque transfer device is arranged to urge said first and second braking members into their second position, overcoming the force due to said biasing arrangement, when torque above a predetermined threshold is applied to said input shaft, thereby causing rotation of said output shaft.