Braking device

Patent metadata

Field	Value
Publication number	US-10900526-B2
Application number	US-201816179094-A
Country	US
Kind code	B2
Filing date	Nov 2, 2018
Priority date	Nov 2, 2017
Publication date	Jan 26, 2021
Grant date	Jan 26, 2021

Abstract

A brake device for braking rotation of an input shaft, comprises a selectively operable trigger brake comprising a preloaded torsion spring rotationally coupled to the input shaft but permitting a limited rotational movement between the trigger brake and the input shaft; and a roller jamming mechanism operable upon the relative rotation between the trigger brake and the input shaft exceeding a predetermined amount to stop rotation of the input shaft upon operation of the trigger brake.

First claim

The invention claimed is:

1. A brake device for braking rotation of an input shaft, comprising:
a selectively operable trigger brake comprising a preloaded torsion spring rotationally coupled to the input shaft but permitting a limited rotational movement between the trigger brake and the input shaft; and
a roller jamming mechanism operable upon the relative rotation between the trigger brake and the input shaft exceeding a predetermined amount to stop rotation of the input shaft upon operation of the trigger brake, wherein the roller jamming mechanism comprises:
a plurality of ramp surfaces provided on the input shaft;
a housing comprising an annular bore;
a plurality of roller elements arranged between the input shaft and the annular bore, the roller elements being received within the annular bore and received between adjacent ramp surfaces; and
an actuator coupled to the trigger brake shaft for moving the roller elements along the ramp surfaces upon relative rotation of the trigger brake shaft and the input shaft thereby forcing the roller elements into wedged contact with the annular bore of the housing.

2. A brake device as claimed in claim 1 , wherein the trigger brake comprises:
at least one static trigger braking element;
at least one rotary trigger braking element mounted to a trigger brake shaft for rotational movement relative to the at least one static braking element, the trigger brake shaft being coupled to the at least one rotary braking element so as to rotate therewith; and
a brake actuator for selectively moving said static and rotary braking elements into engagement with each other;
wherein first and second ends of the torsionally preloaded spring are each coupled to the trigger brake shaft and the input shaft;
wherein the engagement of the static and rotary braking elements overcomes the preload of the torsion spring so as to produce a relative rotation between the brake trigger shaft and the input shaft to operate the roller jamming mechanism.

3. A brake device as claimed in claim 2 , wherein the couplings between the first and second ends of the torsion spring and the trigger brake shaft and the input shaft comprise first and second coupling pins extending through respective apertures in the trigger brake shaft and the input shaft respectively into the torsion spring.

4. A brake device as claimed in claim 3 wherein the openings in the input and trigger brake shafts extend over an circumferential arc (α) greater than the diameter of the coupling pins to permit relative rotational movement of the input and output shafts.

5. A brake device as claimed in claim 2 , wherein the torsion spring is arranged radially outwardly of and around the trigger brake shaft and the input shaft.

6. A brake device for braking rotation of an input shaft, comprising:
a selectively operable trigger brake comprising a preloaded torsion spring rotationally coupled to the input shaft but permitting a limited rotational movement between the trigger brake and the input shaft; and
a roller jamming mechanism operable upon the relative rotation between the trigger brake and the input shaft exceeding a predetermined amount to stop rotation of the input shaft upon operation of the trigger brake, wherein the roller jamming mechanism comprises:
a plurality of ramp surfaces provided on the input shaft;
a static structure of the device;
a plurality of roller elements arranged between the input shaft and the static structure and received between adjacent ramp surfaces; and
an actuator coupled to the trigger brake shaft for moving the roller elements along the ramp surfaces upon relative rotation of the trigger brake shaft and the input shaft.

7. A brake device as claimed in claim 6 , wherein the actuator comprises a plurality of teeth extending between adjacent roller elements, the teeth projecting from one end of the trigger brake shaft.

8. A brake device as claimed in claim 6 , wherein adjacent ramp surfaces are circumferentially symmetrical.

9. A brake device as claimed in claim 1 , wherein the torsion spring comprises means for varying the preload of the spring, wherein optionally at least one end of the torsion spring comprises a series of circumferentially spaced opposed openings for receiving a respective coupling pin therein.

10. A brake device as claimed in claim 1 , wherein the torsion spring is a machined torsion spring or manufactured using Additive Layer Manufacturing techniques.

11. A brake device as claimed in claim 1 , comprising a trigger brake actuator which is, a solenoid actuator.

12. A brake device as claimed in claim 11 , wherein said trigger brake actuator comprises an actuating element which is movable between a non-braking position and a braking position under the force of a biasing spring, the actuating element being held in the non-braking position against the force of the biasing spring when the actuator is energised and released upon de-energisation of the actuator.

13. A drive system comprising a power transmission shaft coupled to or integrally formed with the input shaft of the brake device as claimed in claim 1 .

14. An aircraft actuator system comprising:
the brake device as claimed in claim 1 ; and
a drive system comprising a power transmission shaft coupled to or integrally formed with the input shaft of the brake device;
the power transmission shaft driving a plurality of actuators for deploying or retracting a plurality of slats or flaps in a wing of the aircraft, wherein stopping rotation of the input shaft of the brake device stops rotation of the power transmission shaft and thus stops deployment or retraction of the slats or flaps.

15. An aircraft system as claimed in claim 14 , comprising first and second power transmission shafts for driving respective pluralities of actuators in respective wings of the aircraft, the braking device being provided for each power transmission shaft; wherein, each power transmission shaft is coupled to an asymmetry sensor for sensing asymmetrical operation of the power transmission shafts, and sensing of asymmetrical operation by one or other of the asymmetry sensors causes operation of both braking devices in unison.

Assignees

• Goodrich Actuation Systems Ltd

Inventors

• Davies Stephen

Classifications

• B64D45/00 Primary

  Aircraft indicators or protectors not otherwise provided for · CPC title

• B64C13/24

  Transmitting means · CPC title

• B60T1/062

  acting on transmission parts · CPC title

• F16D47/02

  of which at least one is a coupling · CPC title

• F16D3/72

  with axially-spaced attachments to the coupling parts (F16D3/56 takes precedence) · CPC title