COUPLING
20170343068 · 2017-11-30
Assignee
Inventors
Cpc classification
F16D2121/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D65/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D2121/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D2121/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D55/226
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D55/228
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16D65/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A coupling comprising a brake plate (70); a first friction pad (64) operable to be selectively biased against the brake plate (70). In a first mode of operation the first friction pad (64) is biased against the brake plate (70) by a first force. In a second mode of operation the first friction pad (64) is biased against the brake plate (70) by a second force. The second force is substantially greater than the first force.
Claims
1. A coupling comprising: a brake plate; and a first friction pad operable to be selectively biased against the brake plate such that in a first mode of operation the first friction pad is biased against the brake plate by a first force, and in a second mode of operation the first friction pad is biased against the brake plate by a second force; the second force being greater than the first force.
2. The coupling as claimed in claim 1 wherein the first friction pad is operable to be selectively biased against the brake plate such that in a third mode of operation the first friction pad is biased against the brake plate by a third force, wherein the third force is greater than the first force but lower than the second force.
3. The coupling as claimed in claim 1 wherein the first friction pad is biased against the brake plate by an actuator.
4. The coupling as claimed in claim 1 wherein there is provided a second friction pad biased into contact with the brake plate.
5. The coupling as claimed in claim 4 wherein the second friction pad is biased against the brake plate by a resilient member.
6. The coupling as claimed in claim 3 further comprising a housing which carries the actuator, the actuator being located in a first cavity provided in the housing.
7. The coupling as claimed in claim 6 wherein the housing carries the resilient member, the resilient member being located in a second cavity provided in the housing.
8. The coupling as claimed in claim 5 wherein the resilient member is biased against the brake plate on the opposite side of the brake plate to the actuator such that the resilient member is operable to bias the second friction pad in an opposite direction to which the actuator is operable to bias the first friction pad.
9. The coupling as claimed in claim 1 wherein the brake plate is fixedly mounted to a rotatable drive shaft which is rotatable about a rotational axis.
10. The coupling as claimed in claim 9 wherein the housing is rotatable about the same rotational axis as the brake plate.
11. A vehicle control system comprising a vehicle control lever coupled to a lever drive via a coupling as claimed in claim 1.
12. The vehicle control system as claimed in claim 10 wherein the first friction pad is biased against the brake plate by an actuator, and wherein the vehicle control lever is coupled to a lever drive via a housing which carries the actuator, the actuator being located in a first cavity provided in the housing.
13. A method of operating a vehicle control system, the system including a lever coupled a lever drive via a brake plate, and a first friction pad operable to be selectively biased against the brake plate, the method comprising: biasing the first friction pad against the brake plate by a first force when the lever drive is in a first mode of operation; and biasing the first friction pad against the brake plate by a second force when the lever drive is in a second mode of operation, the second force being substantially greater than the first force.
14. The method as claimed in claim 13 wherein the method further comprises: selectively biasing the first friction pad against the brake plate by a third force; wherein the third force is greater than the first force but lower than the second force.
15. The method of operating a vehicle control system as claimed in claim 13 wherein the first mode of operation is when the lever drive is non-operational, and the second mode of operation is when the lever drive is operational.
16. (canceled)
17. (canceled)
18. (canceled)
19. The vehicle control system as claimed in claim 10 wherein there is provided a second friction pad biased into contact with the brake plate, the second friction pad being biasable against the brake plate by a resilient member, and wherein the resilient member is biasable against the brake plate on the opposite side of the brake plate to the actuator such that the resilient member is operable to bias the second friction pad in an opposite direction to which the actuator is operable to bias the first friction pad, and wherein the vehicle control lever is coupled to a lever drive via a housing.
20. The vehicle control system as claimed in claim 10 wherein the brake plate is fixedly mounted to a rotatable drive shaft which is rotatable about a rotational axis, and wherein the vehicle control lever is coupled to a lever drive via the housing.
21. The vehicle control system as claimed in claim 20 wherein the housing is rotatable about the same rotational axis as the brake plate wherein the vehicle control lever is coupled to a lever drive via the housing.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0028] Examples of the present disclosure will now be described with reference to the accompanying drawings, in which:
[0029]
[0030]
[0031]
[0032]
[0033]
[0034]
DETAILED DESCRIPTION
[0035] An example of a vehicle control lever actuation system, for example a flight control lever system for an aircraft, comprising a coupling device of the present disclosure is shown in
[0036] A vehicle control lever 50, for example a joystick or inceptor for an aircraft, is selectively linked to a lever drive 56, which may be a motor or gear box, via a coupling according to the present disclosure.
[0037] The coupling comprises a clutch plate 70 (which may also be termed a brake disc or brake plate), a ring shaped housing 52 which surrounds the brake plate 70, and a rotatable drive shaft 54 that extends from the lever drive 56 and is rotatable about a rotational axis 55. The brake plate 70 is located in an annular groove 75 provided in the housing 52. The brake plate 70 is fixedly mounted to the rotatable drive shaft 54 and extends away from the shaft 54 in a radial direction. The housing 52 is rotatable with, and about the same rotational axis 55 as, the brake plate 70.
[0038] A first friction pad 64, or brake pad, is mounted adjacent the brake plate 70.
[0039] The first friction pad 64 is mounted and operable such that it may be selectively biased against the brake plate 70 by a first force, and also biased against the clutch plate by a second force greater than the first force.
[0040] The first friction pad 64 is operable to be selectively biased against the brake plate 70 by an actuator 62, for example a piezo electric actuator. The actuator 62 is located in a first cavity 73 provided in the housing 52, and hence carried by the housing 52.
[0041] A second friction pad 66, or brake pad, is biased into contact with the brake plate 70 by a resilient member 68. The resilient member 68 may be a passive device, for example a spring. The resilient member 68 is located in a second cavity 71 provided in the housing 52, and hence carried by the housing 52.
[0042] The spring 68 provides a passive compression force to press the brake pad 66 against the brake plate 70, to thereby provide a passive frictional force that resists, but does not prevent, rotation of the brake plate 70 relative to the housing 52.
[0043] In the example shown, the outer circumference of the brake plate 70 is located between the pads 64, 66.
[0044] The resilient member 68 is biased against the brake plate 70 on the opposite side of the brake plate 70 to the actuator 62. Hence the resilient member 68 is operable to bias the second friction pad 68 in an opposite direction to which the actuator 62 is operable to bias the first friction pad 64.
[0045] There may also be provided a shaft brake 57 for preventing rotation of the drive shaft 54 in the first mode of operation. The shaft brake 57 is selectively operable to engage or disengage with the shaft 54 as required. The shaft brake 57 may be provided as part of the lever drive unit 56, or external and/or separate to the lever drive unit 56.
[0046] In the first mode of operation the lever drive 56 is non operational and thus either jammed by a malfunction, deliberately switched off or locked by some other means. For example the shaft 54 may be definitively locked in position by the shaft brake 57 in order to ensure the shaft 54 is fixed into a non rotatable state.
[0047] In the first mode of operation the second friction pad 66 is biased into contact with the brake plate 70.
[0048] In the first mode of operation the actuator 62 may not be actively pressing the second pad 64 against the plate 70. However, the cavity 73, actuator 62 and pad 64 may be sized such that even at rest, the friction pad 64 is biased towards, and into contact with, the brake plate 70 by a first force. Hence in the first mode of operation the first friction pad 64 may also be biased against the brake plate 70, and thus resisting its rotation relative to the housing.
[0049] Alternatively, in the first mode of operation, the first friction pad 64 may be spaced apart from, or only lightly touching, the brake plate 70.
[0050] Hence in the first mode of operation, motion of the lever 50 by a user is resisted by virtue of its connection to the non-rotatable shaft 54 of the drive 56 via the housing 52 and brake pads 64, 66 acting on the brake plate 70. However, the lever 50 is operable to move (i.e. slide) relative to the brake plate 70, albeit with frictional resistance.
[0051] In a second mode of operation, as shown in
[0052] Hence in the second mode of operation, slippage between the brake pads 64, 66 and the brake plate 70 is prevented such that there is a coupled link between the control lever 50 and the shaft 54. Hence motion of the shaft 54 by the drive 56 will result in movement of the lever 50 without slippage.
[0053] The coupling is selectively switched between the modes of operation, for example, either by default, as a result of detection of the operational status of the system, or on request by a user.
[0054] When assisted movement and/or control of the control levers is required (i.e. in the second mode of operation), the actuator 62 actively biases the pad 64 into frictional contact with the brake plate 70.
[0055] However, failure of the lever drive 56 or loss of power may result in a “fail safe” mode of operation (i.e. the first mode of operation) wherein the actuator 62 is non operational, and hence not actively biasing the pad 64 into frictional contact with the brake plate 70.
[0056] Alternatively the first mode of operation may be selectively chosen by the user of the vehicle, for example for full authority control of the vehicle, by preference or for training purposes.
[0057] An alternative example of a vehicle control lever actuation system according to the present disclosure is shown in
[0058] The example shown in
[0059] Hence in this example, as in the example of
[0060] As in the example of
[0061] The actuator 62 of the examples shown in
[0062] The device of the present disclosure provides similar functionality to the brake-clutch arrangement of the related art, but is smaller, lighter and requires less electrical power to operate, which is hugely advantageous in aeronautical applications.
[0063] Attention is directed to all papers and documents which are filed concurrently with or previous to this specification in connection with this application and which are open to public inspection with this specification, and the contents of all such papers and documents are incorporated herein by reference.
[0064] All of the features disclosed in this specification (including any accompanying claims, abstract and drawings), and/or all of the steps of any method or process so disclosed, may be combined in any combination, except combinations where at least some of such features and/or steps are mutually exclusive.
[0065] Each feature disclosed in this specification (including any accompanying claims, abstract and drawings) may be replaced by alternative features serving the same, equivalent or similar purpose, unless expressly stated otherwise. Thus, unless expressly stated otherwise, each feature disclosed is one example only of a generic series of equivalent or similar features.
[0066] The invention is not restricted to the details of the foregoing embodiment(s). The invention extends to any novel one, or any novel combination, of the features disclosed in this specification (including any accompanying claims, abstract and drawings), or to any novel one, or any novel combination, of the steps of any method or process so disclosed.