Manual brake override
11679862 · 2023-06-20
Assignee
Inventors
Cpc classification
Y02T50/10
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B64C23/072
PERFORMING OPERATIONS; TRANSPORTING
B64C3/56
PERFORMING OPERATIONS; TRANSPORTING
International classification
B64C3/56
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A manual brake override system includes a gear system, an electric motor in operative communication with the input of the gear system, a holding brake in operative communication with the input of the gear system. The holding brake is configured to prevent movement within the gear system when engaged. A manual handwind is provided in operative communication with the input of the gear system and the manual handwind and holding brake are configured such that the input of the gear system can be driven, with the manual handwind, whilst the holding brake is engaged.
Claims
1. A manual brake override system, comprising: a gear system; an electric motor in operative communication with the input of the gear system; a holding brake in operative communication with the input of the gear system, configured to prevent movement within the gear system when engaged; and a manual handwind in operative communication with the input of the gear system; wherein the manual handwind and holding brake are configured such that the input of the gear system can be driven, with the manual handwind, whilst the holding brake is engaged.
2. The manual brake override system of claim 1, wherein the gear system, electric motor, holding brake and manual handwind form part of an actuator.
3. The manual brake override system of claim 2, wherein the actuator is a rotary actuator.
4. The manual brake override system of claim 1, wherein the gear system is a multi-stage gearbox.
5. The manual brake override system of claim 1, wherein the electric motor and the holding brake are connected in series along an axle.
6. The manual brake override system of claim 1, wherein the holding brake is configured such that it is engaged when depowered.
7. The manual brake override system of claim 1, wherein the holding brake is configured to provide a braking torque τ.sub.brake; and wherein the manual handwind is configured such that it can impart a torque, τ.sub.handwind which is greater than τ.sub.brake, in response to a manually applied torque τ.sub.manual applied through the manual drive handwind.
8. An aircraft, comprising: the manual brake override system of claim 1.
9. The aircraft of claim 8, wherein the gear system, electric motor, holding brake and manual handwind form part of a rotary actuator that is used to fold a wing of the aircraft.
10. The manual brake override system of claim 1, wherein the holding brake is configured such that it is engaged when depowered.
11. A manual brake override system, comprising: a gear system; an electric motor in operative communication with the input of the gear system; a holding brake in operative communication with the input of the gear system, configured to prevent movement within the gear system when engaged; and a manual handwind in operative communication with the input of the gear system; wherein the manual handwind and holding brake are configured such that the input of the gear system can be driven, with the manual handwind, whilst the holding brake is engaged; wherein the holding brake is configured to provide a braking torque τ.sub.brake; and wherein the manual handwind is configured such that it can impart a torque, which is greater than, in response to a manually applied torque applied through the manual drive handwind; wherein the ratio of the manually applied torque τ.sub.manual and the imparted torque by the handwind τ.sub.handwind is greater than 5:1.
12. An aircraft, comprising: the manual brake override system of claim 8.
13. The aircraft of claim 12, wherein the gear system, electric motor, holding brake and manual handwind form part of a rotary actuator that is used to fold a wing of the aircraft.
14. The manual brake override system of claim 8, wherein the gear system, electric motor, holding brake and manual handwind form part of an actuator.
15. The manual brake override system of claim 8, wherein the gear system is a multi-stage gearbox.
16. The manual brake override system of claim 8, wherein the electric motor and the holding brake are connected in series along an axle.
17. A method comprising: providing a gear system; providing an electric motor in operative communication with the input of the gear system; providing a holding brake in operative communication with the input of the gear system, configured to prevent movement within the gear system when engaged; providing a manual handwind in operative communication with the input of the gear system; and manually driving the input of the gear system whilst the holding brake is engaged.
18. The method of claim 17, wherein the gear system, electric motor, holding brake and manual handwind form part of an actuator.
19. The method of claim 18, wherein said actuator is a rotary actuator.
20. The method of claim 17, wherein method is used manually fold a wing of an aircraft.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1)
DETAILED DESCRIPTION
(2) Folding wing mechanisms for aircraft typically utilise electrically-powered rotary actuators to fold portions of the wing. Such rotary actuators comprise an electrical motor, which drives a multi-stage gearbox. The output 7 (see
(3) The present invention provides a manual drive gear arrangement for a rotary actuator. In this arrangement, a manual drive handwind 4 is geared and sized to manually overcome the holding brake without the need to release it. As illustrated by
(4) As can be seen by
(5) According to the present invention, the holding brake 3, by virtue of its coupling with the input 5 of the gear system 6 via axle 8, provides a minimum frictional braking torque, τ.sub.brake, required to prevent involuntary movement of the rotary actuator during maintenance procedures throughout the full positional range of the actuator. This means that, when the holding brake 3 is engaged, without any externally applied forces to the rotary actuator, and in some examples to the wing or wing fold mechanism, there can be no movement of the components of the actuator. In known systems, the magnitude of the braking torque, τ.sub.brake, is so high that it cannot be overcome manually via a manual handwind, in order to manually drive the actuator during maintenance procedures. In these scenarios, an additional brake release mechanism is required to reduce or nullify τ.sub.brake. This presents problems such as the additional cost, weight and size of this additional mechanism. The use of such a mechanism also compromises safety, since, when in use, the brake is disengaged, which can lead to involuntary movement and injury to operators. In the present invention, however, the manual handwind 4 is geared such that an operator can apply a torque τ.sub.manual to the manual handwind, which results in a minimum torque, τ.sub.handwind, being applied to the input of the gear system 6. The manual handwind 4 is geared and sized such that τ.sub.handwind>τ.sub.brake. This can also be expressed as a ratio: τ.sub.handwind: τ.sub.brake is greater than 1:1. Similarly, the holding brake 3 is configured to ensure that the frictional braking torque τ.sub.brake is lower than τ.sub.handwind, for even the lower than average strength operators, whilst still being of a great enough magnitude to serve its purpose of preventing involuntary movement of the actuator during maintenance. In general, the holding torque τ.sub.brake of the brake is around 50 Nm and the manual drive handwind 4 is geared and sized such that the required input torque τ.sub.manual to overcome the brake torque and manually operate the rotary actuator is less than 10 Nm. This means that the ratio between the output torque of the handwind τ.sub.handwind the manually applied torque τ.sub.manual is greater than 5:1 since 10 Nm of torque applied to the handwind results in a torque of greater than 50 Nm applied to the input of the gearbox, thereby overcoming the 50 Nm braking torque of the holding brake. Other ratios τ.sub.handwind:τ.sub.manual are also envisaged, such as 2:1, 3:1, 4:1, 6:1, 7:1, 8:1, 9:1 10:1 and greater. In these cases, the braking torque τ.sub.brake is always lower than τ.sub.handwind so that the brake can always be overcome manually. The holding brake 3 can therefore remain fully engaged during the manual maintenance operation, under non-operating conditions. As the brake 3 is permanently engaged, sudden back driving of the panel during maintenance procedures due to, for example, the weight of components, is prevented. This greatly improves the safety of maintenance operations where manual driving is required.
(6) In addition to improving safety and reliability, the present invention requires no additional brake release mechanism, thereby reducing cost and weight. The envelope is also reduced since no additional brake release mechanism is required, which would protrude from the unit housing when in use. The use of a manual brake release mechanism adds complexity to and reduces the reliability of the entire rotary actuator.
(7) Although this disclosure has been described in terms of preferred examples, it should be understood that these examples are illustrative only and that the claims are not limited to those examples. Those skilled in the art will be able to make modifications and alternatives in view of the disclosure which are contemplated as falling within the scope of the appended claims.