Braked wheel equipped with a drive device
The integration of a braking and drive device into an aircraft wheel is achieved through a design that uses a brake disc and caliper for braking and a geared motor and toothed crown gear for rotational drive, addressing space constraints and enabling efficient wheel operation.
Patent Information
- Application Number
- FR2023012754
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2023-11-20
- Publication Date
- 2025-05-23
AI Technical Summary
The integration of a drive device into an aircraft wheel is challenging due to limited space, especially when combined with a brake caliper and its actuator.
A vehicle wheel design that incorporates both a braking device and a drive device, where the braking device includes a brake disc and caliper, and the drive device features a geared motor and toothed crown gear that meshes with the brake disc, allowing for both braking and rotational drive torque.
This design enables efficient braking and rotational movement of the aircraft wheel, with the geared motor's reduction ratio allowing for a parking brake function and reduced wear on the braking system.
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Abstract
Description
Title of the invention: Braked wheel equipped with a drive device
[0001] The present invention relates to the ground movement of a vehicle, and more particularly to a wheel equipped with a braking device and a drive device. The invention also relates to an aircraft landing gear and an aircraft equipped with such a wheel.
[0002] BACKGROUND OF THE INVENTION
[0003] In the field of aviation, it is known to equip aircraft wheels with a brake intended to selectively slow down and stop said aircraft when they are moving on the ground.
[0004] For aircraft of a certain size, such as helicopters, the brake generally comprises a disc which is integral in rotation with the wheel and which is associated with a caliper which straddles the disc. The caliper comprises two jaws each receiving a brake pad, one of the jaws being mounted movably to be able to pinch the disc between the two pads by means of a braking actuator. To minimize the size of the brake, the caliper is placed astride the disc from the inside of the latter.
[0005] It is also known to equip aircraft wheels with a device for driving the wheels in rotation to enable the aircraft to move on the ground without using its powertrains. However, the integration of such a drive device proves very difficult in the presence of the brake caliper and its actuator, the available space being limited.
[0006] SUBJECT OF THE INVENTION
[0007] The invention aims to remedy at least in part the aforementioned drawback. Summary of the invention
[0008] For this purpose, a vehicle wheel is provided, rotatably mounted on an axle, comprising a braking device and a wheel drive device. The braking device comprises a brake disc rotatably secured to the wheel and a brake caliper overlapping the disc to exert friction forces on the disc by means of a braking actuator mounted on the caliper. The drive device comprises a geared motor rotating a pinion which is arranged to mesh with a toothed crown rotatably secured to the disc.
[0009] Thus, the disc allows both braking torque and rotational drive torque to be exerted on the wheel.
[0010] Furthermore, the geared motor can be sized so as to have a sufficient reduction ratio so that, when the geared motor is not powered electrically The pinion exerts sufficient force on the crown gear to lock the disc and therefore the rotating wheel, thus performing the parking brake function. The geared motor can also be sized so that it can be used as a low-speed brake and thus limit wear on the braking device.
[0011] In particular, the caliper internally overlaps the disc.
[0012] In particular, the caliper is mounted on the axle.
[0013] In particular, the geared motor is mounted on the bracket.
[0014] In particular, the toothed crown is attached to the disc.
[0015] In particular, the disc has an external periphery which comprises radial peripheral notches defining tenons received in axial peripheral notches of the wheel.
[0016] In particular, the disc is mounted floating on the wheel.
[0017] In particular, the geared motor and the actuator extend coaxially to the axis (X) of rotation of the wheel.
[0018] The invention also relates to an aircraft landing gear comprising at least one such wheel.
[0019] The invention also relates to an aircraft comprising at least one such landing gear. Brief description of the drawings
[0020] The invention will be better understood in light of the following description, which is purely illustrative and non-limiting, and must be read in conjunction with the appended figures, among which:
[0021] [Fig-1] [Fig.l] is a schematic view of a helicopter comprising wheels equipped with a braking and rotation drive device according to a particular embodiment of the invention;
[0022] [Fig.2] [Fig.2] is a perspective view of one of the braked / powered wheels of the aircraft illustrated in [Fig.l];
[0023] [Fig.3] [Fig.3] is an exploded view, from a first viewing angle, of the braked / motorized wheel illustrated in [Fig.2];
[0024] [Fig.4] [Fig.4] is an exploded view, from a second viewing angle, of the braked / motorized wheel illustrated in [Fig.2];
[0025] [Fig.5] [Fig.5] is a perspective view of the braking and rotational drive device of the wheel illustrated in [Fig.2];
[0026] [Fig.6] [Fig.6] is an exploded view of the brake disc of the braking and rotational drive device illustrated in [Fig.5]. DETAILED DESCRIPTION OF THE INVENTION
[0027] With reference to [Fig.l], the invention is described in application to a helicopter H but is applicable to other types of aircraft or vehicles such as vehicles terrestrial. The helicopter H comprises two main landing gears, each comprising a leg having an upper end fixed to a structure of the helicopter H and, opposite, a lower end carrying a wheel 1 rotating around an axis X on a shaft or axle E. The following description relates to one of the wheels 1 of the helicopter H, the wheels 1 being identical here but may also be different.
[0028] The wheel 1 comprises, as illustrated in Figures 2 to 4, an annular rim 2 connected by a web 3 to a hub 4 which is pivotally received on the axle E by means of bearings (not shown). The rim 2 comprises two annular edges or beads 2.1, 2.2 between which a tire (not shown) is mounted. The bead 2.1 comprises a collar extending axially and comprising axial peripheral notches 2.3 which open onto a free edge of the collar and are equally distributed around the axis X. These notches 2.3 define, as will be seen later, mortises.
[0029] The wheel 1 is said to be “braked”, that is to say equipped with a braking device 10 intended to ensure the immobilization of the helicopter H when it is on the ground, in particular when parked.
[0030] With reference to Figures 2 to 6, the braking device 10 comprises a brake disc 11 having a central axis coaxial with the axis X of rotation of the wheel 1. The disc 11, here made of carbon, is annular in shape and has an external periphery which comprises radial peripheral notches defining tenons 11.1 (here seven in number) equally distributed around the axis X. The tenons 11.1 are protected by riders 12 fixed to said tenons 11.1 each by two rivets 13 extending parallel to the axis X. The tenons 11.1 are received in the notches 2.3 of the rim bead 2.1 to ensure rotational coupling of the brake disc 11 with the wheel 1 while allowing said disc 11 to move axially with respect to said wheel 1. The disc 11 is thus mounted “floating” and the riders 12 define an interface between the tenons 11.1 of the disc 11 and the notches 2.3 of the rim 2.
[0031] The braking device 10 also comprises a caliper 14 comprising a body 14.1 fixedly mounted on the axle E by means of a protrusion Ei extending in radial projection from the axle E ([Fig. 3]). The protrusion Ei is received in a receptacle 14.2, of a shape complementary to that of the protrusion EB of the body 14.1 to ensure both positioning of the caliper 14 on the axle E and the transmission of braking forces.
[0032] The body 14.1 overlaps an inner periphery of the disc 11 and comprises a first fixed jaw 14.3 which extends axially opposite the disc 3 of the wheel 1 and which carries a first brake pad 15.1 extending parallel opposite a first friction face of the disc 11. The caliper 14 also comprises a second jaw which is mounted axially movable in a first bore of the body 14.1 and which carries a second brake pad 15.2 extending parallel opposite a second friction face of the disc 11, opposite the first friction face. The first pad 15.1 and the second pad 15.2, here made of carbon, are arranged to ensure axial pinching of the disc 11 under the action of a braking actuator 16 attached to the caliper body 14.1, and thus exert friction forces on the disc 11 tending to slow down and / or block the wheel 1 by means of the tenons 11.1 of the disc 11 engaged in the notches 2.3 of the rim 2.
[0033] The braking actuator 16 is here an electromechanical actuator which comprises an electric motor 16.1 connected to a ball screw 16.3 via a reducer 16.2 to ensure a movement of the second jaw in a direction parallel to the axis X. The ball screw 16.3 is mounted on the caliper body 14.1 and extends, along an axis Xi63 parallel to the axis X, projecting from a front surface 14.4 of said body 14.1 which is turned towards the outside of the wheel 1. The reducer 16.2 extends generally in a plane perpendicular to the axis X and comprises a first end connected to the ball screw 16.3 and, opposite, a second end connected to the electric motor 16.1 which extends along an axis Xi6.i parallel to the axis X in the direction of the wheel 1.
[0034] In order to limit the overall volume of the braking actuator 16, it will be noted that the motor 16.1 and the ball screw 16.3 do not extend on either side of the reducer 16.2, but on one and the same side of said reducer 16.2.
[0035] The wheel is also said to be “motorized”, that is to say equipped with a device 20 for driving the wheel 1 in rotation, intended to ensure movement of the helicopter H without using its powertrains when it is on the ground.
[0036] The drive device 20 comprises a toothed crown 21 mounted coaxially to fit inside the brake disc 11. The crown 21 comprises an inner periphery provided with a row of teeth 21.1, and an outer periphery cooperating with an inner surface 11.2 of the inner periphery of the brake disc 11, the outer periphery of the crown 21 having a diameter slightly smaller than that of the inner surface of the brake disc 11. The toothing of the crown (formed by the teeth 21.1) is here straight.
[0037] The crown 21 is held in position inside the disc 11 by means of keys 22 (here seven in number) extending in radial projection from the inner surface 11.2 of the disc 11 to fit into notches 21.2, of complementary shape, formed on the external periphery of the crown 21.
[0038] Each of the keys 22 is received in a conforming recess 11.3 of the disc 11, the recess 11.3 extending radially to open on one side onto an upper surface of one of the tenons 11.1 and on the other side onto the inner surface 11.2 of the disc 11. The keys 22 are here identical and comprise a flat element comprising: • a first end which extends slightly back from the su- upper part of the tenons 11.1 and which comprises two transverse holes 22.1 crossed by the rivets 13 of the corresponding tenon, so that the key 22 is fixed with respect to the disc 11; and • a second end, opposite the first end, which comprises teeth 22.2 (here four in number) received in the conforming notches 21.2 of the crown 21.
[0039] It is understood that the keys 22 form means for coupling in rotation the toothed crown 21 with the brake disc 11, but also means for coupling in translation along the axis X of said toothed crown 21 with said brake disc 11: the crown 21 is therefore integral with the disc 11.
[0040] The drive device also comprises a geared motor 23 which is attached to the body 14.1 and which extends along an axis X23 parallel to the axis X, projecting from the front surface 14.4 of the caliper body 14.1. The geared motor 23 comprises an output shaft which extends through a second bore of the body 14.1 and which comprises a free end provided with a pinion 24 meshing with the toothed crown 21 to rotate the disc 11 and thus exert on the brake disc 11 a driving torque tending to rotate the wheel 1 by means of the tenons 11 of the disc 11 engaged in the notches 2.3 of the rim 2.
[0041] Preferably, the motor - reducer 23 has a reduction ratio greater than a predetermined ratio so that, when the motor - reducer 23 is not electrically powered, the pinion 24 exerts sufficient forces on the toothed crown 21 to block the rotation of the wheel 1. The drive device can then be used as a parking brake.
[0042] The motor - reducer 23 can also be sized so as to be able to be used as a low - speed brake and thus limit the wear of the brake disc 11 and the brake pads 16.1, 16.2 and therefore increase their service life.
[0043] Of course, the invention is not limited to the described embodiment but encompasses any variant falling within the scope of the invention as defined by the claims.
[0044] Although the disc 11 is here mounted floating, it can also be fixed.
[0045] The caliper 14 can straddle the outside of the brake disc 11.
[0046] Although the brake disc 11 is here rotationally fixed at the rim, it can also be fixed at the disc 3 or the hub 4.
[0047] Although the stirrup 14 is here made of carbon, it can be made of any suitable material, for example steel.
[0048] Although the first and second plates 16.1, 16.2 are here made of carbon, they can be made of any suitable material.
[0049] Although the toothed crown 21 is here attached to the center of the disc 11, said crown 21 and said disc 11 may be in one piece and form a single piece. The teeth 21.1 of the crown 21 are for example directly machined in the brake disc 11.
[0050] Although the braking device 10 here comprises only a single disc 11, it can comprise a plurality of discs 11.
[0051] Although the braking actuator 16 is electric here, it can be of another nature: hydraulic, pneumatic, etc.
[0052] The positioning of the caliper 14 on the axle E and the transmission of the braking forces can be achieved otherwise than with the protrusion Ei of the axle E received in the conforming receptacle 14.2 of the caliper body 14.1, for example using one or more pins.
[0053] The pinion 24 of the drive device may be a roller pinion, for example a roller pinion produced by the company Nexen®.
[0054] The straight teeth of the pinion 24 may have a curved profile in order to be able to manage small movements and small deformations of the disc / crown assembly 11, 21. The output shaft of the geared motor 23, at the end of which the pinion 24 is fixed, may also be mounted on a spherical bearing.
[0055] If the application requires it, a clutch system (for example, a friction clutch) can be incorporated into the gearmotor 23.
Claims
Claims
1. Vehicle wheel (1), rotatably mounted on an axle (E), comprising a braking device and a wheel drive device, the braking device comprising a brake disc (11) integral in rotation with the wheel and a brake caliper (14) overlapping the disc to exert friction forces on the disc by means of a braking actuator mounted on the caliper, and the drive device comprising a geared motor (23) rotating a pinion which is arranged to mesh with a toothed crown (21) integral in rotation with the disc.
2. A vehicle wheel (1) according to claim 1, wherein the caliper (14) internally overlaps the disc (11).
3. Vehicle wheel (1) according to any one of the preceding claims, wherein the caliper (14) is mounted on the axle (E).
4. Vehicle wheel (1) according to any one of the preceding claims, in which the geared motor (23) is mounted on the caliper (14).
5. Vehicle wheel (1) according to any one of the preceding claims, in which the toothed crown (21) is attached to the disc (11).
6. Vehicle wheel (1), any one of the preceding claims, wherein the disc (11) has an outer periphery which comprises radial peripheral notches defining studs (11.1) received in axial peripheral notches (2.3) of the wheel (1).
7. A vehicle wheel (1), any one of the preceding claims, wherein the disc (11) is mounted floating on the wheel (1).
8. Vehicle wheel (1), any one of the preceding claims, wherein the geared motor and the actuator (16) extend coaxially to the axis (X) of rotation of the wheel.
9. Aircraft landing gear comprising at least one wheel (1) according to any one of the preceding claims.
10. Aircraft comprising at least one landing gear according to claim 9.
Citation Information
Patent Citations
Powered aircraft flight control system
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Braking system for an aircraft landing gear with calliper with several areas for clamping the brake disc
EP3581822A1
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FR1214909A
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US20180252279A1