• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates to an aircraft wheel having a hub (52) for rotatably mounting the wheel on an undercarriage axle about an axis of rotation, a rim (55) with end stubs for receiving a tire, the rim being secured to the hub by a web (56). The hub is adapted to removably receive a bearing housing (60) having two bearings (53,54) mounted in O between a bushing (61) to be threaded onto the axle with an outer wall shaped to receive the rings. internal bearings, the sleeve having one end (63) abutting and another end shaped to receive a precharge nut (67), and a sleeve (62) extending around the sleeve and having an inner wall having two shoulders for axially arresting the outer races of the bearings, the sleeve having an outer wall shaped to be fitably slid into a bore of the hub, with one end (68) abutting and another end shaped to receive a lock nut ( 70).
    公开号:FR3055379A1
    申请号:FR1657907
    申请日:2016-08-24
    公开日:2018-03-02
    发明作者:Sylvain JABER；Vincent BELLENGER；Nicolas MORETTI；Gilles ELUARD
    申请人:Safran Landing Systems SAS；
    IPC主号:
    专利说明:

    (57) The invention relates to an aircraft wheel comprising a hub (52) for rotatably mounting the wheel on a landing axle around an axis of rotation, a rim (55) with heels of end for receiving a tire, the rim being secured to the hub by a web (56). The hub is adapted to removably receive a bearing housing (60) comprising two bearings (53,54) mounted in O between a sleeve (61) intended to be threaded on the axle with an external wall shaped to receive the rings internal bearings, the sleeve having one end (63) shaped as a stop and another end shaped to receive a preload nut (67), and a sleeve (62) extending around the sleeve and having an internal wall having two shoulders for axially stopping the outer rings of the bearings, the sleeve having an outer wall shaped to be slidably adjusted in a bore of the hub, with one end (68) shaped as a stop and another end shaped to receive a stop nut ( 70).

    The invention relates to an aircraft wheel with a separable bearing housing.
    BACKGROUND OF THE INVENTION Aircraft wheels are known comprising a hub which receives bearings for the rotational mounting of the wheel on a landing axle, and a rim with end beads for receiving a tire, the rim being secured to the hub by a veil. The wheel may consist of two half-wheels joined together by bolts at the level of the web or, on the contrary, be a single piece, one of the beads being then provided removable for mounting the tire.
    These wheels are retained on the axle by means of an end nut whose tightening ensures the preload of the bearings mounted in O. It is advisable to replace each of the wheels regularly due to the progressive wear of the tire, typically all the two hundred flights. The maintenance team puts the undercarriage under a jackpot, removes the axle nut and removes the wheel to replace it with a wheel fitted with a new or retreaded tire. The disassembled wheel goes to a maintenance workshop where it is disassembled to remove the worn tire for replacement. This disassembly is an opportunity to inspect the bearings, to grease them, or possibly to replace them if they have reached their prescribed service life.
    Recently, so-called long-lasting tires have appeared, allowing a much greater number of flights between two tires to install the bearings, which according to such maintenance as wheel changes. From question of inspection the programs of current, must be operated at a frequency faster than the change of such tires.
    OBJECT OF THE INVENTION
    The invention aims to propose an aircraft wheel facilitating the inspection, maintenance or change of its bearings.
    SUMMARY OF THE INVENTION
    With a view to achieving this goal, an aircraft wheel is proposed comprising a hub for rotational mounting of the wheel on a landing axle around an axis of rotation, a rim with end beads for receive a tire, the rim being secured to the hub by a web, in which, according to the invention, the hub is adapted to removably receive a bearing housing comprising:
    - Two bearings with tapered seat each with an inner ring and an outer ring, mounted in O between:
    - A sleeve intended to be threaded on the axle with an external wall shaped to receive the inner rings of the bearings, the sleeve having one end shaped as a stop and another end shaped to receive a preload nut;
    - A sleeve extending around the sleeve and having an internal wall having two shoulders for axially stopping the outer rings of the bearings, external wall shaped to be adjusted in a bore of the hub shaped as a stop and shaped to receive the sleeve having a slide to with another one a nut end stop end.
    Such a wheel can be mounted like a conventional wheel on the axle, the axle nut then serving to stop the bushing of the bearing housing axially on the axle. During a maintenance operation, the wheel is removed from the axle by unscrewing the axle nut and the housing is separated from the rest of the wheel by unscrewing the stop nut for replacement by another housing with bearings inspected and greased, the operation can be done directly at the foot of the aircraft. The wheel is then reassembled on the aircraft, and the disassembled case is taken for inspection and lubrication of the bearings.
    Thanks to the wheel of the invention, it is therefore possible to dissociate the frequency of inspection and maintenance of the bearings, and the frequency of replacement of the tire.
    What is more, the presence of a sleeve guided by the wheel bearings allows all kinds of elements to be coupled to it, such as the blades of a fan or the target of a rotation sensor, such as an effect tachometer lobby.
    In addition, the presence of the sleeve and the sleeve makes it possible to easily motorize the wheel, by adapting to the housing a motor whose stator is integral with the sleeve, and the rotor integral with the sleeve.
    According to a particular embodiment, the motor does not have bearings between the rotor and the stator, the two elements being guided in rotation by the bearings of the housing.
    BRIEF DESCRIPTION OF THE DRAWINGS
    The invention will be better understood in the light of the following description of particular embodiments of the invention, with reference to the figures of the appended drawings in which:
    - Figure 1 is a sectional perspective view of an aircraft wheel known per se, mounted on a landing gear axle;
    - Figure 2 is a sectional perspective view of an aircraft wheel according to a particular embodiment of the invention;
    - Figure 3 is an enlarged view of the bearing housing fitted to the wheel of Figure 2;
    - Figures 4 to 6 are views similar to those of Figure 2 of alternative embodiments in which the bearing housing is motorized.
    DETAILED DESCRIPTION OF THE INVENTION A conventional aircraft wheel 1 as illustrated in FIG. 1 comprises a hub 2 which here receives the outer rings of tapered roller bearings 3,4. The hub 2 is connected to a rim 5 by means of an openwork veil 6. The rim 5 has beads 7 which hold the sidewalls of a tire (not shown), one of the beads being removable for receiving the tire. The inner rings of the bearings 3,4 are received on an axle protector 8 in the form of a bushing, one end of which is shaped as a stop to come to bear on a shoulder 101 of an axle 100 of the undercarriage on which the protector axle 8 is threaded. An axle nut 102 screwed onto the end of the axle 100 comes to preload the bearings 3,4 and axially stop the wheel on the axle which then turns along the axis of rotation defined by the axle and the bearings. When replacing the wheel, simply unscrew the axle nut 102, remove the wheel assembly to replace it with a wheel with a new or retreaded tire, and with the bearings inspected and greased.
    According to the invention, a wheel with a separable hub is proposed such as the wheel 51 illustrated in FIG. 2. Such a wheel always includes a rim 55 provided with heels 57 and connected by a web 56 to a hub 52. However, the hub does not directly accept bearings with a tapered seat 53,54. According to the invention, the hub 52 is attached to a bearing housing 60 illustrated in more detail in FIG. 3 which includes a bushing 61 which is threaded onto the axle 100, and a sleeve 62 on the external face of which the hub 52 is reported. The bearings 53, 54 extend between the sleeve 61 which receives the inner rings of the bearings, and the sleeve 62 which receives the outer rings of the bearings.
    For this purpose, the sleeve 62 has ends shaped into housings with shoulders forming stops to receive the outer rings of the bearings 53,54. The sleeve 61 for its part has an end 63 shaped so as to project from either side of a tubular part 64 with a thin core. The part of the end 63 projecting towards the bearings forms a stop for the latter, while the part of the end 63 projecting towards the axle 100 has grooves 65 to cooperate with homologous grooves of the axle 100 for ensuring a rotation stop of the sleeve 61 on the axle 100. The other end 66 of the sleeve 61 is threaded to receive a preload nut 67 for preloading the bearings.
    The outer wall of the sleeve 62 is received with adjustment in the bore of the hub 52, one end 68 of the sleeve 62 forms an external step to constitute an axial stop of the sleeve 62, and the other end 69 is threaded to receive a nut d stop 70, visible in FIG. 2.
    During a bearing inspection operation when the tire carried by the wheel can still last for several flights, it is enough to dismantle the wheel, remove the bearing housing to replace it with a housing whose bearings have been inspected and greased, then reassemble the wheel. The operation can be easily done at the foot of the aircraft, the removal of the wheel housing requiring only the unscrewing of the stop nut 70.
    Thus, the wheel of the invention is brought back to the workshop only for changing the tire, the inspection, maintenance and replacement cycle of the bearings being decorrelated from that of the tire.
    The presence of a housing allows easy motorization of the wheel. Indeed, as illustrated in FIGS. 4 to 6, it suffices to secure the stator of an engine to the socket 61 and its rotor to the sleeve 62 to rotate the sleeve relative to the socket, and thus drive the wheel in rotation. It is of course appropriate to provide means for securing in rotation (not shown here) between the hub and the sleeve (of the spline or pin type for example).
    As illustrated in FIG. 4, a motor 80 is constituted on the one hand by an extension 81 of the sleeve 61 which extends to receive a winding 82 and form a stator 83 of the motor, and on the other hand by an extension 84 the sleeve 62 which extends opposite the stator to carry permanent magnets 85 and form a rotor 86 of the motor. It will be noted that there is no bearing between the stator and the rotor of the motor, the guiding in rotation being ensured by the bearings of the bearing housing 60. It will also be noted that the stator is shaped to allow a tightening key to pass axle nut 102.
    According to a variant illustrated in FIG. 5, the rotor 86 is no longer directly integral with the sleeve, but is mounted for rotation on the stator 83 by means of bearings 87. The rotor 86 is selectively coupled in rotation to the sleeve by means a dog clutch 88 carried by a disc 89 forming an extension of the sleeve 62.
    According to a variant illustrated in FIG. 6, the rotor 83 is now connected to the disc 89 by means of pins 90 (only one is visible here) calibrated to yield when the transmission torque between the disc 89 and the rotor 83 exceeds a predetermined threshold .
    In all of these motorized variants, the bearing housing 60 can always be easily detached from the rest of the wheel by unscrewing the stop nut 70.
    According to a particular aspect of the invention, it will further be noted that the bearing housing 60 is here shaped to allow mounting, instead of a wheel of the invention, of a conventional wheel according to the prior art, like that of FIG. 1, on the same axle without any modification or adaptation of the axle. This allows the replacement of a wheel according to the invention with a conventional wheel in case of service need. In this regard, it will be noted that the bearings of the bearing housing 60 are identical and are placed in the same position as that of the conventional wheel, so that they bear identically on the axle while transmitting the same forces. We can then simply choose a suitable axle nut or insert a spacer between the nut and the bearing of the conventional wheel, to compensate for the thickness of the bushing stop, which is no longer present in a conventional wheel.
    The invention is not limited to what has just been described, but on the contrary covers any variant coming within the scope defined by the claims.
    In particular, although it has been indicated that the sleeve was grooved for its rotation stop on the axle, this arrangement is optional, and is really only necessary if the sleeve is equipped with a motor, the stator of which must be stopped in rotation.
    Although there have been shown here bearing housings fitted with motors, with extensions of the sleeve or of the sleeve forming the stator, the rotor, or the coupling disc to a rotor, these elements may have come in one piece with the sleeve or the sleeve, or even simply attached to them.
    These boxes can also be fitted with other components than motors, such as a fan for cooling the brake discs through the web of the wheel, or a speed sensor of the wheel.
    权利要求:
    Claims (7)
    [1" id="c-fr-0001]
    1. Aircraft wheel comprising a hub (52) for rotatably mounting the wheel on a undercarriage axle about an axis of rotation, a rim (55) with end beads for receiving a tire, the rim being secured to the hub by a web (56), characterized in that the hub is adapted to removably receive a bearing housing (60) comprising:
    - Two bearings (53,54) with conical bearing, each with an internal ring and an external ring, mounted at O between:
    - A sleeve (61) intended to be threaded on the axle with an external wall shaped to receive the inner rings of the bearings, the sleeve having one end (63) shaped as a stop and another end shaped to receive a preload nut ( 67);
    - A sleeve (62) extending around the sleeve and having an inner wall having two shoulders for axially stopping the outer rings of the bearings, the sleeve having an outer wall shaped to be slidably adjusted in a bore of the hub, with a end (68) shaped as a stop and another end shaped to receive a stop nut (70).
    [2" id="c-fr-0002]
    2. Aircraft wheel according to claim 1, in which the socket comprises (65) able to cooperate with axles.
    anti-rotation means homologous means of
    [3" id="c-fr-0003]
    3. Aircraft wheel according to claim 2, in which the anti-rotation means are grooves (65) carried by the end of the sleeve shaped as a stop for the bearings.
    ίο
    [4" id="c-fr-0004]
    4. Wheel according to claim 1, wherein the bearing housing is equipped with a motor (80) for rotating the sleeve relative to the sleeve.
    [5" id="c-fr-0005]
    5. Wheel according to claim 4, wherein the motor comprises a stator (83) integral with the sleeve (61), and a rotor (86) integral with the sleeve (62), the rotor and the stator being guided in rotation by the wheel bearings (53,54) without any bearing being arranged between the stator and the rotor.
    [6" id="c-fr-0006]
    6. Wheel according to claim 4, wherein the motor comprises a stator (83) integral with the sleeve (61) and a rotor (86) mounted rotating on the stator by means of bearings (87), the rotor being secured in rotation to a disc (89) secured to the sleeve (62) by a fastening member (88; 90), such as a dog clutch (88) or pins (90) dimensioned to rupture when a torque transmitted between the disc and the rotor exceeds a predetermined threshold.
    [7" id="c-fr-0007]
    7. Assembly comprising a undercarriage comprising at least one axle (100) provided with an axle nut (102), and a choice of wheels mountable on the axle of which:
    - A wheel (1), the hub directly receives bearings for its rotational mounting on the axle 100, so that the bearings are threaded on the axle while being stopped axially and preloaded by the axle nut;
    - a wheel according to one of the preceding claims, the bearing housing of which is threaded on the axle while being stopped axially by the axle nut;
    the two wheels having the same bearings, arranged identically.
    1/3
    类似技术:
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    FR3103019A1|2021-05-14|Roller gear element
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    FR2718850A1|1995-10-20|Tachometer for aircraft landing gear
    FR3012997A1|2015-05-15|ROLLING TRAIN WITH AXIAL ROTOR RETENTION MEMBER ON STATOR
    同族专利:
    公开号 | 公开日
    EP3287652B1|2019-06-12|
    CN107776876A|2018-03-09|
    EP3287652A1|2018-02-28|
    FR3055379B1|2018-08-10|
    CN107776876B|2021-03-12|
    US20180057151A1|2018-03-01|
    US10829208B2|2020-11-10|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
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    FR1155836A|1955-08-18|1958-05-08|Dunlop Rubber Co|Wheel|
    EP0687826A1|1994-06-14|1995-12-20|SKF Industrial Trading & Development Co, B.V.|Bearing assembly for avehicle hub, and also hub assembly|
    EP2394912A1|2010-06-10|2011-12-14|Messier-Bugatti-Dowty|Autonomous displacement means for aircraft|
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    US8528856B2|2010-10-29|2013-09-10|Honeywell International, Inc.|Compact electric taxi assembly for installation on an aircraft|
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    DE202015103560U1|2015-06-22|2015-07-23|Ford Global Technologies, Llc|Wheel module for a driven axle of a motor vehicle|CN109291784A|2018-10-31|2019-02-01|武汉理工大学|Hub motor and electric car|
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    法律状态:
    2017-08-22| PLFP| Fee payment|Year of fee payment: 2 |
    2018-03-02| PLSC| Publication of the preliminary search report|Effective date: 20180302 |
    2018-08-27| PLFP| Fee payment|Year of fee payment: 3 |
    2020-05-08| ST| Notification of lapse|Effective date: 20200406 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1657907|2016-08-24|
    FR1657907A|FR3055379B1|2016-08-24|2016-08-24|AIRCRAFT WHEEL WITH SEPARABLE BEARING HOUSING|FR1657907A| FR3055379B1|2016-08-24|2016-08-24|AIRCRAFT WHEEL WITH SEPARABLE BEARING HOUSING|
    EP17182205.9A| EP3287652B1|2016-08-24|2017-07-19|Aircraft wheel with a separable bearing box|
    CN201710611766.7A| CN107776876B|2016-08-24|2017-07-25|Aircraft wheel equipped with separable bearing housing|
    US15/685,019| US10829208B2|2016-08-24|2017-08-24|Aircraft wheel with a separable bearing box|
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