• 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 a disk brake for an aircraft wheel, comprising friction disks (20, 30), including rotor disks and stator disks, a structure comprising a torsion tube (11) on which the disks are threaded, a rear plate (12) at one end of the tube, and a support (13) of brake actuators (14,15) at another end of the tube, the actuators being selectively activatable to apply a press force on the disks. According to the invention, the discs are separated into two groups, of which a first group (20) which is usable alone for taxing braking, and a second group (30) which is usable, alone or in conjunction with the first group, for takeoff / landing braking.
    公开号:FR3021378A1
    申请号:FR1454575
    申请日:2014-05-21
    公开日:2015-11-27
    发明作者:Pierre Chambard；Come Dorge；Richard Masson；Jean-Baptiste Vaney
    申请人:Messier Bugatti Dowty SA；
    IPC主号:
    专利说明:

    [0001] The invention relates to a disc brake for a vehicle wheel, in particular an aircraft. BACKGROUND OF THE INVENTION Aircraft wheel brakes of a certain size generally include a stack of disks alternately having stators that do not rotate with the wheel and rotors that rotate with the wheel. . The discs are arranged between a rear support and one or more actuators that selectively press the discs against each other to generate a resistive torque which causes a deceleration of the wheel, and thus contribute to braking the aircraft. The disk stack is generally sized to provide braking of the aircraft during an interrupted full load take-off situation. This event, very exceptional in the life of the aircraft, leads to multiply the number of disks to have sufficient frictional interfaces, and to provide a thick stack of disks important. The heat sink formed by the discs is then oversized for routine braking. In addition, the multiplication of the number of disks adversely affects the life of the disks, the wear being all the more important as the number of friction faces is large. OBJECT OF THE INVENTION The object of the invention is a disk brake for an aircraft wheel capable of performing any type of braking, including during a fully loaded, unattended take-off situation, without having oversize disks. PRESENTATION OF THE INVENTION With a view to achieving this object, an aircraft wheel disk brake is provided comprising: friction disks, including rotor disks and stator disks; A structure comprising a torsion tube on which the discs are threaded, a rear plate located at one end of the tube, and a brake actuator support at another end of the tube, the actuators being selectively activatable to apply a force press on the disks. According to the invention, the discs are separated into two groups, of which a first group which is used alone for braking below a given braking torque threshold, and a second group which is used alone or in conjunction with the first one. group, for braking beyond said threshold. Thus, the discs of the first group undergo only the current braking and therefore do not need to be oversized. The disks of the second group may be numerous to multiply the interfaces, but thinner, since they are used only for high-intensity braking, which are rare and generate little wear. Only the discs of the first group are regularly changed as and when they wear, the second group of discs may last longer or even last the life of the aircraft, if they are used only for exceptional braking. In addition, the reduction in the number of rubbing surfaces of the discs of the first group considerably extends its life. All this makes it possible to design a brake whose user cost is much lower than that of a conventional brake. DESCRIPTION OF THE FIGURES The invention will be better understood in the light of the following description of various particular embodiments of the invention, with reference to the figures of the attached drawings, in which: FIG. 1 is a diagrammatic section of a portion aircraft wheel brake according to the invention, illustrating a brake with two heat sinks in a so-called "parallel" arrangement; FIGS. 2A and 2B are figures similar to FIG. 1, showing an alternative embodiment of a brake arranged in parallel; Figure 3 is a schematic section of a wheel brake portion according to the invention, illustrating a brake to two heat sinks in a so-called "series" arrangement; FIG. 4 is a figure similar to FIG. 3, showing an alternative embodiment of a brake available in series; - Figure 5 is a figure similar to Figure 3, showing another alternative embodiment of a brake available in series.
    [0002] DETAILED DESCRIPTION OF PARTICULAR EMBODIMENTS OF THE INVENTION In FIG. 1, an undercarriage axle 1 carrying a wheel 2 is recognized by means of bearings 3. The wheel 2 comprises a rim 4 intended to receive a tire. According to a first embodiment of the invention, the wheel 2 is equipped with a brake 10 comprising: A structure which comprises a torsion tube 11 equipped at its end with a rear plate 12 and at its other end with a support 13 receiving a first group of braking actuators 14 and a second group of actuators 15, arranged further from the axis of rotation of the wheel (only the actuators of each group in the plane of section are here visible, but they are distributed over the entire circumference of the support). The structure, which is centered on the axle, is either fixed to the axle, or prevented from rotating relative to it when braking by means of a torque recovery bar, as is well known; A first group of discs 20, called the first heat sink, which extends between the torsion tube and the rim, comprising rotor discs 20a constrained to rotate with the wheel 2 and stator discs 20b prevented from rotating relative to the tube twist 11; A second group of discs 30, called the second heat sink, which also extends between the torsion tube and the rim, but on the other side of the torsion tube 11, having rotor discs 30a constrained to rotate with the wheel 2 and stator disks 30b prevented from rotating relative to the torsion tube 11. The two heat sinks 20 and 30 are therefore arranged concentrically on either side of the torsion tube. The actuators of the first group 14 are arranged to selectively exert a press force on the first heat sink 20, while the actuators of the second group 15 are arranged to selectively exert a force on the second heat sink. The first heat sink 20 and the first group of actuators 14 are used to provide braking of current intensity, such as taxing braking, and landing braking, so below a given braking torque threshold. In this respect, it will be noted that the discs are thick and therefore in few numbers. It is known that taxing braking, even if they do not require a significant braking force, causes a temperature rise of the discs, and are responsible for a large part of the wear of a conventional brake. The use of thick discs in reduced numbers for a given heat sink length makes it possible to increase the service life of this heat sink in proportion to the reduction in the number of friction faces. The second heat sink 30, which is disposed outside the first heat sink 20, and the second group of actuators 15 are used to provide distress braking of the type that may occur during a take-off. full mass interrupted, which require a much greater braking torque, but with less torque releases than taxing braking. They use less the discs. The second heat sink 30 thus comprises disks in greater number to increase the number of braking interface, and thus the braking torque, but of smaller thickness, since they wear much less. It will be noted that the second heat sink 30 is placed outside the first heat sink, so that the braking torque is increased, for the same press force, because of the greater distance between the axis of the wheel and the point of application of the force of the actuators on the heat sink. This distribution of braking allows the use of two heat sinks each adapted to a specific use. The set, although more complex, requires much less maintenance and has a life before replacement much higher than in conventional brakes. According to a particular aspect of the invention, the discs of the two heat sinks are made of different materials: a friction material which uses little and generates a normal friction for the first heat sink 20, and a material which can use more importantly, but which generates a greater friction, for the second heat sink 30. For high-intensity braking exceeding said torque threshold, such as in interrupted take-off situations in which a very large braking torque is required, it will be possible to size the second heat sink 30 so that it alone can provide this type of braking. Alternatively, the two heat sinks 20, 30 may be used simultaneously, simultaneously activating the two groups of actuators 14, 15. The resulting braking torque is the sum of the braking torques generated by the two heat sinks. The two heat sinks are then used in parallel. According to a variant illustrated in FIGS. 2A and 2B, the brake of the invention is always arranged in a parallel arrangement, but it has only one group of actuators 16. Each actuator 16 is associated with a distribution member 40 that, as long as the braking force developed by the actuator does not exceed a predetermined threshold, applies the force of the actuator on the first heat sink 20, and when the effort required exceeds said threshold apply the force of the actuator to the two heat sinks 20,30. The effort threshold is advantageously chosen so that the first heat sink 20 provides braking below said braking torque threshold, while the other braking is ensured by the use of the two heat sinks. The distribution member comprises a latch 41 which is articulated on the rod 17 of the actuator 16 and which actuates two pushers 42,43. The pusher 43 is facing the first heat sink 20, while the pusher 42 is opposite the second heat sink 30. The latch 41 is connected to the rod 17 of the actuator by a torque mechanism 44 which holds the rocker 41 as shown in Figure 2A, so that only the pusher 43 can press the heat sink 20 opposite, as the force applied by the actuator 16 does not exceed a stress threshold S. When the threshold is exceeded, the torque mechanism 44 gives way, the latch 41 is then free to rotate as shown in Figure 2B, and the two pushers 42,43 bear on their respective heat sinks. The two heat sinks are then solicited simultaneously. At the release of the effort, the dynamometric mechanism is rearmed again to maintain the right-angle swing. According to a second embodiment of the invention illustrated in FIGS. 3 to 5, in which the reference of the similar elements has been increased by one hundred, the two heat sinks 120 and 130 are now no longer arranged in parallel, but in series, one behind the other around the torsion tube 111, the first heat sink 120 being directly opposite the actuators 114. It will be noted that there is more than one group of actuators 114. On each of the illustrated embodiments, a distribution member makes it possible to solicit only the first heat sink up to a determined actuator force threshold, corresponding to a braking torque threshold. When this threshold is exceeded, the distribution member allows the solicitation of the second heat sink to enable it to contribute to the generation of the braking torque. In the first embodiment in series illustrated in Figure 3, the two heat sinks are arranged directly one behind the other. The distribution member comprises a support pallet 145 which is pushed by springs 146 to an abutment 147 interposed between the rear plate 112 and the second heat sink 130. The pallet 145 can be pushed back only when the force exerted by the actuators 114 exceeds the threshold, determined by the stiffness of the springs 146.
    [0003] Note that the bars 148 of the rim 104 which serve to rotate the rotor discs of the two heat sinks 120,130 are discontinuous. They present an interruption in the second heat sink 130. Thus, in the usual braking situations, only the first heat sink 120 can generate a braking torque. The second heat sink 130 receives the press force of the actuator, but since its rotor discs are not rotated by the bars 148, the second heat sink 130 generates no braking torque, and so do not use. If the actuator exerts a force greater than the threshold, the two heat sinks recoil by pushing the pallet 145 so that the rotors disks of the second heat sink 130 engage on the bars 148, and are therefore rotated with the rim 104. The second heat sink 130 then generates a braking torque, which is added to that generated by the first heat sink 120.
    [0004] In the second embodiment in series illustrated in FIG. 4, the distribution member comprises a sleeve 150 slidably mounted without rotation on the torsion tube 111 and which receives the first heat sink 120. The sleeve 150 is pushed back by springs 151 to a stop 152. The sleeve 150 carries a support pad 153 on which the first heat sink comes to rest. In the idle state, a clearance is provided between the bearing pad 153 and the second heat sink 130. The sheath 150 can only be pushed back when the force exerted by the actuator 114 exceeds a given threshold, determined by the stiffness of the springs 151. As long as the force exerted by the actuator 114 does not exceed the threshold, the sleeve 150 does not move, and only the first heat sink 120 is biased to generate a braking torque. When the force exerted by the actuator 114 exceeds the threshold, the sheath 150 moves and presses against the second heat sink, which, thus pressed, also generates a braking torque.
    [0005] In the third embodiment in series illustrated in FIG. 5, the two heat sinks 120 and 130 are engaged on the torsion tube 111. The distribution member comprises a flexible pallet 160 which is interposed between the two heat sinks. 120,130. The pallet has a foot 161 anchored to the torsion tube frangibly. In the idle state, a clearance is provided between the support pallet 160 and the second heat sink 130. As long as the force exerted by the actuator 114 is less than a given threshold, only the first heat sink 120 is biased and generates a braking torque. When the force exerted exceeds the threshold, the anchoring of the foot 161 gives way and the pallet 160 is released and comes into contact with the second heat sink, which is then solicited and generates a braking torque.
    [0006] Alternatively, it is possible to provide a non-breakable anchoring, the pallet 160 being provided so as to come into contact with the second heat sink if the force exerted by the actuators exceeds the threshold, so that the second heat sink contributes to generating the braking torque for braking above said threshold. In the three embodiments in series, the distribution member makes it possible to generate a braking torque only by the first heat sink, up to a force threshold exerted by the actuators. Beyond this threshold, the second heat sink is biased to generate a complementary braking torque, thereby generating a greater total braking torque.
    [0007] The invention is not limited to what has just been described, but on the contrary covers any variant within the scope defined by the claims. In particular, although it has been indicated that the second heat sink is used for landing braking and intense braking (interrupted takeoff at full load), it will be possible to choose to solicit the second heat sink only for these intense braking, using the first heat sink for taxiing braking and landing braking.
    权利要求:
    Claims (10)
    [0001]
    REVENDICATIONS1. Disk brake for an aircraft wheel, comprising: friction discs (20, 30, 120, 130), including rotor disks and stator disks; a structure comprising a torsion tube (11; 111) on which the discs are threaded, a rear plate (12; 112) at one end of the tube, and a support (13; 113) of brake actuators (14; 15,16; 114) at another end of the tube, the actuators being selectively activatable to apply a press force to the disks; characterized in that the disks are separated into two groups, of which a first group (20,120) which is used alone for braking below a given braking torque threshold, and a second group (30,130) which is used alone or together with the first group, for braking beyond said threshold.
    [0002]
    2. Brake according to claim 1, wherein the two groups of disks (20,30) extend on either side of the torsion tube (11).
    [0003]
    3. Brake according to claim 2, wherein the support (13) carries two groups of actuators (14,15) each of the groups of actuators acting on one of the groups of disks.
    [0004]
    4. Brake according to claim 2, wherein the support (13) carries actuators associated with a distribution member which, as the braking force developed by the actuator does not exceed a predetermined threshold, applies the effort of the actuator on the --Framier group of disks (20), and when the effort required exceeds said threshold, applies the force of the actuator on the two groups of disks.
    [0005]
    Brake according to claim 1, in which two groups of discs (120, 130) are arranged one behind the other around the torsion tube (111).
    [0006]
    6. Brake according to claim 5, equipped with a distribution member which, up to a predetermined force threshold exerted by the actuators (114), causes a braking torque to be generated by the first group of disks, and beyond said threshold, causes a braking torque to be generated by the two groups of disks.
    [0007]
    7. Brake according to claim 6, wherein the distribution member comprises a support paddle (145) disposed behind the second group of disks and pushed towards a stop (147) by springs (146) which define a threshold of 'force, and wherein the rim is equipped with bars (148) for rotating the rotor discs which have a discontinuity at the second group of discs so that when the actuators exert a pressing force the two groups of discs in below said threshold, only the rotor disks of the first group of disks are rotated, whereas when the force of the actuators exceeds said threshold, all of the two groups of disks retreat so that the rotor disks of the second group are driven in rotation by engagement on the bars.
    [0008]
    8. Brake according to claim 6, wherein the distribution member comprises a sheath (150) slidably mounted without rotation on the torsion tube (111) and which carries the first group of disks (120), the sheath (150). ) being pushed by springs (151) towards an abutment (152) and carrying a bearing pallet (153) on which the first group of disks comes to rest, so that as long as the force exerted by the actuators (114) does not exceed a threshold determined by the springs, the sleeve does not move and only the first group of discs is biased to generate a braking torque, and when the force exerted by the actuators exceeds said threshold, the sleeve moves and comes press against the second group of disks, which, thus solicited, also generates a braking torque.
    [0009]
    The brake according to claim 6, wherein the distribution member comprises a bearing pad (160) which is interposed between the disk groups (120, 130) by being frangibly anchored on the torsion tube, so that the force exerted by the actuators (114) is less than a threshold, the support pallet (160) does not touch the second group of disks (130) and only the first group of disks (120) is solicited and generates a braking torque, while when the force exerted exceeds the threshold, the anchor gives way and the support pallet (160) is released to come into contact with the second group of disks, which is then solicited and also generates a braking torque.
    [0010]
    The brake according to claim 6, wherein the distribution member comprises a flexible bearing pad (160) which is interposed between the disk groups (120, 130) by being anchored to the torsion tube, so that the force exerted by the actuators (114) is less than a threshold, the support pallet (160) flexes under the force but does not come to touch the second group of discs (130) and only the first group of discs (120) is urged and generates a braking torque, whereas when the force exerted exceeds the threshold, the support pallet (160) flexes sufficiently to come into contact with the second group of disks, which is then solicited and also generates a torque braking.
    类似技术:
    公开号 | 公开日 | 专利标题
    FR3021378A1|2015-11-27|DISC BRAKE FOR AIRCRAFT WHEEL
    EP3089898B1|2018-02-14|Drum brake device including a parking brake operating in duo servo mode, associated vehicle and assembly methods
    EP2876326B1|2016-10-12|Method for renovating and using rear-stator brake discs with pads, assembled disc and corresponding stack of discs
    EP2327595B1|2012-07-18|Aircraft brake management method and -system
    FR2859512A1|2005-03-11|BRAKING SYSTEM
    EP3090190B1|2017-10-18|Actuator with non-reversible screw-and-nut system, drum brake and braking device provided with same
    FR2880602A1|2006-07-14|PROTECTIVE METHOD IN A BRAKE SYSTEM OF A VEHICLE WITH ELECTRIC BRAKES
    CA2773770C|2015-01-27|Process for distribution of braking torque between wheels braked by at least one aircraft landing gear
    EP3002215B1|2017-03-22|An aircraft undercarriage
    FR2982922A1|2013-05-24|ROTARY SHAFT BRAKE SYSTEM, ESPECIALLY FOR ROTOR OR AIRCRAFT PROPELLER, COMPRISING A LINEAR ACTUATOR
    EP2818750B1|2020-05-13|Method for using and renovating a disc of a disc stack
    FR2970698A1|2012-07-27|DEVICE FOR BRAKING AND DRIVING IN ROTATION OF AN AIRCRAFT WHEEL
    FR2566859A1|1986-01-03|DISC BRAKE AND METHOD FOR ASSEMBLY THEREOF
    FR2616501A1|1988-12-16|CLUTCH CONTROL, ESPECIALLY FOR A MOTOR VEHICLE, AND CLUTCH FASTER CLEAR FOR CARRYING OUT SUCH AN ORDER
    EP0720700A1|1996-07-10|Clutch mechanism, particularly for a motor vehicle
    EP0117815B1|1986-07-30|Braking-system with at least one sliding brake-disc and brake-disk for such a braking-system
    WO2016097410A1|2016-06-23|Piston for electric brake actuator, drum brake or disc brake and method of assembly
    EP1900960B1|2009-06-24|Brake pad
    EP2647861B1|2016-03-30|A method of using and renovationg a disk from a stack of disks of vehicle brake
    EP3071855B1|2018-01-03|Drum brake operating in simplex mode and/or in servo-dual mode
    EP0966620B1|2002-05-29|Hybrid multiple disc brake
    FR2755195A1|1998-04-30|Vehicle braking system
    FR2724999A1|1996-03-29|SLIDING CLUTCH INSPECTION, IN PARTICULAR FOR A MOTOR VEHICLE
    FR3097021A1|2020-12-11|REDUCER AND GEAR MOTOR FOR BRAKE WITH INTEGRATED CLUTCH
    EP3074286A2|2016-10-05|Braking system and method
    同族专利:
    公开号 | 公开日
    US9593726B2|2017-03-14|
    GB201507158D0|2015-06-10|
    FR3021378B1|2016-06-03|
    GB2527650A|2015-12-30|
    GB2527650B|2016-09-21|
    US20150337915A1|2015-11-26|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US3480115A|1967-03-22|1969-11-25|Hispano Suiza Lallemant Soc|Disc brakes|
    US4207968A|1978-02-21|1980-06-17|Caterpillar Tractor Co.|Double disc type brake system|
    FR2862280B1|2003-11-14|2006-03-03|Messier Bugatti|LANDING DEVICE, BRAKE FOR AIRCRAFT WHEEL, AIRCRAFT AIRBORNE WHEEL ASSEMBLY, AND METHOD OF MAINTAINING SUCH A LICENSOR|
    FR2890374B1|2005-09-02|2009-05-01|Messier Bugatti Sa|METHOD FOR MANAGING AN ELECTROMECHANICAL BRAKE ACTUATOR, IN PARTICULAR FOR AN AIRCRAFT|
    FR2925017B1|2007-12-13|2010-01-15|Messier Bugatti|METHOD FOR POWER SUPPLYING ACTUATORS ASSOCIATED WITH AN AIRCRAFT LANDING TRAIN|
    US8319384B2|2010-12-15|2012-11-27|Honeywell International Inc.|Electromechanical brake actuator motor brake|
    FR2990413B1|2012-05-10|2014-06-06|Messier Bugatti Dowty|BRAKE FOR AIRCRAFT WHEEL|US9995353B2|2015-12-21|2018-06-12|Goodrich Corporation|Modified actuator design to improve load distribution and damping|
    CN106218870B|2016-04-29|2018-12-11|西安航空制动科技有限公司|A kind of single-wheel double-brake brake machine wheel|
    CN106218869B|2016-04-29|2019-03-19|西安航空制动科技有限公司|A kind of wheel of Contiuum type Twin brakes|
    FR3070370B1|2017-08-28|2019-09-06|Safran Landing Systems|AIR TERMINAL AIR TERMINAL WITH REPORTED AXLE, AND ASSOCIATED ASSEMBLY METHODS|
    FR3082256B1|2018-06-12|2020-05-29|Airbus Helicopters|BRAKING SYSTEM FOR A CALIPER AIRCRAFT LANDING GEAR WITH MULTIPLE BRAKE DISC PUNCHING AREAS|
    GB2583706A|2019-04-23|2020-11-11|Airbus Operations Ltd|Aircraft braking system|
    US11226019B2|2019-09-30|2022-01-18|Goodrich Corporation|Carbon brake stack assembly for improved life|
    法律状态:
    2015-05-21| PLFP| Fee payment|Year of fee payment: 2 |
    2015-11-27| PLSC| Search report ready|Effective date: 20151127 |
    2016-05-20| PLFP| Fee payment|Year of fee payment: 3 |
    2017-05-23| PLFP| Fee payment|Year of fee payment: 4 |
    2017-06-23| CD| Change of name or company name|Owner name: MESSIER-BUGATTI-DOWTY, FR Effective date: 20170518 |
    2018-05-22| PLFP| Fee payment|Year of fee payment: 5 |
    2019-04-19| PLFP| Fee payment|Year of fee payment: 6 |
    2020-04-22| PLFP| Fee payment|Year of fee payment: 7 |
    2021-04-21| PLFP| Fee payment|Year of fee payment: 8 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1454575A|FR3021378B1|2014-05-21|2014-05-21|DISC BRAKE FOR AIRCRAFT WHEEL|FR1454575A| FR3021378B1|2014-05-21|2014-05-21|DISC BRAKE FOR AIRCRAFT WHEEL|
    US14/691,825| US9593726B2|2014-05-21|2015-04-21|Disc brake for an aircraft wheel|
    GB1507158.2A| GB2527650B|2014-05-21|2015-04-28|Disc brake for an aircraft wheel|
    [返回顶部]