US20010007296A1 - Aircraft wheel brake with exchangeable brake segements - Google Patents
Aircraft wheel brake with exchangeable brake segements Download PDFInfo
- Publication number
- US20010007296A1 US20010007296A1 US09/760,158 US76015801A US2001007296A1 US 20010007296 A1 US20010007296 A1 US 20010007296A1 US 76015801 A US76015801 A US 76015801A US 2001007296 A1 US2001007296 A1 US 2001007296A1
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- Prior art keywords
- brake
- segment
- arrangement according
- disk
- ceramic
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D65/12—Discs; Drums for disc brakes
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D55/00—Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes
- F16D55/24—Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes with a plurality of axially-movable discs, lamellae, or pads, pressed from one side towards an axially-located member
- F16D55/26—Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes with a plurality of axially-movable discs, lamellae, or pads, pressed from one side towards an axially-located member without self-tightening action
- F16D55/36—Brakes with a plurality of rotating discs all lying side by side
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D2065/13—Parts or details of discs or drums
- F16D2065/1304—Structure
- F16D2065/1312—Structure circumferentially segmented
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D2065/13—Parts or details of discs or drums
- F16D2065/1304—Structure
- F16D2065/1324—Structure carrying friction elements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D2065/13—Parts or details of discs or drums
- F16D2065/134—Connection
- F16D2065/1392—Connection elements
Definitions
- the invention relates to a brake for a vehicle and particularly an aircraft, but also a land vehicle, including at least one stator brake disk that is fixed to a rotatable wheel axle, and at least one rotor brake disk that is rotatable relative to the wheel axle and arranged parallel to the stator brake disk.
- the stator brake disk includes a brake lining or brake pad arranged circumferentially around a supporting ring that is mechanically secured to the wheel axle.
- multi-disk brakes for the landing gear wheels, especially of larger aircraft such as commercial transport aircraft.
- Such multi-disk brakes include stator disks and rotor disks that are arranged or stacked alternately and parallel to each other to form a brake disk packet.
- the disks of conventional aircraft brakes are generally made essentially of stainless steel (SST) or carbon fiber-reinforced synthetic composites (CFC). Due to the reduced weight and higher braking power capacity, the brake disks of almost all known military and civil aircraft types of modern construction consist of carbon fiber reinforced composites (CFC).
- SST brakes carbon fiber reinforced composites
- a typical aircraft brake using CFC material for both the stator and rotor disks is characterized by a lower total weight and a higher braking load capacity in comparison to aircraft brakes of SST material.
- the CFC brake also avoids the use of an actual brake pad or brake lining per se, because the braking effect is achieved by means of a so-called disk/disk pair.
- a typical aircraft brake using SST material is constructed as a multi-disk brake packet including stator disks and rotor disks arranged alternately in sequence one after another on the wheel axis, and received between an end disk (or backing disk) and a pressure disk (or pressure plate).
- the end disk is located on the side of a counter support bearing, which presses or braces against a support member that is rigidly mounted on the wheel axis and, for example, rigidly screwed to the landing gear strut or the like of the aircraft landing gear.
- the pressure disk on the other hand, is located on the side of a braking piston housing which is screwed to the support on the wheel axis.
- a braking piston received in the braking piston housing selectively exerts a braking force onto the pressure disk in a direction toward the counter bearing, so as to press the alternately stacked discs into frictional contact with each other.
- the support ring can suffer wear or damage as a result of repeated removal of old rivets and re-setting of new rivets.
- the overall maintenance cost and effort is quite considerable for aircraft using such brakes, because such civil aircraft operated by commercial airlines have rather strictly limited time frames prescribed for the maintenance and replacement of the brakes and particularly the brake pads.
- German Patent Publication DE 197 11 829 C1 discloses a method of manufacturing a fiber-reinforced composite ceramic material with high-temperature high-strength fibers on the basis of silicon, carbon, boron, nitrogen or compounds thereof, which are reaction bonded with a matrix of silicon or silicon alloys or compounds.
- Such fiber-reinforced composite ceramic materials are also usable for manufacturing brake disks in a simple and economical manner.
- Other ceramic materials are also generally known in the art.
- a vehicle brake arrangement including a rotatable wheel axle, and a brake disk stack or packet that includes at least one stator brake disk secured on the wheel axle, and at least one rotor brake disk that is rotatably supported relative to the wheel axle and is arranged parallel to the stator brake disk.
- the stator brake disk includes a support arrangement that is mechanically connected to the wheel axle and a brake pad arrangement secured to the support arrangement.
- the support arrangement includes a support ring and a plurality of support members or support arms that protrude substantially radially from the outer circumference of the support ring and are circumferentially spaced apart from one another.
- the brake pad or lining arrangement includes a plurality of plate-shaped brake segments that are respectively removably and exchangeably arranged between respective neighboring ones of the support arms.
- plate-shaped is intended to designate a shape of a member that extends along a plane and that is significantly larger in two dimensions along that plane than in a thickness dimension perpendicular to that plane.
- radial circumferential
- axial axial
- a vehicle brake arrangement including at least one stator brake disk and at least one rotor brake disk as generally described above, whereby the stator brake disk includes a support arrangement and a brake pad arrangement secured thereon.
- the brake pad arrangement includes a plurality of brake segment pads made of a sintered metal material and adhered onto a plate-shaped brake segment carrier, whereby the brake segment carrier and brake segment pad together form a respective brake segment which is removably and exchangeably arranged on the support arrangement.
- the rotor brake disk is made of a ceramic material.
- FIG. 1 shows a schematic axial side view of a portion of a brake arrangement according to the present invention
- FIG. 2 shows a schematic top view of a portion of an inventive brake arrangement, as seen in a radial direction
- FIG. 3 shows a schematic top view of another portion of an inventive brake arrangement, as seen in a radial direction.
- the inventive brake arrangement is applicable to any moving vehicle brake system, including the brakes of a land vehicle (e.g. a rail vehicle or a roadway motor vehicle), the invention is primarily directed to an aircraft landing gear brake. Accordingly, the example embodiment that will be described below relates to an aircraft brake.
- a typical conventional aircraft brake is generally constructed as has been described above. More particularly, the above mentioned brake disk packet or stack is bounded between a pressure disk or pressure plate on the side of the brake piston housing, and a counter disk or counter plate on the side of the counter bearing.
- a brake piston is arranged in the form of a ring in the brake piston housing, and is selectively actuated to exert a braking force onto the pressure disk so as to move the pressure disk toward the counter bearing, thereby clamping the brake disks between the pressure disk and the counter disk.
- the braking effect is thereby achieved in that an increased frictional force and thus an increased resistance against relative rotation is achieved between the rotor brake disks and the stator brake disks due to the axially directed clamping force applied thereto.
- the rotor disks exhibit a higher resistance against being rotated along with the rotating wheel, due to the friction of the rotor disks relative to the stator disks, or even the rotor disks are completely locked or fixed against rotation relative to the stator disks.
- a return spring arrangement retracts the pressure disk back into its initial inactive position, which releases the respective brake disks to allow free rotation therebetween.
- the inventive brake arrangement is generally based on or begins from the above described conventional brake arrangement as a starting point, with further special features according to the invention, as shown in FIGS. 1 to 3 .
- the complete structure of the inventive brake arrangement is generally called or designated as a CMC (ceramic-metal-ceramic) brake. The details thereof will now be described in connection with the drawings.
- the brake arrangement according to the invention includes a brake disk packet arranged between a pressure disk 20 and a counter disk, as generally described above. Furthermore, the inventive brake arrangement includes guide elements arranged with respect to the pressure disk 20 and the counter disk mentioned above, as well as a brake piston housing with a brake piston that acts on the pressure disk, and a counter bearing that supports or braces the counter disk, as generally discussed above.
- the arrangement of the pressure disk, the counter disk, the brake piston and its housing, the counter bearing, and the guide elements to allow a relative lateral or axial guided motion of the components when the brake piston exerts a braking force onto the pressure disk can be according to any conventionally known arrangement, and will not be described or illustrated in detail herein.
- the brake disk packet includes a plurality of alternately arranged or stacked stator brake disks 1 and rotor brake disks 2 .
- Each individual stator brake disk 1 is secured onto a wheel axle 3 , which rotates as shown by the arrow M together with the respective associated aircraft landing gear wheel that is carried by this wheel axle 3 .
- each individual rotor brake disk 2 is movably or rotatably supported relative to the wheel axle 3 , so that the rotor brake disk 2 can rotate relative to the wheel axle 3 , or vice versa.
- one set of the brake disks rotates together with the rotating wheel that is to be braked, and the other set of brake disks remains relatively stationary with respect to the vehicle, for example by being fixed to a non-rotating frame member of the vehicle.
- the terms “rotor” and “stator” are of course dependent on the frame of reference for the motion.
- the respective stator brake disks 1 and rotor brake disks 2 of the brake disk packet are all arranged parallel to one another, i.e. the major brake disk surfaces of the brake disks extending radially relative to the axis of the wheel axle 3 are all parallel to one another.
- a frictional force F is generated respectively between the rotor brake disks and the brake pads of the stator brake disks when the braking force is applied thereto in the axial direction.
- FIG. 1 shows a side view or end view of half of a stator brake disk 1 , which comprises a support arrangement including a support ring 4 and a plurality of support members or support arms 6 protruding radially outwardly from an outer circumferential surface of the support ring 4 .
- An inner circumferential surface of the support ring 4 is provided with key-way grooves 5 which engage with the keys or splines of a splined shaft, by which the support ring 4 is mechanically fixed to the wheel axle 3 , which is simply schematically indicated by the axis 3 .
- the several support arms 6 protruding radially from the outer circumferential surface of the support ring 4 are uniformly circumferentially spaced from one another, for example by about 90° in the embodiment of FIG. 1 having four of the support arms 6 .
- the support arms 6 are rigidly connected to the support ring 4 , for example being integrally formed with the support ring 4 or being rigidly secured thereto by welding, riveting, bolting, etc.
- respective annular disk-shaped support areas or spaces 10 are formed between successive ones of the support arms 6 .
- four such spaces 10 are provided respectively between successive ones of the four support arms 6 .
- a respective plurality of brake segments 7 are respectively arranged in these annular arc-segment shaped spaces 10 between the successive support arms 6 .
- the brake segments 7 respectively extend along a radial plane perpendicular to the wheel axis 3 , and are secured to and between the support arms 6 as will be described in detail below.
- the particular structure of each brake segment 7 will also be described in more detail below.
- Each individual support arm 6 preferably has a non-rectangular cross-section, and for example has a trapezoid-shaped cross-section.
- each individual support arm 6 does not have a cylindrical shape, but rather an angular three-dimensional body shape, for example in the form of a frustum of a cone.
- the base of such a support arm body is rigidly secured onto the outer circumference of the support ring 4 , preferably to be substantially flush with the ring width of the support ring 4 .
- each one of the support arms 6 is equipped with a rotatable or pivotable locking member 8 , which is rotatable or pivotable relative to the support arm 6 , and particularly about the longitudinal axis of the support arm 6 , which extends radially relative to the wheel axis 3 .
- the pivotable locking member 8 comprises a latch disk or bar 81 with a pivot hole therein, through which a bolt or screw 9 is fastened into the end of the support arm 6 so as to pivotably hold the locking member 8 to the support arm 6 .
- a threaded hole may simply be provided in the free end of the support arm 6 .
- FIGS. 2 and 3 in connection with FIG. 1.
- At least alternate ones of the support arms 6 are respectively equipped with a spring-biased catch 12 that is movably, e.g. pivotably, arranged in a slot-shaped recess in a lateral side of the first support arm 61 , facing circumferentially toward the next or second support arm 62 (see FIG. 1).
- a spring (not shown) is arranged to urge or bias the catch 12 laterally outwardly from the side of the first support arm 61 toward the second support arm 62 .
- Each one of the support arms 6 may be provided with such a catch 12 , for example on only one side of the respective support arm facing toward the next support arm.
- a respective brake segment 7 is received in a respective one of the receiving areas or support spaces 10 having an annular segment shape, between the adjacent is first support arm 61 and second support arm 62 .
- the spring-biased catch 12 on the first support arm 61 presses the brake segment 7 circumferentially tightly against the second support arm 62
- the latch bar 81 of each pivotable locking member 8 is toggled or pivoted into a circumferential extending position so as to securely hold the brake segment 7 in the respective support space 10 , and against a corresponding segment 11 of the circumferential surface of the support ring 4 bounding the support space 10 .
- the annular arc segment shaped support space 10 is bounded between the circumferential surface segment 11 of the support ring 4 , the two mutually facing sides of the support arms 61 and 62 , and an imaginary circular arc extending between the radially inwardly facing surfaces of the two latch bars 81 of the two locking members 8 of the support arms 61 and 62 .
- the brake segment 7 preferably entirely fills this annular segment-shaped space 10 .
- FIGS. 2 and 3 the respective possible positions of the latch bar 81 of the pivotable locking member 8 are evident.
- a latch bar 81 of a locking member 8 of a respective support arm 61 is shown in solid lines in a position in which the longitudinal extension of the latch bar 81 is aligned parallel to the wheel axis 3 .
- This position is the unlatched position, in which the respective brake segments 7 can be removed from the respective support spaces 10 .
- This same latch bar 81 is shown with dotted lines in a locked or latched position, in which the longitudinal extension of the latch bar 81 is aligned circumferentially on a plane perpendicular to the wheel axis 3 .
- FIG. 1 further shows additional preferred features of a brake segment 7 for ensuring that the brake segment 7 is fixedly secured in the respective corresponding support space 10 between two successive ones of the support arms 6 .
- the brake segment 7 On one end of the brake segment 7 , namely the end thereof facing and contacting the side of the first support arm 61 provided with the spring-biased catch 12 , the brake segment 7 has a recess 16 into which the spring-biased catch 12 engages. Thereby, the brake segment 7 effectively snaps and engages into its secured position by the engagement of the catch 12 into the recess 16 .
- a fixing element here particularly embodied as a protruding nose or hook 15 , protrudes radially outwardly and hooks in the circumferential direction from the circumferentially outer corner of the brake segment 7 .
- This fixing element or hook 15 preferably integrally protrudes from the structure of the brake segment 7 , as will be discussed below.
- the hook 15 hooks around the above-described latch bar 81 when the latch bar is in the locking position.
- the brake segment 7 is positively and fixedly secured to the support ring 4 , yet remains easily replaceable or exchangeable, by simply pivoting the latching bars 81 by 90°, depressing the spring-biased catch 12 against the biasing force of the spring, and then tilting and lifting the used brake segment 7 substantially radially out of the support space 10 .
- a new brake segment 7 is installed and secured in this support space 10 by carrying out the opposite procedure.
- FIG. 2 shows a top view of a portion of the inventive brake disk arrangement, and particularly only a portion of a brake disk stack, including a single stator brake disk 1 and a single rotor brake disk 2 arranged parallel to each other along the wheel axis 3 .
- the complete brake arrangement includes a plurality of alternating stator brake disks and rotor brake disks arranged between a pressure plate and a counter plate as described above.
- each respective brake segment 7 which comprises a plate-shaped brake segment carrier or substrate 13 and a brake segment lining or pad 14 respectively secured on (one side or) both opposite sides of the brake segment carrier 13 .
- the brake segment pads 14 are preferably adhesively bonded onto the brake segment carrier 13 using an appropriate adhesive for the respective materials being bonded and with a sufficient temperature resistance in view of the expected operating temperatures of the brake arrangement.
- dashed lines indicating the locked or latched position of the latch bar 81 in FIG. 2 it is clear that the latch bar 81 only bears against the brake segment carrier 13 , and does not apply any locking force onto the brake segment pads 14 .
- the latch bar 81 does not interfere with the adjacent rotor brake disk 2 .
- the above described support arms 6 do not protrude beyond the effective brake surfaces of the brake segment pads 14 in the axial direction of the wheel axis 3 .
- the effective brake pad surfaces of the brake segment pads 14 will come into contact with the facing surface of the rotor brake disk 2 when a braking force is clampingly applied to the brake disk stack or packet.
- FIG. 3 shows another portion of the brake disk packet, namely a portion at an end of the brake disk packet, including a pressure disk 20 and an adjacent rotor brake disk 2 .
- a respective brake segment carrier 13 is provided with a brake segment lining or pad 14 on only one side thereof, namely the side facing the adjacent rotor brake disk 2 .
- the opposite side of the brake segment carrier 13 is adjacent to the pressure disk 20 .
- the pivotable locking member 8 secured to the support arm 61 in this case, secures the stator brake disk 1 to the pressure disk 20 .
- the latch bar 81 once it is turned into the illustrated latching position and the screw or bolt 9 is turned tight, bears on and secures the brake segment carrier 13 while also overlapping onto the outer circumference of the pressure disk 20 .
- the stator brake disk 1 is secured to the pressure disk 20
- the respective rotor brake disks 2 of the stack or packet are each secured to the rotating wheel axle indicated by the wheel axis 3 .
- the brake segment pads 14 of the brake segments 7 as described above are fabricated of a sintered metal material which is securely joined onto the plate-segment-shaped brake segment carrier 13 , for example by an adhesive that is suitable for the materials and temperatures at hand.
- the brake segment pads 14 can be sintered, brazed, or welded onto the brake segment carrier 13 .
- These two elements are securely joined to each other to form the removable brake segment 7 , which can be exchanged and replaced as a unit relative to the support ring 4 .
- This replacement or exchange of the brake segments 7 can be carried out not only to replace used brake segments 7 with new brake segments 7 , but also to achieve different braking characteristics simply by installing different brake segments 7 , for example made of different materials.
- the support ring 4 , the support arms 6 , 61 , 62 , and the brake segment carrier 13 can respectively be made of any suitable materials, such as light metal alloys known in the art.
- the rotor brake disks 2 are fabricated of a ceramic material. Thus, the alternating braking contact between the sintered metal brake segment pads 14 and the ceramic rotor brake disks 2 provides the desired friction to achieve the required braking effect.
- the ceramic material of the rotor brake disks 2 is a fiber-reinforced ceramic material, of which the reinforcement fibers are preferably homogeneously distributed in order to achieve uniform and homogeneous thermo-physical material characteristics.
- a fiber-reinforced ceramic is especially advantageous in that it withstands, transmits, and thereby reduces the internal stresses that arise during the braking process within the rotor brake disks 2 .
- Such a fiber-reinforced ceramic material also provides a good thermal conductivity through the cross-section of the rotor brake disk 2 , which allows the frictional heat during the braking process to be dissipated effectively.
- the rotor brake disks may be made of a C/SiC, C/SiSiC, SiC/Sic, SiC/SiSiC or other ceramic comprising an oxide ceramic system.
- Such an oxide system ceramic may comprise Nextel (TM) fibers on the basis of aluminum dioxide with an oxide matrix, for example mullite, or in combination with a carbide matrix such as SiC.
- the ceramic material of the rotor brake disk 2 preferably comprises a combination of approximately 75 to 40 vol. % of short carbon fibers, approximately 40 to 70 vol. % of silicon carbide, and a maximum of 15 vol. % of silicon.
- the term “approximately” designates a range of ⁇ 1 vol. %, for example.
- the term “short fibers” has its ordinary art-recognized meaning, based on the aspect ratio or length of the fibers.
- the ceramic raw material substances are mixed as homogeneously as possible to form the rotor brake disks 2 .
- a homogenous distribution of carbon fibers can be achieved by carrying out a pressing process to form the brake disk, with a preferred orientation of the carbon fibers in the plane of the brake disk. In such a process, only relatively few large pores, which would form initiation sites for the cumulation of free silicon, will arise. On the other hand, fine pores will be homogeneously distributed, whereby these fine pores become significant for silicon melt infiltration during the fabrication of the brake disk.
- the molten liquid silicon reacts with the matrix carbon while thereby forming a rather large proportion of silicon carbide, which is advantageous for achieving a high thermal conductivity in the direction perpendicular to the major planes of the brake disk.
- any conventionally known I- brake pad or brake lining materials for example materials conventionally used in the brake pads of rail vehicles and motor vehicles, may alternatively be used for the brake segment pads 14 of the stator brake disks 1 according to the invention.
- a person of ordinary skill in the art will readily be able to select a suitable material among available organic-based pad materials or metal/carbon composite pad materials.
- FIG. 1 Another optional but advantageous detail is to provide hollow spaces or venting passages within the stator brake disks 1 or the rotor disks, in order to provide an air-cooling effect to improve the dissipation of the frictionally generated heat during braking.
- Such hollow chambers or air vent passages can be provided in any configuration or any manner known in the prior art relevant to brake arrangements.
- the inventive arrangement allows a very simple, quick and economical replacement or exchange of the brake segments 7 .
- the pivotable locking members 8 are simply opened by turning the latching bars 81 by 90° so that they do not bear on and secure the brake segment carriers 13 .
- the respective released brake segment 7 is simply pulled essentially radially away from the wheel axis 3 , whereby it may be additionally necessary or advantageous to depress the spring-biased catch 12 in order to release the catch 12 from the corresponding recess 16 in the brake segment carrier 13 .
- a new brake segment 7 is simply placed into the now-vacant support space 10 , whereby the spring-biased catch 12 engages into the corresponding recess 16 of the new brake segment 7 .
- the latching bars 81 are simply turned by 90° to be aligned in a circumferential direction and thereby securely lock the brake segments 7 into place. Due to the simple access and removal and replacement of the brake segments 7 in this manner, it is very simple to carry out the brake segment exchange without needing to disassemble the other remaining components of the brake arrangement.
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Abstract
Description
- PRIORITY CLAIM
- This application is based on and claims the priority under 35 U.S.C. §119 of German Patent Application 100 00 915.8, filed on Jan. 12, 2000, the entire disclosure of which is incorporated herein by reference.
- The invention relates to a brake for a vehicle and particularly an aircraft, but also a land vehicle, including at least one stator brake disk that is fixed to a rotatable wheel axle, and at least one rotor brake disk that is rotatable relative to the wheel axle and arranged parallel to the stator brake disk. The stator brake disk includes a brake lining or brake pad arranged circumferentially around a supporting ring that is mechanically secured to the wheel axle.
- In the field of aircraft construction, it is conventionally known to use hydraulically actuated multi-disk brakes for the landing gear wheels, especially of larger aircraft such as commercial transport aircraft. Such multi-disk brakes include stator disks and rotor disks that are arranged or stacked alternately and parallel to each other to form a brake disk packet. The disks of conventional aircraft brakes are generally made essentially of stainless steel (SST) or carbon fiber-reinforced synthetic composites (CFC). Due to the reduced weight and higher braking power capacity, the brake disks of almost all known military and civil aircraft types of modern construction consist of carbon fiber reinforced composites (CFC). Such CFC aircraft brakes, however, suffer the disadvantage of a high replacement cost, while SST brakes have a relatively short operating life (in comparison to CFC brakes), due to the high loads and resultant wear occurring during the braking of large aircraft.
- A typical aircraft brake using CFC material for both the stator and rotor disks is characterized by a lower total weight and a higher braking load capacity in comparison to aircraft brakes of SST material. The CFC brake also avoids the use of an actual brake pad or brake lining per se, because the braking effect is achieved by means of a so-called disk/disk pair.
- On the other hand, a typical aircraft brake using SST material is constructed as a multi-disk brake packet including stator disks and rotor disks arranged alternately in sequence one after another on the wheel axis, and received between an end disk (or backing disk) and a pressure disk (or pressure plate). The end disk is located on the side of a counter support bearing, which presses or braces against a support member that is rigidly mounted on the wheel axis and, for example, rigidly screwed to the landing gear strut or the like of the aircraft landing gear. The pressure disk, on the other hand, is located on the side of a braking piston housing which is screwed to the support on the wheel axis. A braking piston received in the braking piston housing selectively exerts a braking force onto the pressure disk in a direction toward the counter bearing, so as to press the alternately stacked discs into frictional contact with each other.
- The brake linings or pads, which are subjected to extreme loads and resultant high wear due to the braking process, are rather difficult to replace, i.e. exchange, after they have been worn beyond an acceptable limit. Namely, a complete disassembling of the brake arrangement is practically always required when it is necessary to exchange the brake linings or pads. Since the brake pads are secured to the brake disk or rotor support ring by rivets, these rivet connections must be bored out or otherwise broken or released in order to exchange the used brake pads with new brake pads. Then the new brake pads are once again riveted onto the associated support ring. Then, the rest of the previously disassembled brake arrangement must be reassembled. As can be appreciated, this is a very time consuming and costly process.
- Also, the support ring can suffer wear or damage as a result of repeated removal of old rivets and re-setting of new rivets. The overall maintenance cost and effort is quite considerable for aircraft using such brakes, because such civil aircraft operated by commercial airlines have rather strictly limited time frames prescribed for the maintenance and replacement of the brakes and particularly the brake pads.
- The German Patent Publication DE 197 11 829 C1 discloses a method of manufacturing a fiber-reinforced composite ceramic material with high-temperature high-strength fibers on the basis of silicon, carbon, boron, nitrogen or compounds thereof, which are reaction bonded with a matrix of silicon or silicon alloys or compounds. Such fiber-reinforced composite ceramic materials are also usable for manufacturing brake disks in a simple and economical manner. Other ceramic materials are also generally known in the art. For example, a fiber-reinforced ceramic with an oxide system, for example Nextel (TM) fibers of the 3M Company, based on alumina with an oxide matrix, such as mullite for example, or in combination with a carbide matrix, such as silicon carbide for example, are generally known in the art.
- Without further going into the details, there is no known reference in the relevant trade literature, that makes a suggestion to use brake pads made of the above mentioned materials in the above mentioned manner for vehicle brakes and particularly air-craft brakes. The trade literature further gives no hints or suggestions toward the particular localized use of at least one of such brake disks as a stator or a rotor within a multi-disk brake packet of an aircraft brake.
- In the field of aircraft construction, there has been a constant effort to achieve landing gear wheel brakes having a relatively low weight, a relatively high braking power capacity, an economical fabrication, and relatively low expected maintenance and replacement part costs, in comparison to prior conventional aircraft brakes. Mostly due to these constant efforts to achieve these advantages in combination, there has never been achieved or suggested a multi-disk brake with alternating disks of different materials, and particularly using a fiber-reinforced ceramic for one of the two brake disks that will come into contact with each other, in view of the braking properties and the unavoidable wear of the effective brake surfaces of such a vehicle brake.
- In view of the above, it is an object of the invention to provide a vehicle brake arrangement having a low total weight and a high braking power capacity, and which utilizes brake disks that achieve a simple and economical maintenance with a simple and quick exchange of the brake linings or pads, in comparison to prior art brake arrangements. The invention further aims to avoid or overcome the disadvantages of the prior art, and to achieve additional advantages, as apparent from the present specification.
- The above objects have been achieved according to the invention in a vehicle brake arrangement including a rotatable wheel axle, and a brake disk stack or packet that includes at least one stator brake disk secured on the wheel axle, and at least one rotor brake disk that is rotatably supported relative to the wheel axle and is arranged parallel to the stator brake disk. The stator brake disk includes a support arrangement that is mechanically connected to the wheel axle and a brake pad arrangement secured to the support arrangement. The support arrangement includes a support ring and a plurality of support members or support arms that protrude substantially radially from the outer circumference of the support ring and are circumferentially spaced apart from one another. The brake pad or lining arrangement includes a plurality of plate-shaped brake segments that are respectively removably and exchangeably arranged between respective neighboring ones of the support arms.
- Throughout this specification, the term “plate-shaped” is intended to designate a shape of a member that extends along a plane and that is significantly larger in two dimensions along that plane than in a thickness dimension perpendicular to that plane. Throughout this specification, the terms “radial”, “circumferential”, “axial” and the like are to be understood with respect to the rotation axis of the rotating set of brake discs, unless otherwise stated or apparent from a particular context.
- The above objects have further been achieved according to the invention in a vehicle brake arrangement including at least one stator brake disk and at least one rotor brake disk as generally described above, whereby the stator brake disk includes a support arrangement and a brake pad arrangement secured thereon. The brake pad arrangement includes a plurality of brake segment pads made of a sintered metal material and adhered onto a plate-shaped brake segment carrier, whereby the brake segment carrier and brake segment pad together form a respective brake segment which is removably and exchangeably arranged on the support arrangement. The rotor brake disk is made of a ceramic material. By selectively bringing the rotor brake disk into contact with the brake segment pad of the stator brake disk, the resulting friction provides the desired braking effect.
- In order that the invention may be clearly understood, it will now be described in connection with example embodiments, with reference to the accompanying drawings, wherein:
- FIG. 1 shows a schematic axial side view of a portion of a brake arrangement according to the present invention;
- FIG. 2 shows a schematic top view of a portion of an inventive brake arrangement, as seen in a radial direction; and
- FIG. 3 shows a schematic top view of another portion of an inventive brake arrangement, as seen in a radial direction.
- While the inventive brake arrangement is applicable to any moving vehicle brake system, including the brakes of a land vehicle (e.g. a rail vehicle or a roadway motor vehicle), the invention is primarily directed to an aircraft landing gear brake. Accordingly, the example embodiment that will be described below relates to an aircraft brake.
- A typical conventional aircraft brake is generally constructed as has been described above. More particularly, the above mentioned brake disk packet or stack is bounded between a pressure disk or pressure plate on the side of the brake piston housing, and a counter disk or counter plate on the side of the counter bearing. A brake piston is arranged in the form of a ring in the brake piston housing, and is selectively actuated to exert a braking force onto the pressure disk so as to move the pressure disk toward the counter bearing, thereby clamping the brake disks between the pressure disk and the counter disk. The braking effect is thereby achieved in that an increased frictional force and thus an increased resistance against relative rotation is achieved between the rotor brake disks and the stator brake disks due to the axially directed clamping force applied thereto. Thus, the rotor disks exhibit a higher resistance against being rotated along with the rotating wheel, due to the friction of the rotor disks relative to the stator disks, or even the rotor disks are completely locked or fixed against rotation relative to the stator disks. Once the braking force is no longer applied by the brake piston, a return spring arrangement retracts the pressure disk back into its initial inactive position, which releases the respective brake disks to allow free rotation therebetween.
- The inventive brake arrangement is generally based on or begins from the above described conventional brake arrangement as a starting point, with further special features according to the invention, as shown in FIGS.1 to 3. The complete structure of the inventive brake arrangement is generally called or designated as a CMC (ceramic-metal-ceramic) brake. The details thereof will now be described in connection with the drawings.
- The brake arrangement according to the invention includes a brake disk packet arranged between a
pressure disk 20 and a counter disk, as generally described above. Furthermore, the inventive brake arrangement includes guide elements arranged with respect to thepressure disk 20 and the counter disk mentioned above, as well as a brake piston housing with a brake piston that acts on the pressure disk, and a counter bearing that supports or braces the counter disk, as generally discussed above. The arrangement of the pressure disk, the counter disk, the brake piston and its housing, the counter bearing, and the guide elements to allow a relative lateral or axial guided motion of the components when the brake piston exerts a braking force onto the pressure disk, can be according to any conventionally known arrangement, and will not be described or illustrated in detail herein. - The brake disk packet includes a plurality of alternately arranged or stacked
stator brake disks 1 androtor brake disks 2. Each individualstator brake disk 1 is secured onto awheel axle 3, which rotates as shown by the arrow M together with the respective associated aircraft landing gear wheel that is carried by thiswheel axle 3. On the other hand, each individualrotor brake disk 2 is movably or rotatably supported relative to thewheel axle 3, so that therotor brake disk 2 can rotate relative to thewheel axle 3, or vice versa. In general, it can be said that one set of the brake disks rotates together with the rotating wheel that is to be braked, and the other set of brake disks remains relatively stationary with respect to the vehicle, for example by being fixed to a non-rotating frame member of the vehicle. The terms “rotor” and “stator” are of course dependent on the frame of reference for the motion. The respectivestator brake disks 1 androtor brake disks 2 of the brake disk packet are all arranged parallel to one another, i.e. the major brake disk surfaces of the brake disks extending radially relative to the axis of thewheel axle 3 are all parallel to one another. As a result of the relative rotation M, a frictional force F is generated respectively between the rotor brake disks and the brake pads of the stator brake disks when the braking force is applied thereto in the axial direction. - FIG. 1 shows a side view or end view of half of a
stator brake disk 1, which comprises a support arrangement including asupport ring 4 and a plurality of support members orsupport arms 6 protruding radially outwardly from an outer circumferential surface of thesupport ring 4. An inner circumferential surface of thesupport ring 4 is provided with key-way grooves 5 which engage with the keys or splines of a splined shaft, by which thesupport ring 4 is mechanically fixed to thewheel axle 3, which is simply schematically indicated by theaxis 3. Theseveral support arms 6 protruding radially from the outer circumferential surface of thesupport ring 4 are uniformly circumferentially spaced from one another, for example by about 90° in the embodiment of FIG. 1 having four of thesupport arms 6. Thesupport arms 6 are rigidly connected to thesupport ring 4, for example being integrally formed with thesupport ring 4 or being rigidly secured thereto by welding, riveting, bolting, etc. - With this arrangement, respective annular disk-shaped support areas or
spaces 10 are formed between successive ones of thesupport arms 6. For example, in the embodiment of FIG. 1, foursuch spaces 10, each spanning substantially almost 90°, are provided respectively between successive ones of the foursupport arms 6. A respective plurality ofbrake segments 7 are respectively arranged in these annular arc-segment shapedspaces 10 between thesuccessive support arms 6. Thebrake segments 7 respectively extend along a radial plane perpendicular to thewheel axis 3, and are secured to and between thesupport arms 6 as will be described in detail below. The particular structure of eachbrake segment 7 will also be described in more detail below. - Each
individual support arm 6 preferably has a non-rectangular cross-section, and for example has a trapezoid-shaped cross-section. As a further example, eachindividual support arm 6 does not have a cylindrical shape, but rather an angular three-dimensional body shape, for example in the form of a frustum of a cone. The base of such a support arm body is rigidly secured onto the outer circumference of thesupport ring 4, preferably to be substantially flush with the ring width of thesupport ring 4. - The outwardly protruding free end of each one of the
support arms 6 is equipped with a rotatable orpivotable locking member 8, which is rotatable or pivotable relative to thesupport arm 6, and particularly about the longitudinal axis of thesupport arm 6, which extends radially relative to thewheel axis 3. In its simplest form, thepivotable locking member 8 comprises a latch disk or bar 81 with a pivot hole therein, through which a bolt orscrew 9 is fastened into the end of thesupport arm 6 so as to pivotably hold the lockingmember 8 to thesupport arm 6. For example, a threaded hole may simply be provided in the free end of thesupport arm 6. In this regard, also see FIGS. 2 and 3 in connection with FIG. 1. - As a further device for securing a
respective brake segment 7 between successive ones of thesupport arms 6, at least alternate ones of thesupport arms 6, e.g. afirst support arm 61, are respectively equipped with a spring-biasedcatch 12 that is movably, e.g. pivotably, arranged in a slot-shaped recess in a lateral side of thefirst support arm 61, facing circumferentially toward the next or second support arm 62 (see FIG. 1). A spring (not shown) is arranged to urge or bias thecatch 12 laterally outwardly from the side of thefirst support arm 61 toward thesecond support arm 62. Each one of thesupport arms 6 may be provided with such acatch 12, for example on only one side of the respective support arm facing toward the next support arm. - As can be seen in FIG. 1, a
respective brake segment 7 is received in a respective one of the receiving areas orsupport spaces 10 having an annular segment shape, between the adjacent isfirst support arm 61 andsecond support arm 62. Thereby, the spring-biasedcatch 12 on thefirst support arm 61 presses thebrake segment 7 circumferentially tightly against thesecond support arm 62, while thelatch bar 81 of eachpivotable locking member 8 is toggled or pivoted into a circumferential extending position so as to securely hold thebrake segment 7 in therespective support space 10, and against a corresponding segment 11 of the circumferential surface of thesupport ring 4 bounding thesupport space 10. In its entirety, the annular arc segment shapedsupport space 10 is bounded between the circumferential surface segment 11 of thesupport ring 4, the two mutually facing sides of thesupport arms latch bars 81 of the two lockingmembers 8 of thesupport arms brake segment 7 preferably entirely fills this annular segment-shapedspace 10. - In FIGS. 2 and 3, the respective possible positions of the
latch bar 81 of thepivotable locking member 8 are evident. In FIG. 2, alatch bar 81 of a lockingmember 8 of arespective support arm 61 is shown in solid lines in a position in which the longitudinal extension of thelatch bar 81 is aligned parallel to thewheel axis 3. This position is the unlatched position, in which therespective brake segments 7 can be removed from therespective support spaces 10. Thissame latch bar 81 is shown with dotted lines in a locked or latched position, in which the longitudinal extension of thelatch bar 81 is aligned circumferentially on a plane perpendicular to thewheel axis 3. This is the locked or latched position, in which thelatch bar 81 securely holds therespective brake segments 7 in therespective support spaces 10 on the two opposite sides of therespective support arm 61. Such a locking or latching position of thelatch bar 81 of anothersupport arm 61 is shown in FIG. 3 as well, where thislatch bar 81 secures a “one-sided” brake segment in connection with apressure plate 20 as will be described below. - FIG. 1 further shows additional preferred features of a
brake segment 7 for ensuring that thebrake segment 7 is fixedly secured in the respectivecorresponding support space 10 between two successive ones of thesupport arms 6. On one end of thebrake segment 7, namely the end thereof facing and contacting the side of thefirst support arm 61 provided with the spring-biasedcatch 12, thebrake segment 7 has a recess 16 into which the spring-biasedcatch 12 engages. Thereby, thebrake segment 7 effectively snaps and engages into its secured position by the engagement of thecatch 12 into the recess 16. On the other end of thebrake segment 7, a fixing element, here particularly embodied as a protruding nose orhook 15, protrudes radially outwardly and hooks in the circumferential direction from the circumferentially outer corner of thebrake segment 7. This fixing element or hook 15 preferably integrally protrudes from the structure of thebrake segment 7, as will be discussed below. Thehook 15 hooks around the above-describedlatch bar 81 when the latch bar is in the locking position. - With the above described measures, the
brake segment 7 is positively and fixedly secured to thesupport ring 4, yet remains easily replaceable or exchangeable, by simply pivoting the latching bars 81 by 90°, depressing the spring-biasedcatch 12 against the biasing force of the spring, and then tilting and lifting the usedbrake segment 7 substantially radially out of thesupport space 10. Anew brake segment 7 is installed and secured in thissupport space 10 by carrying out the opposite procedure. - FIG. 2 shows a top view of a portion of the inventive brake disk arrangement, and particularly only a portion of a brake disk stack, including a single
stator brake disk 1 and a singlerotor brake disk 2 arranged parallel to each other along thewheel axis 3. It should be understood that the complete brake arrangement includes a plurality of alternating stator brake disks and rotor brake disks arranged between a pressure plate and a counter plate as described above. - In any event, the detail view of FIG. 2 shows the structure of each
respective brake segment 7, which comprises a plate-shaped brake segment carrier orsubstrate 13 and a brake segment lining orpad 14 respectively secured on (one side or) both opposite sides of thebrake segment carrier 13. Thebrake segment pads 14 are preferably adhesively bonded onto thebrake segment carrier 13 using an appropriate adhesive for the respective materials being bonded and with a sufficient temperature resistance in view of the expected operating temperatures of the brake arrangement. As shown by the dashed lines indicating the locked or latched position of thelatch bar 81 in FIG. 2, it is clear that thelatch bar 81 only bears against thebrake segment carrier 13, and does not apply any locking force onto thebrake segment pads 14. This is also true of the above described protruding hook 15 (i.e. the hook integrally protrudes from thecarrier 13 but not the pads 14) and the recess 16 cooperating with the spring-loaded 20 catch 12 (i.e. the recess 16 is provided in the edge of thecarrier 13 but not in the pads 14). Namely, all of the securing and bearing force is applied to the structurally strongbrake segment carrier 13, while thebrake segment pads 14 are adhesively carried by thecarrier 13. - It is further apparent that the
latch bar 81 does not interfere with the adjacentrotor brake disk 2. Also, the above describedsupport arms 6 do not protrude beyond the effective brake surfaces of thebrake segment pads 14 in the axial direction of thewheel axis 3. Thus, only the effective brake pad surfaces of thebrake segment pads 14 will come into contact with the facing surface of therotor brake disk 2 when a braking force is clampingly applied to the brake disk stack or packet. - FIG. 3 shows another portion of the brake disk packet, namely a portion at an end of the brake disk packet, including a
pressure disk 20 and an adjacentrotor brake disk 2. In this area, a respectivebrake segment carrier 13 is provided with a brake segment lining orpad 14 on only one side thereof, namely the side facing the adjacentrotor brake disk 2. The opposite side of thebrake segment carrier 13 is adjacent to thepressure disk 20. As further shown in FIG. 3, thepivotable locking member 8 secured to thesupport arm 61, in this case, secures thestator brake disk 1 to thepressure disk 20. Namely, thelatch bar 81, once it is turned into the illustrated latching position and the screw orbolt 9 is turned tight, bears on and secures thebrake segment carrier 13 while also overlapping onto the outer circumference of thepressure disk 20. Thus, thestator brake disk 1 is secured to thepressure disk 20, while the respectiverotor brake disks 2 of the stack or packet are each secured to the rotating wheel axle indicated by thewheel axis 3. - The following description will address the various materials that can be used to manufacture the
brake segment 7 to achieve selected particular braking characteristics of the so-called CMC brake while allowing the efficient replacement or exchange of the brake pads. In this context, thebrake segment pads 14 of thebrake segments 7 as described above are fabricated of a sintered metal material which is securely joined onto the plate-segment-shapedbrake segment carrier 13, for example by an adhesive that is suitable for the materials and temperatures at hand. Alternatively, thebrake segment pads 14 can be sintered, brazed, or welded onto thebrake segment carrier 13. These two elements are securely joined to each other to form theremovable brake segment 7, which can be exchanged and replaced as a unit relative to thesupport ring 4. This replacement or exchange of thebrake segments 7 can be carried out not only to replace usedbrake segments 7 withnew brake segments 7, but also to achieve different braking characteristics simply by installingdifferent brake segments 7, for example made of different materials. - The
support ring 4, thesupport arms brake segment carrier 13, can respectively be made of any suitable materials, such as light metal alloys known in the art. Therotor brake disks 2 are fabricated of a ceramic material. Thus, the alternating braking contact between the sintered metalbrake segment pads 14 and the ceramicrotor brake disks 2 provides the desired friction to achieve the required braking effect. - More particularly, the ceramic material of the
rotor brake disks 2 is a fiber-reinforced ceramic material, of which the reinforcement fibers are preferably homogeneously distributed in order to achieve uniform and homogeneous thermo-physical material characteristics. Such a fiber-reinforced ceramic is especially advantageous in that it withstands, transmits, and thereby reduces the internal stresses that arise during the braking process within therotor brake disks 2. Such a fiber-reinforced ceramic material also provides a good thermal conductivity through the cross-section of therotor brake disk 2, which allows the frictional heat during the braking process to be dissipated effectively. - According to particular advantageous embodiments, the rotor brake disks may be made of a C/SiC, C/SiSiC, SiC/Sic, SiC/SiSiC or other ceramic comprising an oxide ceramic system. Such an oxide system ceramic may comprise Nextel (TM) fibers on the basis of aluminum dioxide with an oxide matrix, for example mullite, or in combination with a carbide matrix such as SiC. The ceramic material of the
rotor brake disk 2 preferably comprises a combination of approximately 75 to 40 vol. % of short carbon fibers, approximately 40 to 70 vol. % of silicon carbide, and a maximum of 15 vol. % of silicon. In this context, the term “approximately” designates a range of ±1 vol. %, for example. Also, the term “short fibers” has its ordinary art-recognized meaning, based on the aspect ratio or length of the fibers. - In each of these embodiments, it is important that the ceramic raw material substances are mixed as homogeneously as possible to form the
rotor brake disks 2. A homogenous distribution of carbon fibers can be achieved by carrying out a pressing process to form the brake disk, with a preferred orientation of the carbon fibers in the plane of the brake disk. In such a process, only relatively few large pores, which would form initiation sites for the cumulation of free silicon, will arise. On the other hand, fine pores will be homogeneously distributed, whereby these fine pores become significant for silicon melt infiltration during the fabrication of the brake disk. In this context, the molten liquid silicon reacts with the matrix carbon while thereby forming a rather large proportion of silicon carbide, which is advantageous for achieving a high thermal conductivity in the direction perpendicular to the major planes of the brake disk. - It should be further understood that any conventionally known I- brake pad or brake lining materials, for example materials conventionally used in the brake pads of rail vehicles and motor vehicles, may alternatively be used for the
brake segment pads 14 of thestator brake disks 1 according to the invention. For as example, a person of ordinary skill in the art will readily be able to select a suitable material among available organic-based pad materials or metal/carbon composite pad materials. - Another optional but advantageous detail is to provide hollow spaces or venting passages within the
stator brake disks 1 or the rotor disks, in order to provide an air-cooling effect to improve the dissipation of the frictionally generated heat during braking. Such hollow chambers or air vent passages can be provided in any configuration or any manner known in the prior art relevant to brake arrangements. - The inventive arrangement allows a very simple, quick and economical replacement or exchange of the
brake segments 7. Using appropriate tools, thepivotable locking members 8 are simply opened by turning the latching bars 81 by 90° so that they do not bear on and secure thebrake segment carriers 13. Then, the respective releasedbrake segment 7 is simply pulled essentially radially away from thewheel axis 3, whereby it may be additionally necessary or advantageous to depress the spring-biasedcatch 12 in order to release thecatch 12 from the corresponding recess 16 in thebrake segment carrier 13. Then, anew brake segment 7 is simply placed into the now-vacant support space 10, whereby the spring-biasedcatch 12 engages into the corresponding recess 16 of thenew brake segment 7. Thereafter, the latching bars 81 are simply turned by 90° to be aligned in a circumferential direction and thereby securely lock thebrake segments 7 into place. Due to the simple access and removal and replacement of thebrake segments 7 in this manner, it is very simple to carry out the brake segment exchange without needing to disassemble the other remaining components of the brake arrangement. - Although the invention has been described with reference to specific example embodiments, it will be appreciated that it is intended to cover all modifications and equivalents within the scope of the appended claims. It should also be understood that the present disclosure includes all possible combinations of any individual features recited in any of the appended claims.
Claims (24)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10000915 | 2000-01-12 | ||
DE10000915.8 | 2000-01-12 | ||
DE10000915A DE10000915C2 (en) | 2000-01-12 | 2000-01-12 | Braking device for a vehicle |
Publications (2)
Publication Number | Publication Date |
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US20010007296A1 true US20010007296A1 (en) | 2001-07-12 |
US6439353B2 US6439353B2 (en) | 2002-08-27 |
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US09/760,158 Expired - Fee Related US6439353B2 (en) | 2000-01-12 | 2001-01-11 | Aircraft wheel brake with exchangeable brake segments |
Country Status (5)
Country | Link |
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US (1) | US6439353B2 (en) |
EP (1) | EP1116898B1 (en) |
AT (1) | ATE314588T1 (en) |
DE (2) | DE10000915C2 (en) |
ES (1) | ES2254105T3 (en) |
Cited By (4)
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US20050276961A1 (en) * | 2003-08-04 | 2005-12-15 | Sherwood Walter J | Materials and methods for making ceramic matrix composites |
US20090032344A1 (en) * | 2006-03-23 | 2009-02-05 | Qinetiq Limited | Liquid-Cooled Disc Brakes |
CN104321252A (en) * | 2012-05-21 | 2015-01-28 | 梅西耶道蒂有限公司 | Aircraft brake assembly |
US20170102043A1 (en) * | 2015-10-07 | 2017-04-13 | Goodrich Corporation | Composite brake disks with an integrated heat sink, methods for manufacturing the same, and methods for producing encapsulated heat sink material |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
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DE10000915C2 (en) * | 2000-01-12 | 2002-11-07 | Daimler Chrysler Ag | Braking device for a vehicle |
DE10131769C5 (en) * | 2001-06-30 | 2010-02-18 | Audi Ag | Brake system with composite brake disc |
US6820884B2 (en) | 2001-08-29 | 2004-11-23 | Meritor Heavy Vehicle Braking Systems | Integrated axle adaptor and spring seat for a vehicle suspension system |
US20030042082A1 (en) * | 2001-08-29 | 2003-03-06 | Mccann Denis John | Vehicle axle assembly having a brake carrier secured directly to the axle |
DE10142806B4 (en) | 2001-08-31 | 2005-02-10 | Audi Ag | brake disc |
US20060260886A1 (en) * | 2004-02-05 | 2006-11-23 | Erlston Lester J | Coaxial helical brake and method of braking in lightweight brake configuration |
US7159698B2 (en) | 2004-07-22 | 2007-01-09 | Bendix Spicer Foundation Brake, Llc | Disc brake rotor assembly with replaceable wear surfaces |
US20060046081A1 (en) * | 2004-08-26 | 2006-03-02 | Edward Williams | Laminated wear-resistant assemblies |
US10724591B2 (en) | 2017-11-27 | 2020-07-28 | Goodrich Corporation | Brake assembly with disks of variable thickness and methods for disk reuse |
US10941823B2 (en) | 2017-11-27 | 2021-03-09 | Goodrich Corporation | Segmented wear liner |
US11209059B2 (en) | 2019-03-13 | 2021-12-28 | Goodrich Corporation | Segmented integrated slot wear liner with structural carbon or ceramic core |
US10948037B2 (en) | 2019-03-28 | 2021-03-16 | Goodrich Corporation | Segmented rivetless wear liner with structural carbon or ceramic core |
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US2683504A (en) * | 1950-03-01 | 1954-07-13 | Bendix Aviat Corp | Brake assembly |
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US3731776A (en) * | 1970-03-19 | 1973-05-08 | Fort Dunlop | Friction mechanisms |
US3807534A (en) * | 1972-06-16 | 1974-04-30 | Bendix Corp | Friction disc |
US4119179A (en) * | 1976-06-18 | 1978-10-10 | Messier-Hispano | Brake disc structure |
US4860865A (en) * | 1987-09-10 | 1989-08-29 | The Montalvo Corporation | Quick release, high torque, friction brakes and clutches |
US4763762A (en) * | 1987-11-10 | 1988-08-16 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Preloaded brake disc |
FR2675450B1 (en) * | 1991-04-19 | 1993-08-06 | Aerospatiale | MULTIPLE DISC BRAKING DEVICE. |
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DE29710533U1 (en) * | 1996-07-22 | 1997-12-04 | Knorr-Bremse Systeme für Schienenfahrzeuge GmbH, 80809 München | Brake disc |
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DE19752777C2 (en) * | 1997-11-28 | 1999-12-09 | Daimler Chrysler Ag | Process for the production of an Al¶2¶O¶3¶ / titanium aluminide composite body and use of the process for the production of tribologically stressed system components |
DE10000915C2 (en) * | 2000-01-12 | 2002-11-07 | Daimler Chrysler Ag | Braking device for a vehicle |
-
2000
- 2000-01-12 DE DE10000915A patent/DE10000915C2/en not_active Expired - Fee Related
- 2000-12-23 AT AT00128466T patent/ATE314588T1/en not_active IP Right Cessation
- 2000-12-23 DE DE50011969T patent/DE50011969D1/en not_active Expired - Lifetime
- 2000-12-23 EP EP00128466A patent/EP1116898B1/en not_active Expired - Lifetime
- 2000-12-23 ES ES00128466T patent/ES2254105T3/en not_active Expired - Lifetime
-
2001
- 2001-01-11 US US09/760,158 patent/US6439353B2/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050276961A1 (en) * | 2003-08-04 | 2005-12-15 | Sherwood Walter J | Materials and methods for making ceramic matrix composites |
US20090032344A1 (en) * | 2006-03-23 | 2009-02-05 | Qinetiq Limited | Liquid-Cooled Disc Brakes |
CN104321252A (en) * | 2012-05-21 | 2015-01-28 | 梅西耶道蒂有限公司 | Aircraft brake assembly |
US20170102043A1 (en) * | 2015-10-07 | 2017-04-13 | Goodrich Corporation | Composite brake disks with an integrated heat sink, methods for manufacturing the same, and methods for producing encapsulated heat sink material |
US10253832B2 (en) * | 2015-10-07 | 2019-04-09 | Goodrich Corporation | Composite brake disks with an integrated heat sink, methods for manufacturing the same, and methods for producing encapsulated heat sink material |
US10865841B2 (en) | 2015-10-07 | 2020-12-15 | Raytheon Technologies Corporation | Composite brake disks with an integrated heat sink, methods for manufacturing the same, and methods for producing encapsulated heat sink material |
Also Published As
Publication number | Publication date |
---|---|
EP1116898B1 (en) | 2005-12-28 |
DE10000915A1 (en) | 2001-07-26 |
ATE314588T1 (en) | 2006-01-15 |
DE50011969D1 (en) | 2006-02-02 |
ES2254105T3 (en) | 2006-06-16 |
DE10000915C2 (en) | 2002-11-07 |
US6439353B2 (en) | 2002-08-27 |
EP1116898A2 (en) | 2001-07-18 |
EP1116898A3 (en) | 2003-09-24 |
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