WO2009082397A1 - Wheel and brake assembly with torque bar - Google Patents

Wheel and brake assembly with torque bar Download PDF

Info

Publication number
WO2009082397A1
WO2009082397A1 PCT/US2007/088596 US2007088596W WO2009082397A1 WO 2009082397 A1 WO2009082397 A1 WO 2009082397A1 US 2007088596 W US2007088596 W US 2007088596W WO 2009082397 A1 WO2009082397 A1 WO 2009082397A1
Authority
WO
WIPO (PCT)
Prior art keywords
wheel
torque bar
spacer block
torque
set forth
Prior art date
Application number
PCT/US2007/088596
Other languages
French (fr)
Inventor
Jerry L. Miller
Joshua C. Houser
Original Assignee
Goodrich Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Goodrich Corporation filed Critical Goodrich Corporation
Priority to PCT/US2007/088596 priority Critical patent/WO2009082397A1/en
Publication of WO2009082397A1 publication Critical patent/WO2009082397A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D55/00Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes
    • F16D55/24Brakes 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
    • F16D55/26Brakes 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
    • F16D55/36Brakes with a plurality of rotating discs all lying side by side
    • F16D55/40Brakes with a plurality of rotating discs all lying side by side actuated by a fluid-pressure device arranged in or one the brake
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42Arrangement or adaptation of brakes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D65/00Parts or details
    • F16D65/78Features relating to cooling
    • F16D2065/785Heat insulation or reflection

Definitions

  • the present invention relates generally to aircraft wheel and brake assemblies. More particularly, the invention relates to torque transmitting drive bars fastened to the radially inner surface of a wheel well of an aircraft wheel for engagement with brake rotors.
  • Torque bars also known as torque transmitting drive lugs, are employed in aircraft wheel and brake assemblies to couple the wheels to the rotors of the brake assembly.
  • the torque bars typically extend parallel to the wheel axis and have an outboard end inserted in an aperture formed in the web of the wheel and an inboard end attached to a radially inner side of the wheel at the inboard end of the wheel.
  • the central portion of the torque bar is radially spaced from the well of the wheel, and usually a heat shield is located in this space.
  • Torque bars of the type just described are susceptible to vibration which can result in excessive torque bar deflection both radially and tangentially relative to the wheel.
  • a common practice was to use relatively heavy torque bars to provide the necessary strength and resistance to deflection. This undesirably increases the weight of the wheel and brake assembly, which is particularly undesirable in aircraft.
  • the present invention provides a method and device for supporting one or more of the torque bars used in a wheel and brake assembly to improve the dynamic stability of the torque bars with at most only a minor thermal penalty.
  • the supported torque bar reduces or substantially eliminates excessive vibration-induced deflections.
  • the torque-bar is supported by a spacer block interposed between the wheel and torque bar at a mid-span location along the torque bar.
  • the spacer block which preferably is made of an insulating material that may have some resilient compressibility, and can be compressed between the torque bar and wheel well. This provides effective resistance to radial vibration while mechanical interference between the spacer block and both the torque bar and wheel well resists tangential deflection of the torque bar during braking.
  • the method and device of the present invention can easily be applied to retrofit existing wheel and brake assemblies to improve the operating characteristics of the torque bars and/or allow for the use of lighter and/or smaller torque bars.
  • a wheel and brake assembly comprises a wheel including a wheel well, the wheel well being generally cylindrical and coaxial with a rotational axis of the wheel, a torque bar connected to the wheel, and a spacer block interposed between the wheel well and the torque bar in a manner that preloads the torque bar.
  • the spacer block is secured to the torque bar and the wheel against movement in at least one direction.
  • the spacer block can be secured to the torque bar and the wheel so as to restrict relative movement between the spacer block and the torque bar and wheel.
  • the spacer block has an uncompressed thickness greater than the spacing between a radially inner surface of the wheel well and the torque bar when the spacer block is not installed therebetween.
  • the torque bar includes a recess for receiving the spacer block for securing the spacer block against movement relative to the torque bar in at least one direction. A radially outer portion of the spacer block is received in a recess in the wheel.
  • the torque bar is connected to the wheel in at least two axially spaced apart support locations, and the spacer block is interposed between the radially inner surface of the wheel well and the torque bar at a location between the at least two support locations.
  • the spacer block can have a surface having a shape corresponding to the shape of a portion of the radially inner surface of the wheel well, and can be secured to the torque bar against movement along or transverse to the torque bar.
  • the spacer block can be compressed between a radially inner surface of the wheel well and the torque bar.
  • the torque bar can be connected to the wheel with at least one bolt, and a heat shield can be provided between the spacer block and the torque bar.
  • the spacer block can be made of a material having a low thermal conductivity.
  • a method of installing a torque bar in a wheel assembly the wheel assembly including a generally cylindrical wheel well coaxial with a rotational axis of the wheel, the method comprises interposing a spacer block between a radially inner surface of the wheel well and the torque bar, and securing the torque bar to the wheel in a manner that pre-loads the torque bar against the spacer block.
  • the spacer block is secured to the torque bar and the wheel against movement in at least one direction.
  • FIG. 1 is a cross- sect ion a I view of a wheel and brake assembly.
  • FIG. 2 is an enlarged portion of the cross-sectional view of the wheel and brake assembly of FIG. 1.
  • FIG. 3 is an arcuate portion of a front/inboard end view of the wheel and brake assembly of FIG. 1 , looking into the wheel from the left side of FIG. 1.
  • FIG. 4A is a perspective view of a torque bar used in the wheel and brake assembly of FIG. 1.
  • FIG. 4B is a top view of the torque bar.
  • FIG. 4C is a longitudinal cross-sectional view of the torque bar taken along the line 4C-4C of FIG. 4B.
  • FIG. 4D is a bottom view of the torque bar looking from the line 4D-4D of FIG. 4C.
  • FIG. 4E is an enlarged transverse cross-sectional view of the torque bar taken along the line 4E-4E of FIG. 4B.
  • FIG. 4F is an end view of the torque bar as viewed from the line 4F-4F of FIG. 4B.
  • FIG. 5A is a top view of a heat shield carrier used in the wheel and brake assembly of FIG. 1.
  • FIG. 5B is a side elevational view of the heat shield carrier of FIG. 5A looking from the line 5B-5B of FIG. 5A.
  • FIG. 5C is a bottom view of the heat shield carrier looking from the line 5C-5C of FIG. 5B.
  • FIG. 6 is a partial cross-sectional view of one half of an aircraft wheel and brake assembly in accordance with the present invention.
  • FIG. 7 is an exploded schematic illustration of a torque bar assembly in accordance with an exemplary embodiment of the present invention.
  • FIG. 8 is a cross-sectional view of the torque bar assembly of FIG. 7.
  • FIG. 9 is a cross-sectional view of a torque bar assembly in accordance with another exemplary embodiment of the present invention.
  • FIGS. 1-5 an exemplary wheel and brake assembly is indicated generally by reference numeral 10.
  • the wheel and brake assembly shown in FIGS. 1-5C is fully described in commonly assigned U.S. Patent No. 7,051 ,845 which is hereby incorporated herein by reference in its entirety.
  • the aircraft wheel and brake assembly 10 is shown mounted on an aircraft bogie axle 12.
  • the wheel and brake assembly 10 comprises a wheel 14 (only the inboard half of the wheel is shown in FIG. 1 ) having a hub 16 and a wheel well 18 concentric with the hub 16, and a web 20 interconnecting the hub 16 and the wheel well 18.
  • a torque take-out assembly 22 is aligned with the hub 16, and the wheel 14 is rotatable relative to the torque take-out assembly 22.
  • a plurality of torque bars 24 are fixed to the wheel 14 generally parallel to the axis of rotation 26 (see Fig. 1 ) of the wheel and spaced from the wheel well 18.
  • a heat sink 28 is disposed within the wheel 14, and comprises brake or friction disks in the form of rotors 32 and stators 34.
  • the rotors 32 are engaged with the torque bars 24 for rotation with the wheel, and the stators 34 are engaged with the torque take-out assembly 22 which is fixed against rotation relative to a landing gear strut (not shown).
  • a pressure plate 36 and an end plate 38 may be positioned at opposite ends of the heat sink 28 and retained against rotation with respect to the torque take-out assembly 22.
  • the friction disks may be formed from any material suitable for friction disks, including metals, such as steel with a sintered metallic friction lining, and ceramics or carbon materials, such as a carbon/carbon material.
  • the heat sink 28 is a carbon/carbon composite heat sink having at least one carbon/carbon rotor 32 interleaved with a plurality of carbon/carbon stators 34.
  • At least one actuator 30 (FIGS. 1 and 2) is provided to compress the heat sink 28.
  • the actuator 30 is a hydraulically actuated piston, but other types of actuators may be used in the practice of the invention, such as electromechanical actuators.
  • a heat shield 40 is attached to the wheel 14 between the wheel well 18 and the heat sink 28. As illustrated in FIGS. 1 and 3, the heat shield 40 is concentric with the wheel well 18 and has a plurality of heat shield sections 42 disposed between respective, relatively adjacent pairs of torque bars 24. The heat shield sections are spaced from the wheel well 18 and secured in place by respective pairs of heat shield carriers 44 that are fixed to the wheel 14 generally parallel to the axis of rotation 26 of the wheel 14 intermediate the torque bars 24 and the wheel well 18.
  • the carriers are preferably aligned with respective torque bars, and have "groove-like" side edges that define edge channels for axially receiving and radially constraining side edge tap portions of the heat shield sections 42, as described below with greater particularity.
  • the torque bars 24 and heat shield carriers 44 are attached at their axially inboard end to the wheel 14 by torque bar bolts 48.
  • the torque bar bolts 48 extend through respective holes in a flange provided on the wheel as shown, which flange for purposes of the present description is intended to be considered as part of the wheel well.
  • Each torque bar 24 preferably has a pin 50 at its axially outboard end (i.e., the end opposite the torque bar bolts 48) that is received within a hole 52 in the web 20 of the wheel.
  • the heat shield sections 42 may be secured in place and to the wheel well 18 by suitable means, such as fasteners, and more particularly heat shield bolts 54 (FIGS. 1 and 3). Other securement devices may be employed.
  • Each torque bar 24 is substantially rectangular-shaped in cross-section (FIG. 4F) and has a mounting hole 57 at its axially inboard end that receives the torque bar bolt 48.
  • Each torque bar 24 also includes a coupling device in the form of a button 58 for coupling the heat shield carrier 44 to the torque bar 24 in the below described manner.
  • the button 58 also serves to secure a spacer block against axial and circumferential movement relative to the torque bar 24.
  • the illustrated button 58 is T-shaped in cross section and includes a stem portion 59 which extends radially outward from the body of the torque bar 24 to an enlarged, circular- shaped head portion 61.
  • the button 58 is located axially outwardly from the inboard end of the torque bar 24 and preferably is located between the inboard and outboard ends of the torque bar 24.
  • the button 58 is located along the neutral axis of bending of the torque bar 24 (i.e., the axial line located midway along the circumferential span of the torque bar 24). In the illustrated example, the T-shaped button 58 is located about midway between the inboard end and outboard end of the wheel well 18.
  • FIGS. 5A-5C the heat shield carrier is shown in detail.
  • a mounting hole 68 that receives the torque bar bolt 48 is provided in a mounting portion 104 of the heat shield carrier 44.
  • the mounting portion 104 is sandwiched between the torque bar 24 and the insulating spacer 96 which spaces the carrier 44 and torque bar 24 from the wheel 14 at the attachment location.
  • the heat shield carrier is provided with an aperture and more particularly a keyhole 110 for receiving and coupling with the button 58 of the torque bar 24.
  • the keyhole 110 is thus located axially between the inboard end and outboard end of the wheel well 18.
  • the keyhole 110 has a combined geometry of an axially extending slot 116 at its axially outboard end and a round hole 118 at the inboard end of the keyhole 110.
  • the slot 116 has a width about equal to the stem 59 of the button 58 and less than the head 61 of the button 58, and the hole 118 has a diameter larger than the diameter of the head 61 of the button 58 for allowing passage therethrough of the head 61 of the button 58.
  • each torque bar 24 has associated therewith a pre-load device that functions to pre-stress the torque bar 24.
  • the pre-load device is a mid-span spacer block 150 that is interposed between a radially inner surface 155 of wheel well 18 and the torque bar 24 about midway between the ends of the torque bar 24 that are connected to the wheel.
  • the spacer block 150 preferably is made of an insulating material that when not radially compressed, has a thickness greater than the distance between the torque bar 24 and the wheel well 18 when the spacer block 150 is not interposed between the tube well 18 and the torque bar 24, i.e., when the torque bar 24 is not preloaded.
  • the spacer block 150 when the spacer block 150 is installed between the torque bar 24 and the wheel well 18, the spacer block 150 will be compressed and will pre-load the torque bar 24.
  • This pre-loading or pre-stressing of the torque bars 24 reduces deflections of the torque bars 24 both radially and tangentially during braking.
  • the amount of pre-load may be varied by varying the radial thickness of the spacer block 150, for example.
  • the spacer block 150 is provided with a retention feature in the form of a recess 158.
  • the recess 158 is provided in the radially inner surface of the spacer block 150 for capturing a protrusion on the torque bar, such as the button 58 on the torque bar 24.
  • the button 58 cooperates with the recess 158 to restrict axial or circumferential movement of the spacer block 150 while the wheel well 18 and torque bar 24 capture the spacer block 150 in a radial direction.
  • the upper surface of the spacer block 150 preferably is frictionally engaged with the radially inner surface 155 of the wheel well 18.
  • the spacer block 150 may be installed between the torque bar 24 and the wheel well 18 before the torque bar bolt 48 has been tightened down against the torque bar 24. As the torque bar bolt 48 is tightened to draw the end of the torque bar 24 to the wheel well 18, the spacer block 150 will be compressed by the torque bar 24 thereby applying a pre-load to the torque bar 24.
  • the torque bar 24 may resiliency flex radially inwardly to accommodate the spacer block 150 as the torque bar bolt 48 is tightened. As above mentioned, the amount of pre-load on the torque bar 24 can be altered by adjusting the radial dimension of the spacer block 150.
  • the radially outer surface 160 of the spacer block 150 preferably is curved or otherwise shaped to conform to the radially inner surface 155 of the wheel well 18. Frictional engagement and/or mechanical interference between the spacer block 150 and both the wheel well 18 and torque bar 24 in the tangential direction resists deflection of the torque bar 24 midway between the ends of the torque bar 24. Of particular note, however, is that in this embodiment such resistance to deflection, radially and/or tangentially, may be effected without fasteners piercing the torque bar 24 and/or wheel well 18 at a location between the ends of the torque bar 24 that are attached to the wheel 14.
  • the torque bar 24 may flex thereby causing movement of the spacer block 150 relative to the wheel well 18. Frictional and pre-load forces between the block 150 and the radially inner surface 155 of the wheel well 18 generally oppose such movement thereby acting to damp the flexing of the torque bar 24.
  • the spacer block 150 preferably is made of an insulating material, i.e., a material having a relatively low thermal conductivity and relatively low compressive stiffness as compared to the torque bar 24.
  • the insulating material may be the same type of insulating material heretofore used in wheel and brake assemblies, such as the material used to form the insulating spacer 96.
  • the spacer block 150 opposes and/or restricts radially outward flexing of the torque bar 24, while the preload on the torque bar 24 opposes and/or restricts radially inward flexing of the torque bar 24.
  • Frictional forces between the spacer block 150 and the radially inner surface 155 of the wheel well 18 resist and/or clamp circumferential flexing of the torque bar 24.
  • the pre-loaded torque bar 24 can resist flexure under a wider range of dynamic vibrations thus making the wheel and brake assembly 10 more stable than a similar wheel and brake assembly without a pre-loaded torque bar 24.
  • all of the torque bars can be provided with a spacer block.
  • spacer blocks may be desirable to install spacer blocks with less than all of the torque bars.
  • spacer blocks may be suitable to install spacer blocks with two- thirds, or even one-third, of the torque bars.
  • the spacer block 150 can be easily used in combination with a heat shield. As shown in FIGS. 7 and 8, a heat shield 40, specifically the heat shield carrier 44, can be sandwiched between the spacer block 150 and the torque bar 24. In other embodiments, the heat shield may be provided with an aperture for accommodating the spacer block 150.
  • a wear surface may also be provided on the radially inner surface 155 of the wheel well 18. It will be understood that the spacer block 150 functions to create an interference against which the torque bar 24 can be pre-loaded. Therefore, and as desired or necessary, other elements between the torque bar 24 and the wheel well 18 can be utilized to create the interference.
  • the spacer block 150 can be formed as part of the torque bar 24 and suitable insulating material can be interposed between the wheel well 18 and the spacer block 150 on the torque bar 24 to limit thermal conduction between the torque bar 24 and the wheel well 18.
  • the spacer block 150 can be used with existing wheel and brake assemblies generally without modification to the assembly.
  • the present invention provides a way to retrofit existing wheel and brake assemblies with a spacer block 150 to support and pre-load the torque bar 24. This capability can be useful in situations were the unanticipated dynamic instability of a wheel and brake assembly otherwise renders the assembly unfit for use.
  • the wheel and brake assembly 10 may be disassembled to replace such components without disassembling the entire wheel assembly 10.
  • one or more damaged heat shield sections 40 may be replaced by removing the heat shield bolts 54 for those sections, axially withdrawing the damaged sections, inserting new sections, and replacing the heat shield bolts 54. This may be accomplished without removing the torque bar 24 and spacer block 150, thus greatly facilitating field repair of the wheel and brake assembly.
  • FIG. 9 another exemplary torque bar assembly in accordance with the invention is illustrated.
  • a radially outer portion of the spacer block 150 is retained in a recess 170 formed in the wheel 14.
  • the recess 170 is formed by a pair of circumferentially-spaced apart shoulders 174 that extend radially inwardly from the inner surface 155 of the wheel 14.
  • the shoulders 174 can be part of a boss on the inner surface 155 of the wheel 14 (e.g., a thickened portion of the wheel 14).
  • the shoulders 174 restrict circumferential movement of the spacer block 150.
  • a radially inner portion of the spacer block 150 is retained in a recess 178 in the torque bar 24, which in the illustrated embodiment is formed by flanges 182 of the torque bar 24.
  • the spacer block 150 in FIG. 9 is restrained in recesses 170 and 178 thereby restricting relative movement between the wheel 14 and the torque bar 24.
  • the spacer block 150 is compressed by the torque bar 24 thereby applying a preload to the torque bar 24.
  • the torque bar 24 may resiliently flex radially inwardly to accommodate the spacer block 150.
  • the amount of pre-load on the torque bar 24 can be altered by adjusting the radial dimension of the spacer block 150.
  • the torque bar may or may not be prestressed in this embodiment, depending on the specific application. In some applications, a clearance may be provided between the spacer block 150 and the inner surface 155 of the wheel such the spacer block 150 can move radially an amount without causing undue stress on the wheel 14.
  • the spacer block 150 opposes and/or restricts radially outward flexing of the torque bar 24, while the pre-load on the torque bar 24 opposes and/or restricts radially inward flexing of the torque bar 24.
  • Shoulders 174 and flanges 182 captivate the spacer block 150 so as to resist circumferential flexing of the torque bar 24.
  • the pre-loaded torque bar 24 can resist flexure under a wider range of dynamic vibrations thus making the wheel and brake assembly 10 more stable than a similar wheel and brake assembly without a pre-loaded torque bar 24.
  • the invention has been shown and described in the context of a torque bar 24 that is secured to a wheel and brake assembly by inserting a pin portion of a first end of the torque bar into a hole in the wheel and bolting the opposite end to the wheel, the invention can be used in connection with a wide variety of wheel and brake assemblies.
  • the invention can be used in a wheel and brake assembly wherein a torque bar is secured to the wheel at each end by bolts.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)

Abstract

Α method and. device for supporting a torque bar (24) at a mid-span location in a wheel and 'brake assembly. 'A spacer block (150) interposed between the wheel well (18) and the torque bar generally restricts relative motion between the wheel well and the torque bar. The torque bar can be pre-loaded against spacer block.

Description

WHEEL AND BRAKE ASSEMBLY WITH TORQUE BAR
Field of the Invention
The present invention relates generally to aircraft wheel and brake assemblies. More particularly, the invention relates to torque transmitting drive bars fastened to the radially inner surface of a wheel well of an aircraft wheel for engagement with brake rotors.
Background of the Invention Torque bars, also known as torque transmitting drive lugs, are employed in aircraft wheel and brake assemblies to couple the wheels to the rotors of the brake assembly. The torque bars typically extend parallel to the wheel axis and have an outboard end inserted in an aperture formed in the web of the wheel and an inboard end attached to a radially inner side of the wheel at the inboard end of the wheel. To minimize thermal conduction from the brake assembly to the wheel rim, the central portion of the torque bar is radially spaced from the well of the wheel, and usually a heat shield is located in this space.
Torque bars of the type just described are susceptible to vibration which can result in excessive torque bar deflection both radially and tangentially relative to the wheel. To overcome deflection problems, a common practice was to use relatively heavy torque bars to provide the necessary strength and resistance to deflection. This undesirably increases the weight of the wheel and brake assembly, which is particularly undesirable in aircraft.
Summary of the Invention
The present invention provides a method and device for supporting one or more of the torque bars used in a wheel and brake assembly to improve the dynamic stability of the torque bars with at most only a minor thermal penalty. The supported torque bar reduces or substantially eliminates excessive vibration-induced deflections. In a preferred embodiment, the torque-bar is supported by a spacer block interposed between the wheel and torque bar at a mid-span location along the torque bar. The spacer block, which preferably is made of an insulating material that may have some resilient compressibility, and can be compressed between the torque bar and wheel well. This provides effective resistance to radial vibration while mechanical interference between the spacer block and both the torque bar and wheel well resists tangential deflection of the torque bar during braking. As will be appreciated, the method and device of the present invention can easily be applied to retrofit existing wheel and brake assemblies to improve the operating characteristics of the torque bars and/or allow for the use of lighter and/or smaller torque bars.
In accordance with one aspect of the invention, a wheel and brake assembly comprises a wheel including a wheel well, the wheel well being generally cylindrical and coaxial with a rotational axis of the wheel, a torque bar connected to the wheel, and a spacer block interposed between the wheel well and the torque bar in a manner that preloads the torque bar. The spacer block is secured to the torque bar and the wheel against movement in at least one direction.
In accordance with another aspect of the invention, a torque bar assembly for use in an aircraft wheel comprises a torque bar and a spacer block. The spacer block can be secured to the torque bar and the wheel so as to restrict relative movement between the spacer block and the torque bar and wheel.
In one embodiment, the spacer block has an uncompressed thickness greater than the spacing between a radially inner surface of the wheel well and the torque bar when the spacer block is not installed therebetween. The torque bar includes a recess for receiving the spacer block for securing the spacer block against movement relative to the torque bar in at least one direction. A radially outer portion of the spacer block is received in a recess in the wheel. The torque bar is connected to the wheel in at least two axially spaced apart support locations, and the spacer block is interposed between the radially inner surface of the wheel well and the torque bar at a location between the at least two support locations.
The spacer block can have a surface having a shape corresponding to the shape of a portion of the radially inner surface of the wheel well, and can be secured to the torque bar against movement along or transverse to the torque bar. The spacer block can be compressed between a radially inner surface of the wheel well and the torque bar. The torque bar can be connected to the wheel with at least one bolt, and a heat shield can be provided between the spacer block and the torque bar. The spacer block can be made of a material having a low thermal conductivity.
According to still another aspect of the invention, a method of installing a torque bar in a wheel assembly, the wheel assembly including a generally cylindrical wheel well coaxial with a rotational axis of the wheel, the method comprises interposing a spacer block between a radially inner surface of the wheel well and the torque bar, and securing the torque bar to the wheel in a manner that pre-loads the torque bar against the spacer block. The spacer block is secured to the torque bar and the wheel against movement in at least one direction. Further features of the invention will become apparent from the following detailed description when considered in conjunction with the drawings.
Brief Description of the Drawings
FIG. 1 is a cross- sect ion a I view of a wheel and brake assembly. FIG. 2 is an enlarged portion of the cross-sectional view of the wheel and brake assembly of FIG. 1.
FIG. 3 is an arcuate portion of a front/inboard end view of the wheel and brake assembly of FIG. 1 , looking into the wheel from the left side of FIG. 1.
FIG. 4A is a perspective view of a torque bar used in the wheel and brake assembly of FIG. 1. FIG. 4B is a top view of the torque bar.
FIG. 4C is a longitudinal cross-sectional view of the torque bar taken along the line 4C-4C of FIG. 4B.
FIG. 4D is a bottom view of the torque bar looking from the line 4D-4D of FIG. 4C. FIG. 4E is an enlarged transverse cross-sectional view of the torque bar taken along the line 4E-4E of FIG. 4B.
FIG. 4F is an end view of the torque bar as viewed from the line 4F-4F of FIG. 4B.
FIG. 5A is a top view of a heat shield carrier used in the wheel and brake assembly of FIG. 1.
FIG. 5B is a side elevational view of the heat shield carrier of FIG. 5A looking from the line 5B-5B of FIG. 5A.
FIG. 5C is a bottom view of the heat shield carrier looking from the line 5C-5C of FIG. 5B. FIG. 6 is a partial cross-sectional view of one half of an aircraft wheel and brake assembly in accordance with the present invention.
FIG. 7 is an exploded schematic illustration of a torque bar assembly in accordance with an exemplary embodiment of the present invention.
FIG. 8 is a cross-sectional view of the torque bar assembly of FIG. 7. FIG. 9 is a cross-sectional view of a torque bar assembly in accordance with another exemplary embodiment of the present invention. Detailed Description
Referring now to the drawings in detail and initially to FIGS. 1-5, an exemplary wheel and brake assembly is indicated generally by reference numeral 10. The wheel and brake assembly shown in FIGS. 1-5C is fully described in commonly assigned U.S. Patent No. 7,051 ,845 which is hereby incorporated herein by reference in its entirety.
In FIG. 1 , the aircraft wheel and brake assembly 10 is shown mounted on an aircraft bogie axle 12. The wheel and brake assembly 10 comprises a wheel 14 (only the inboard half of the wheel is shown in FIG. 1 ) having a hub 16 and a wheel well 18 concentric with the hub 16, and a web 20 interconnecting the hub 16 and the wheel well 18. A torque take-out assembly 22 is aligned with the hub 16, and the wheel 14 is rotatable relative to the torque take-out assembly 22.
As shown in FIG. 2, a plurality of torque bars 24 are fixed to the wheel 14 generally parallel to the axis of rotation 26 (see Fig. 1 ) of the wheel and spaced from the wheel well 18. A heat sink 28 is disposed within the wheel 14, and comprises brake or friction disks in the form of rotors 32 and stators 34. The rotors 32 are engaged with the torque bars 24 for rotation with the wheel, and the stators 34 are engaged with the torque take-out assembly 22 which is fixed against rotation relative to a landing gear strut (not shown). A pressure plate 36 and an end plate 38 may be positioned at opposite ends of the heat sink 28 and retained against rotation with respect to the torque take-out assembly 22. The friction disks may be formed from any material suitable for friction disks, including metals, such as steel with a sintered metallic friction lining, and ceramics or carbon materials, such as a carbon/carbon material. According to a preferred embodiment, the heat sink 28 is a carbon/carbon composite heat sink having at least one carbon/carbon rotor 32 interleaved with a plurality of carbon/carbon stators 34.
At least one actuator 30 (FIGS. 1 and 2) is provided to compress the heat sink 28. In the example presented, the actuator 30 is a hydraulically actuated piston, but other types of actuators may be used in the practice of the invention, such as electromechanical actuators. A heat shield 40 is attached to the wheel 14 between the wheel well 18 and the heat sink 28. As illustrated in FIGS. 1 and 3, the heat shield 40 is concentric with the wheel well 18 and has a plurality of heat shield sections 42 disposed between respective, relatively adjacent pairs of torque bars 24. The heat shield sections are spaced from the wheel well 18 and secured in place by respective pairs of heat shield carriers 44 that are fixed to the wheel 14 generally parallel to the axis of rotation 26 of the wheel 14 intermediate the torque bars 24 and the wheel well 18. The carriers are preferably aligned with respective torque bars, and have "groove-like" side edges that define edge channels for axially receiving and radially constraining side edge tap portions of the heat shield sections 42, as described below with greater particularity.
The torque bars 24 and heat shield carriers 44 are attached at their axially inboard end to the wheel 14 by torque bar bolts 48. The torque bar bolts 48 extend through respective holes in a flange provided on the wheel as shown, which flange for purposes of the present description is intended to be considered as part of the wheel well. Each torque bar 24 preferably has a pin 50 at its axially outboard end (i.e., the end opposite the torque bar bolts 48) that is received within a hole 52 in the web 20 of the wheel.
After axial insertion between respective pairs of carriers 44, the heat shield sections 42 may be secured in place and to the wheel well 18 by suitable means, such as fasteners, and more particularly heat shield bolts 54 (FIGS. 1 and 3). Other securement devices may be employed.
In FIGS. 4A-4F, details of an exemplary torque bar 24 are shown. Each torque bar 24 is substantially rectangular-shaped in cross-section (FIG. 4F) and has a mounting hole 57 at its axially inboard end that receives the torque bar bolt 48.
Each torque bar 24 also includes a coupling device in the form of a button 58 for coupling the heat shield carrier 44 to the torque bar 24 in the below described manner. As will be further described herein the button 58 also serves to secure a spacer block against axial and circumferential movement relative to the torque bar 24. As best shown in FIGS. 4C and 4E, the illustrated button 58 is T-shaped in cross section and includes a stem portion 59 which extends radially outward from the body of the torque bar 24 to an enlarged, circular- shaped head portion 61. The button 58 is located axially outwardly from the inboard end of the torque bar 24 and preferably is located between the inboard and outboard ends of the torque bar 24. As is also preferred, the button 58 is located along the neutral axis of bending of the torque bar 24 (i.e., the axial line located midway along the circumferential span of the torque bar 24). In the illustrated example, the T-shaped button 58 is located about midway between the inboard end and outboard end of the wheel well 18.
In FIGS. 5A-5C, the heat shield carrier is shown in detail. A mounting hole 68 that receives the torque bar bolt 48 is provided in a mounting portion 104 of the heat shield carrier 44. As best seen in FIGS. 2 and 3, the mounting portion 104 is sandwiched between the torque bar 24 and the insulating spacer 96 which spaces the carrier 44 and torque bar 24 from the wheel 14 at the attachment location. The heat shield carrier is provided with an aperture and more particularly a keyhole 110 for receiving and coupling with the button 58 of the torque bar 24. The keyhole 110 is thus located axially between the inboard end and outboard end of the wheel well 18. The keyhole 110 has a combined geometry of an axially extending slot 116 at its axially outboard end and a round hole 118 at the inboard end of the keyhole 110. The slot 116 has a width about equal to the stem 59 of the button 58 and less than the head 61 of the button 58, and the hole 118 has a diameter larger than the diameter of the head 61 of the button 58 for allowing passage therethrough of the head 61 of the button 58.
Turning now to FIG. 6, and in accordance with the present invention, each torque bar 24 has associated therewith a pre-load device that functions to pre-stress the torque bar 24. In the illustrated embodiment, the pre-load device is a mid-span spacer block 150 that is interposed between a radially inner surface 155 of wheel well 18 and the torque bar 24 about midway between the ends of the torque bar 24 that are connected to the wheel. The spacer block 150 preferably is made of an insulating material that when not radially compressed, has a thickness greater than the distance between the torque bar 24 and the wheel well 18 when the spacer block 150 is not interposed between the tube well 18 and the torque bar 24, i.e., when the torque bar 24 is not preloaded. Consequently, when the spacer block 150 is installed between the torque bar 24 and the wheel well 18, the spacer block 150 will be compressed and will pre-load the torque bar 24. This pre-loading or pre-stressing of the torque bars 24 reduces deflections of the torque bars 24 both radially and tangentially during braking. The amount of pre-load may be varied by varying the radial thickness of the spacer block 150, for example.
In the illustrated embodiment, the spacer block 150 is provided with a retention feature in the form of a recess 158. The recess 158 is provided in the radially inner surface of the spacer block 150 for capturing a protrusion on the torque bar, such as the button 58 on the torque bar 24. The button 58 cooperates with the recess 158 to restrict axial or circumferential movement of the spacer block 150 while the wheel well 18 and torque bar 24 capture the spacer block 150 in a radial direction. The upper surface of the spacer block 150 preferably is frictionally engaged with the radially inner surface 155 of the wheel well 18. Those skilled in the art will appreciate that other devices may be used for securing the spacer block 150 in place between the torque bar 24 and wheel well 18, such as, for example, suitable adhesives, mechanical fasteners, etc., although less desired. The spacer block 150 may be installed between the torque bar 24 and the wheel well 18 before the torque bar bolt 48 has been tightened down against the torque bar 24. As the torque bar bolt 48 is tightened to draw the end of the torque bar 24 to the wheel well 18, the spacer block 150 will be compressed by the torque bar 24 thereby applying a pre-load to the torque bar 24. The torque bar 24 may resiliency flex radially inwardly to accommodate the spacer block 150 as the torque bar bolt 48 is tightened. As above mentioned, the amount of pre-load on the torque bar 24 can be altered by adjusting the radial dimension of the spacer block 150.
The radially outer surface 160 of the spacer block 150 preferably is curved or otherwise shaped to conform to the radially inner surface 155 of the wheel well 18. Frictional engagement and/or mechanical interference between the spacer block 150 and both the wheel well 18 and torque bar 24 in the tangential direction resists deflection of the torque bar 24 midway between the ends of the torque bar 24. Of particular note, however, is that in this embodiment such resistance to deflection, radially and/or tangentially, may be effected without fasteners piercing the torque bar 24 and/or wheel well 18 at a location between the ends of the torque bar 24 that are attached to the wheel 14.
During braking, the torque bar 24 may flex thereby causing movement of the spacer block 150 relative to the wheel well 18. Frictional and pre-load forces between the block 150 and the radially inner surface 155 of the wheel well 18 generally oppose such movement thereby acting to damp the flexing of the torque bar 24.
As above mentioned, the spacer block 150 preferably is made of an insulating material, i.e., a material having a relatively low thermal conductivity and relatively low compressive stiffness as compared to the torque bar 24. The insulating material may be the same type of insulating material heretofore used in wheel and brake assemblies, such as the material used to form the insulating spacer 96.
Once installed, the spacer block 150 opposes and/or restricts radially outward flexing of the torque bar 24, while the preload on the torque bar 24 opposes and/or restricts radially inward flexing of the torque bar 24. Frictional forces between the spacer block 150 and the radially inner surface 155 of the wheel well 18 resist and/or clamp circumferential flexing of the torque bar 24. The pre-loaded torque bar 24 can resist flexure under a wider range of dynamic vibrations thus making the wheel and brake assembly 10 more stable than a similar wheel and brake assembly without a pre-loaded torque bar 24.
It will be appreciated that for a given wheel and brake assembly, all of the torque bars can be provided with a spacer block. Alternatively, for a given application it may be desirable to install spacer blocks with less than all of the torque bars. For example, it may be suitable to install spacer blocks with two- thirds, or even one-third, of the torque bars.
The spacer block 150 can be easily used in combination with a heat shield. As shown in FIGS. 7 and 8, a heat shield 40, specifically the heat shield carrier 44, can be sandwiched between the spacer block 150 and the torque bar 24. In other embodiments, the heat shield may be provided with an aperture for accommodating the spacer block 150.
A wear surface may also be provided on the radially inner surface 155 of the wheel well 18. It will be understood that the spacer block 150 functions to create an interference against which the torque bar 24 can be pre-loaded. Therefore, and as desired or necessary, other elements between the torque bar 24 and the wheel well 18 can be utilized to create the interference.
In another embodiment, the spacer block 150 can be formed as part of the torque bar 24 and suitable insulating material can be interposed between the wheel well 18 and the spacer block 150 on the torque bar 24 to limit thermal conduction between the torque bar 24 and the wheel well 18.
The spacer block 150 can be used with existing wheel and brake assemblies generally without modification to the assembly. Thus, the present invention provides a way to retrofit existing wheel and brake assemblies with a spacer block 150 to support and pre-load the torque bar 24. This capability can be useful in situations were the unanticipated dynamic instability of a wheel and brake assembly otherwise renders the assembly unfit for use.
Similarly, should a spacer block 150, heat shield 40 or heat shield carrier 44, or other component be damaged such that replacement is needed before scheduled maintenance of the wheel and brake assembly 10, the wheel and brake assembly 10 may be disassembled to replace such components without disassembling the entire wheel assembly 10. For example, one or more damaged heat shield sections 40 may be replaced by removing the heat shield bolts 54 for those sections, axially withdrawing the damaged sections, inserting new sections, and replacing the heat shield bolts 54. This may be accomplished without removing the torque bar 24 and spacer block 150, thus greatly facilitating field repair of the wheel and brake assembly.
Turning now to FIG. 9, another exemplary torque bar assembly in accordance with the invention is illustrated. In this embodiment, a radially outer portion of the spacer block 150 is retained in a recess 170 formed in the wheel 14. The recess 170 is formed by a pair of circumferentially-spaced apart shoulders 174 that extend radially inwardly from the inner surface 155 of the wheel 14. The shoulders 174 can be part of a boss on the inner surface 155 of the wheel 14 (e.g., a thickened portion of the wheel 14). The shoulders 174 restrict circumferential movement of the spacer block 150. A radially inner portion of the spacer block 150 is retained in a recess 178 in the torque bar 24, which in the illustrated embodiment is formed by flanges 182 of the torque bar 24.
It will be appreciated that the spacer block 150 in FIG. 9 is restrained in recesses 170 and 178 thereby restricting relative movement between the wheel 14 and the torque bar 24. As in the embodiment illustrated in FIGS. 6-8, the spacer block 150 is compressed by the torque bar 24 thereby applying a preload to the torque bar 24. During installation, the torque bar 24 may resiliently flex radially inwardly to accommodate the spacer block 150. As mentioned above, the amount of pre-load on the torque bar 24 can be altered by adjusting the radial dimension of the spacer block 150. It will be appreciated that the torque bar may or may not be prestressed in this embodiment, depending on the specific application. In some applications, a clearance may be provided between the spacer block 150 and the inner surface 155 of the wheel such the spacer block 150 can move radially an amount without causing undue stress on the wheel 14.
Accordingly, the spacer block 150 opposes and/or restricts radially outward flexing of the torque bar 24, while the pre-load on the torque bar 24 opposes and/or restricts radially inward flexing of the torque bar 24. Shoulders 174 and flanges 182 captivate the spacer block 150 so as to resist circumferential flexing of the torque bar 24. The pre-loaded torque bar 24 can resist flexure under a wider range of dynamic vibrations thus making the wheel and brake assembly 10 more stable than a similar wheel and brake assembly without a pre-loaded torque bar 24.
Although the invention has been shown and described in the context of a torque bar 24 that is secured to a wheel and brake assembly by inserting a pin portion of a first end of the torque bar into a hole in the wheel and bolting the opposite end to the wheel, the invention can be used in connection with a wide variety of wheel and brake assemblies. By way of example, the invention can be used in a wheel and brake assembly wherein a torque bar is secured to the wheel at each end by bolts.
Although the invention has been shown and described with respect to a certain preferred embodiment or embodiments, it is obvious that equivalent alterations and modifications will occur to others skilled in the art upon the reading and understanding of this specification and the annexed drawings. In particular regard to the various functions performed by the above described elements (components, assemblies, devices, compositions, etc.), the terms (including a reference to a "means") used to describe such elements are intended to correspond, unless otherwise indicated, to any element which performs the specified function of the described element (i.e., that is functionally equivalent), even though not structurally equivalent to the disclosed structure which performs the function in the herein illustrated exemplary embodiment or embodiments of the invention. In addition, while a particular feature of the invention may have been described above with respect to only one or more of several illustrated embodiments, such feature may be combined with one or more other features of the other embodiments, as may be desired and advantageous for any given or particular application.

Claims

What is claimed is:
1. A wheel and brake assembly comprising: a wheel including a wheel well, the wheel well being generally cylindrical and coaxial with a rotational axis of the wheel; a torque bar connected to the wheel; and a spacer block interposed between the wheel well and the torque bar; wherein the spacer block is secured to the torque bar and the wheel against movement in at least one direction.
2. A wheel assembly as set forth in claim 1 , wherein the spacer block has an uncompressed thickness greater than the spacing between a radially inner surface of the wheel well and the torque bar when the spacer block is not installed therebetween such that the torque bar is pre-loaded against the spacer block.
3. A wheel assembly as set forth in any preceding claim, wherein the spacer block has a surface having a shape corresponding to the shape of a portion of the radially inner surface of the wheel well.
4. A wheel assembly as set forth in any preceding claim, wherein the spacer block is secured to the torque bar against movement along or transverse to the torque bar.
5. A wheel assembly as set forth in any preceding claim, wherein the torque bar includes a recess for receiving the spacer block for securing the spacer block against movement relative to the torque bar in at least one direction.
6. A wheel assembly as set forth in any preceding claim, wherein a radially outer portion of the spacer block is received in a recess in the wheel.
7. A wheel assembly as set forth in any preceding claim, wherein the torque bar is connected to the wheel in at least two axially spaced apart support locations, and wherein the spacer block is interposed between the radially inner surface of the wheel well and the torque bar at a location between the at least two support locations.
8. A wheel assembly as set forth in any preceding claim, wherein the spacer block is compressed between a radially inner surface of the wheel well and the torque bar.
9. A wheel assembly as set forth in any preceding claim, wherein the torque bar is connected to the wheel with at least one bolt.
10. A wheel assembly as set forth in any preceding claim, further comprising a heat shield between the spacer block and the torque bar.
11. A wheel assembly as set forth in any preceding claim, wherein the spacer block is made of a material having a low thermal conductivity.
12. A method of installing a torque bar in a wheel assembly, the wheel assembly including a generally cylindrical wheel well coaxial with a rotational axis of the wheel, the method comprising: interposing a spacer block between a radially inner surface of the wheel well and the torque bar; and securing the torque bar to the wheel in a manner that pre-loads the torque bar against the spacer block; wherein the spacer block is secured to the torque bar and the wheel against movement in at least one direction.
13. A method as set forth in claim 12, further comprising compressing the spacer block between the radially inner surface of the wheel well and the torque bar.
14. A method as set forth in any one of claims 12-13, further comprising supporting the torque bar in at least two locations and interposing the spacer block between the radially inner surface of the wheel well and the torque bar at a location between the at least two support locations.
15. A torque bar assembly for use in an aircraft wheel comprising: a torque bar; and a spacer block; wherein the spacer block can be secured to the torque bar and the wheel so as to restrict relative movement between the spacer block and the torque bar and wheel.
16. A torque bar assembly as set forth in claim 15, wherein the spacer block is securable to the torque bar at a position between distal ends of the torque bar.
17. A torque bar assembly as set forth in any one of claims 15-16, wherein a radially inner portion of the spacer block is received in a recess of the torque bar.
18. A torque bar assembly as set forth in any one of claims 15-17, wherein a radially outer portion of the spacer block is receivable in a recess of the wheel when mounted thereto.
PCT/US2007/088596 2007-12-21 2007-12-21 Wheel and brake assembly with torque bar WO2009082397A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/US2007/088596 WO2009082397A1 (en) 2007-12-21 2007-12-21 Wheel and brake assembly with torque bar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2007/088596 WO2009082397A1 (en) 2007-12-21 2007-12-21 Wheel and brake assembly with torque bar

Publications (1)

Publication Number Publication Date
WO2009082397A1 true WO2009082397A1 (en) 2009-07-02

Family

ID=39666108

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2007/088596 WO2009082397A1 (en) 2007-12-21 2007-12-21 Wheel and brake assembly with torque bar

Country Status (1)

Country Link
WO (1) WO2009082397A1 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2687742A1 (en) * 2012-07-18 2014-01-22 Goodrich Corporation Heat shield assemblies
EP3184843A3 (en) * 2015-12-21 2017-08-16 Goodrich Corporation Multipart torque bar for vibration suppression
EP3258129A1 (en) * 2016-06-17 2017-12-20 Goodrich Corporation Scalloped aircraft wheel rotor drive bar attachment boss for reduced thermal conduction
EP3572556A1 (en) * 2018-04-25 2019-11-27 Goodrich Corporation Hybrid torque bar for a wheel assembly
EP3925874A1 (en) * 2020-06-10 2021-12-22 Goodrich Corporation Aircraft wheel torque bar spacer
WO2022018103A1 (en) * 2020-07-21 2022-01-27 Safran Landing Systems Heat shield assembly
US20230182503A1 (en) * 2021-12-13 2023-06-15 Goodrich Corporation Heat shield assembly with stiffening plate

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5199536A (en) * 1992-02-13 1993-04-06 The B. F. Goodrich Company Heatshield installation for aircraft brake
WO2007118254A2 (en) * 2006-04-11 2007-10-18 Goodrich Corporation Wheel and brake assembly

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5199536A (en) * 1992-02-13 1993-04-06 The B. F. Goodrich Company Heatshield installation for aircraft brake
WO2007118254A2 (en) * 2006-04-11 2007-10-18 Goodrich Corporation Wheel and brake assembly

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2687742A1 (en) * 2012-07-18 2014-01-22 Goodrich Corporation Heat shield assemblies
US9903671B2 (en) 2012-07-18 2018-02-27 Goodrich Corporation Systems and methods for heat shield assemblies
EP3184843A3 (en) * 2015-12-21 2017-08-16 Goodrich Corporation Multipart torque bar for vibration suppression
US9938003B2 (en) 2015-12-21 2018-04-10 Goodrich Corporation Multipart torque bar for vibration suppression
EP3258129A1 (en) * 2016-06-17 2017-12-20 Goodrich Corporation Scalloped aircraft wheel rotor drive bar attachment boss for reduced thermal conduction
US10077818B2 (en) 2016-06-17 2018-09-18 Goodrich Corporation Scalloped aircraft wheel rotor drive bar attachment boss for reduced thermal conduction
EP3572556A1 (en) * 2018-04-25 2019-11-27 Goodrich Corporation Hybrid torque bar for a wheel assembly
US11092203B2 (en) 2018-04-25 2021-08-17 Goodrich Corporation Hybrid torque bar
US11668360B2 (en) 2018-04-25 2023-06-06 Goodrich Corporation Hybrid torque bar
EP3925874A1 (en) * 2020-06-10 2021-12-22 Goodrich Corporation Aircraft wheel torque bar spacer
US11608162B2 (en) 2020-06-10 2023-03-21 Goodrich Corporation Aircraft wheel torque bar spacer
WO2022018103A1 (en) * 2020-07-21 2022-01-27 Safran Landing Systems Heat shield assembly
FR3112755A1 (en) * 2020-07-21 2022-01-28 Safran Landing Systems Heat shield assembly
US20230182503A1 (en) * 2021-12-13 2023-06-15 Goodrich Corporation Heat shield assembly with stiffening plate
US12092175B2 (en) * 2021-12-13 2024-09-17 Goodrich Corporation Heat shield assembly with stiffening plate

Similar Documents

Publication Publication Date Title
EP2010795B1 (en) Wheel and brake assembly
WO2009082397A1 (en) Wheel and brake assembly with torque bar
US6003641A (en) Wheel and brake assembly
US4585096A (en) Brake apparatus
US5024297A (en) Torque transmitting beam for wheel having brake torque drives
AU2001267497B2 (en) Brake disk for a disk brake
EP2076687B1 (en) Segmented heat shield retention
CA2668730C (en) Disk brake
WO2007041518A2 (en) Brake rotor and abs tone ring attachment assembly that promotes in plane uniform torque transfer distribution
EP0774595B1 (en) Nested damping device with relative motion
WO2016014950A1 (en) Brake disc and mounting arrangement
US10895293B2 (en) Brake disc mounting arrangement
CN112469919A (en) Brake disc mounting arrangement
CN112469918A (en) Brake disc mounting arrangement
EP0774596B1 (en) Brake rod having a bending mode coulomb damper
EP0020389B1 (en) Disc brake assembly containing split discs
EP2126398B1 (en) Braking
WO2005088152A1 (en) Brake disc
CN110154640B (en) Elastic wheel for rail transit vehicle, assembling method of elastic wheel and rigidity design method of elastic wheel
EP2066912B1 (en) Brake disc and hub device for a motor vehicle
US20230407933A1 (en) Rotor clip for brake assembly
US20230407934A1 (en) Rotor clip for brake assembly
US20230400075A1 (en) Rotor clip for brake assembly
CN118208506A (en) Multi-stiffness brake assembly

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 07869772

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 07869772

Country of ref document: EP

Kind code of ref document: A1