• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The present application relates to an electromagnet clutch with an annular portion of an acoustic damping material sandwiched between an armature disk and a hub assembly, in particular between its web portion. The annulus and the web work together so that when the armature disc snaps into the engagement with the rotor of the clutch, while the armature magnetically engages the rotor, it slides prior to engagement, and also slips and It is to form an interference-layer attenuation system that reduces the noise that occurs during the disengagement of the armature disk. This design is to provide a reduced axial stretching package for conventional armature assemblies with interference-layer technology.
    公开号:KR19990072921A
    申请号:KR1019990006203
    申请日:1999-02-25
    公开日:1999-09-27
    发明作者:제임스엠. 하임；드위트이. 부쓰；제임스에이. 리카리
    申请人:수 에이 그리핀；데이나코포레이션；
    IPC主号:
    专利说明:

    SOUND DAMPING ARMATURE ASSEMBLY FOR AN ELECTROMAGNETIC COUPLING
    The present invention relates to an armature assembly for coupling, which can be selectively engaged and disengaged, such as an electromagnetic clutch or brake.
    Newton's U.S. Patent No. 4,493,407, which is incorporated herein by reference, discloses a general electromagnet clutch in which a slot armature is connected to a drive hub by a mounting plate such that when the electromagnet receives energy, it is attracted to the joint with the drive rotor. It is starting. The electromagnet clutch is a series of leaf springs coupled with the armature disc to the mounting plate for rotation, while allowing the armature disc to move apart in the direction of the rotor when the electromagnet receives energy or loses energy. Is connected.
    US Patent No. 5,150,779 to Booth, which is incorporated herein by reference, discloses another type of armature assembly. In the armature assembly, a resilient yieldable plastic web is operative to connect with the drive hub and a low magnetic reluctance armature disc for rotation. Upon engagement and disengagement of the clutch, the web is contracted in the axial direction such that the armature disk is spaced apart in the direction towards the rotor.
    However, one problem is that impact noise is generated when the armature disk initially snaps to the joint with the rotor. Noise is also generated by vibrations that occur while the armature disk is sliding and also when the disk is uncoupled from the rotor.
    For example, US Patent No. 5,372,228 to Jan Laningham, et al., Described herein, discloses an electromagnet clutch in which an annular portion of an acoustic damping material is sandwiched between an armature disc and a backing ring. It is starting. The annulus and the back ring work together and a constrained-layer damping system that reduces noise when the armature disk is snapped to the engagement with the rotor of the clutch and also while the armature disk is slipping and during disengagement. damping system). However, this approach increases the axial length of the electromagnet coupling and the rear disc adds weight to the overall device.
    Accordingly, there has been a need to provide an improved electromagnet coupling that solves or minimizes the above mentioned problems.
    It is an object of the present invention to provide a novel and improved armature assembly that reduces the degree of noise generated during initial coupling of the armature, during sliding and by disengagement.
    The above and other objects are achieved by an armature assembly sandwiched between the armature disc and the web portion of the hub assembly and subjected to compression, where the annular portion of the acoustic damping material is generally rigid, but the web portion is rigid to the hub of the hub assembly. It can move in the axial direction with respect to. The web acts as a deterrent-layer, allowing the development of sheer strains in the damping material and the dispersion of noise as a result of the shear deformation of the damping material.
    The armature assembly of the present invention also has the advantage of having a reduced axial length in relation to conventional armature assemblies in which an interference-layer damping technique is employed. In addition, the armature assembly according to the present invention has a reduced weight relative to the conventional armature assembly using the interference-layer damping technique since no back plate is used.
    The above and other objects, advantages and features of the present invention will be described below with reference to the accompanying drawings, for example.
    1 is an enlarged perspective view showing a partial cross-sectional view of an electromagnet coupling according to the present invention.
    2 is a partial cross-sectional view taken along line 2-2 of the electromagnet coupling of FIG. 1 with an armature assembly incorporating characteristic features of the present invention;
    3 is an exploded perspective view of the armature assembly.
    4 is a cross-sectional view taken along line 4-4 of FIG. 2;
    5 is a cross-sectional view taken along line 5-5 of FIG. 4;
    Figure 6 is a plan view of the side of a hub assembly portion of the armature assembly of the present invention.
    FIG. 7 is an enlarged view of a portion of the armature assembly shown in FIG. 5. FIG.
    8 is an end view of the first embodiment of the annular portion made of an acoustic damping material.
    Fig. 9 shows a second embodiment of the annular portion made of an acoustic damping material.
    Fig. 10 shows a third embodiment of the annular portion made of an acoustic damping material.
    11 and 12 show fourth and fifth embodiments of the annular portion made of an acoustic damping material.
    FIG. 13 shows a sixth embodiment of an annular portion made of an acoustic damping material in which a molded mesh tab is incorporated; FIG.
    Fig. 14 shows a seventh embodiment of the annular portion made of an acoustic damping material having an integral adhesive portion with the outer face of the annular portion;
    Explanation of symbols for main parts of the drawings
    10: Clutch 11: Supercharger
    13: drive shaft 14: one-piece annular field cell
    16: ring 18: legs
    20: winding-up part 26: rotor
    30: drive belt 36: rotor face
    38: armature assembly 40: hub assembly
    42: disc 44: elastomeric annular portion
    46: hub 48: spider
    52 lug 56 web portion
    70: notch 72: tongues
    FIG. 1 shows an electromagnet coupling 10 which is in a brake but here in the form of an electromagnet clutch 10.
    2 relates to a drive component which may be an automobile supercharger 11 having an annular nose portion 12 for clutch mounting and additionally having a drive shaft 13 extending through the nose. The figure which shows the clutch 10 used.
    The clutch 10 is partially by a one-piece annular field cell 14 having an L-shaped radial cross section and having an inner pole ring 16 and a radially outer extending pole leg 18 (best shown in FIG. 1). It is provided with an electromagnet formed by. In addition, the supercharger 11 may be provided with a field adapter 19 for fixing the coupling 10. The multiple switching windings 20 are fixed in the annular winding casing 24. The pawl leg 18 has a distal end that extends to the inner face of the rotor pleats for the inner circumference of the rotor pleats (eg, approximately 0.5 mm gap in the configuration embodiment). By the way, the radius height of the legs 18 is reduced through a predetermined area of the circumference to allow the introduction of the electrical conductor for the windings 20. The structure described above is one structure that can be used in the armature assembly of the present application. The armature assembly according to the invention can be used for other rotor assemblies with other structures utilizing electromagnets. For example, it can be prepared in U.S. Patent No. 4,160,498 to Newton, et al., Which interposes a changeable electromagnet structure in detail.
    The annular rotor 26 is adapted to be rotatably journaled to the nose 12 of the supercharger 11 by a bearing 28 and to be driven from an automobile engine by an endless belt 30. The rotor 26 has a U-shaped radial cross section and has inner and outer concentric annular pole pieces 32, 34 made of steel with low magnetic reluctance, the inner pole pieces It is fixed to the bearing outer ring part. The plurality of axially spaced grooves extend around the outer side of the outer pole piece 34 in the circumferential direction and are intermediately installed on the complementary ribs on the inner side of the drive belt 30. Thus, the outer pole piece is to form a pulley for the belt 30.
    The inner pole piece 32 of the rotor 26 is spaced inwardly of the pole ring 16 of the field cell 14 while the outer pole piece 34 of the rotor is wound around the windings 20 and the casing ( 24). When the windings 20 are excited by a voltage source, magnetic flux is generated that travels through the core and the rotor and crosses the various gaps between the pole and the pole piece. Controlled flux transfer properties between the core and the rotor are readily understood in the art, as detailed in the Newton et al. Patent.
    An axial facing friction surface 36, which forms a groove (not shown) in the circumferential circumferential direction in order to form a multiple magnetic pole, is connected between the pole pieces 32, 34 of the rotor 26. Is extended. In a configuration embodiment, face 36 is formed with rows of three radially spaced and angularly spaced grooves extending in the circumferential direction. The groove is offset by a row of two radially spaced grooves of the armature disk. The groove is such that the armature disc has a magnetic pole that operates with the pole of the face 36 of the rotor 26. When the windings 20 receive energy, the friction surface forms a rotating magnetic field member.
    The armature assembly 38 is arranged opposite to the rotor face 36. Once the windings 20 are excited, the magnetic flux pulls the armature assembly component into frictional engagement with the rotor face 36 to engage the rotor and armature assembly for integral rotation. Rotation of the armature assembly 38 is transmitted to the shaft 13 to drive the supercharger 11.
    3 is an exploded perspective view of an armature assembly 38 according to the present invention. In general, the armature assembly 38 may be similar to that disclosed in US Pat. No. 5,150,779 to Booth or US Pat. No. 5,372,228 to Jan Ranningham et al. And as will be described in detail below, the armature assembly 38 is an improvement over the armature assembly. In particular, the armature assembly 38 is an elastomeric annulus 44 consisting of a hub assembly 40, an armature disk 42, and an acoustic damping material interposed between the disk 42 and the web portion of the hub assembly 40. ).
    As shown in FIG. 4 and better shown in FIG. 5, the hub assembly 40 has a tubular hub 46 and a spider 48 having a central axis. The tubular hub 46 is made of powder metallurgy, which is good but not essential, and is installed flexibly on the shaft 13 in an assembled state. In one embodiment, the shaft 13 is provided with an outer helical spline tooth, while the inner diameter of the hub 46 has a corresponding inner helical spline tooth, where the hub is splined to the axis 13. The hub 46 is one that can be clamped to an axially fixed position on the shaft 13 by a helixed nut 50 (preferably in FIG. 2) at the free end portion of the shaft 13. As can be seen in FIG. 6, the hub 46 is formed with radially extending and angularly spaced lugs 52 for the purpose described below.
    The spider 48 may be injection molded from an elastic yielding material such as plastic. Suitable materials for the spider include DuPont ZYTEL® 8018HS BKBO85 or the like.
    As shown in FIG. 5, the spider 48 has a central sleeve 54 that surrounds the forward end portion of the hub 46. The hub 46 is preferably insert molded in place during spider molding, such that the plastic of the sleeve 54 is joined and enclosed to the outer end portion of the hub. Lug 52 functions to engage sleeve 54 and hub 46 for integral rotation. That is, when forming the spider 48, plastic flows into the space between the lugs 52 to fill the space, thereby preventing relative rotation between the hub 46 and the sleeve 54. Each lug 52 may also form two shoulders that face in opposite axial directions and are joined by the plastic of the sleeve 54 to capture the sleeve 54 in the axial direction at the hub 46. For reference, the lugs can be manufactured by US Pat. No. 5,036,964 of Boot et al., Which describes the lugs 52 in more detail.
    The spider 48 additionally has a web portion 56 which is integrally formed in the radial direction from the sleeve 54. Web 56 is preferably circular and quite thin in the axial direction. Since the plastic is relatively flexible, the web portion 54 is in the axial direction with respect to the sleeve 54 in the hinged operation, indicated by " 58 " in FIG. 5, in which the sleeve is formed at the junction of the web 56. As shown in FIG. There is flexibility.
    6 and 7, the spider 48 is formed with three angled spaced pads or bosses 60. The pad 60 is formed integrally with the rear side of the web 56 and is adjacent to the hole 62 formed in the spider 48. As shown in FIG. 7, the pad 60 protrudes in the axial rearward direction from the rear side of the web 56 and advances the armature disc 42 in three angularly spaced areas adjacent the outer periphery of the disc. It is combined with the side. The axial gap, denoted T1, is formed between the web 56 and the armature disk 42 at approximately 0.023 inches (+0.005, -0.004 inches) in the configuration embodiment. It is understood that other gaps and thicknesses are applicable when a suitable annular compression is obtained. 6, the spider 48 may also be formed with three angularly spaced rearwardly projecting tabs 63. As shown in FIG. The installation purpose of the tab 63 is described in detail below.
    As shown in FIG. 3, the armature disk 42 may be formed of a low magnetoresistive material such as AISI 1010 steel. In the armature disc 42 additionally, grooves spaced at regular angles are formed in rows 64, 66 spaced in two radial directions and extending in the circumferential direction. The groove causes the armature disc 42 to have a magnetic pole that operates with the pole of the face 36 of the rotor 26. If the windings 20 lose energy (e.g., in a non-energy state), the narrow axis air gap 68 (FIG. 2) is the width of the armature disk 42 and the pole surface of the rotor 26. Exists in between. When the windings 20 are energized, the magnetic flux cuts the gap 68 transversely and screwes back and forth through the poles of the friction surface 36 and the armature disc 42 in a conventionally known manner, The armature disk is pulled into the frictional engagement with the rotor to engage the armature disk to rotate integrally with the rotor 26.
    Impact noise can be generated upon snap connection of the steel armature disk 42 to the joint with the steel rotor 26. Noise is also generated during the disengagement and sliding of the armature disk 42. According to the present invention, the noise is reduced by constraining the outer periphery of the armature assembly 38 as an interference-layer damping sandwich with acoustic damping material.
    In particular, and with reference to FIG. 8, an elastomeric annulus 44 made of acoustic damping material is provided in the armature assembly 38 to minimize noise. The first embodiment shown in FIG. 8 is not necessary but includes a compressible acoustic damping material. Such materials include silicone composite casts with strands of reinforcing fibers, preferably fiberglass mesh, for example the US trade name PORON HT 1500. Some are available from Rogers Corporation of Elk Grove Village, Illinois. "Mesh" may mean, for example, fiber strands woven in a manner similar to clothing, or may only mean that the fiber strands in any manner are supported by one another. In the first embodiment, an elastomeric annular portion 44 of the following properties is applied:
    itemvalueper Durometer (Shore "A") without Mesh40-75 preferably 6-75 best 75ASTM D-2240 Breaking Strength Warp250 min PPIASTM D-751 Compression set35% maxASTM D-395 Method B Temperature range-65 ° F to + 400 ° F
    The annular part 44 cuts the sheet | seat material (for example, sheet | seat material PORON (trademark) HT-1500). In another method of manufacture, the annulus 44 is in the form of stock silicon and strands of fiber, preferably mesh, having the parameters as described above, and more preferably formed by processing a fiberglass mesh. . And other forms of mesh and / or fibers formed of a polyester material or of a material such as fiber free may optionally be appropriate depending on the strength required for the particular coupling 10 application. For example, missing fiber strands together in annulus 44 (eg, an annulus consisting essentially of certain durometer silicon) may provide adequate continuous rotational speed or the armature assembly 38 may Do not expect to exceed 6,000-7,000 rpm.
    The first embodiment of the annular portion 44 is provided with notches 70 spaced at three constant angles corresponding to the size and shape of accommodating the three pads 60. Further, the annular portion 44 may be formed to have three tongues spaced apart at three predetermined angles to form three corresponding grooves 73 therebetween. The tongue 72 is adapted to be of a size and shape so that one of the individual arc-shaped tabs 63 can be accommodated in one of the individual grooves 73 between the tongues 72.
    The annular portion 44 is well sandwiched between the armature disk 42 and the web 56 forming an interference-layer for the acoustic damping material. The annular portion 44 preferably maintains compression between the armature disk 42 and the web 56 after the armature assembly 38 is assembled. As shown in FIG. 7, the gap between the armature disk 42 and the web 56 is approximately T1. The thickness of the annular portion 44 is chosen to be larger than the gap, and the thickness is approximately that indicated by T2. The acoustic damping annulus 44 is compressed and held between the disk 42 and the web 56 by means such as the rivet 74 so that the armature disk 42 and the spider 48 are secured to each other. Others that can be used to achieve the same effect as above are bolts, screws, pins, moldings, or the like. Rivets 74 are common with shanks extending through holes axially aligned with disk 42 and web 56. The head of the rivet is disposed adjacent to the forward face of the web 56 while the deformed end of the rivet is received in counter-bores formed in the working face of the armature disk 42. In a configuration embodiment, the reverse bore is missing. When the rivet is deformed, the damping annulus 44 is compressed between the armature disk 42 and the web 56. In the configuration embodiment, the gap T1 is approximately 0.023 inches while the annular portion 44 is approximately 0.031 inches thick, which ensures that the annular portion 44 is compressed during assembly. The acoustic attenuation efficacy is to be reduced if the annulus 44 is not kept in compression.
    Example 1
    In the configuration embodiment, the acoustic damping annulus 44 is approximately 0.0031 inches (+/- 0.005 inches) in thickness (uncompressed) cut from Rogers Poron HT-1500 reinforced with silicone rubber having the following specific properties: Durometer = 75 (shore “A”); Braking strength = 250 ppi (pounds per inch); Tear strength = 70 ppi; Compression set = 35% maximum; Weight loss <1%; "Time before weeping = 24 hours minimum; and resistance to radiant heat 500F. The shape structure is generally as shown in Figure 8. The coupling meets the following threshold without loss of compression in the annulus 44; By incorporating an armature assembly with an annular portion 44 of the structure to maintain the effectiveness of the noise attenuation operation:
    (i) 13,500 rpm at 250 ° F. for 2 hours.
    (ii) 12,250 sowl 4,000 rpm cycling test at 250 ° F. for 509 hours.
    Example 2
    The second configuration embodiment comprises a silicone material having a durometer between about 40-60 (Shore “A”) and is formed of a loose woven yarn (eg, approximately 1/16 inch spaced strands, ie, 16 The thickness (uncompressed) with the polyester mesh with strands / inch) is approximately 0.031 inch (+/- 0.005 inch). The strand is formed from a crossing mesh having a set of strands (all parallel to each other) where the second set of strands (all parallel to each other) intersect at an angle of about 45 degrees. The shape of this structure is similar to that shown in FIG. 8 except for the tongue 72 formed in its inner diameter. An armature assembly having an annular portion of this structure made of attenuating material exhibits a noise reduction effect of up to about 10,000 rpm.
    The armature assembly 38 according to the present invention is more compact in the axial direction than the armature assembly disclosed in U.S. Patent No. 5,372,228 and does not require a steel plate as disclosed in the patent, further improving the patent as a lighter one. will be. In addition, the added strength provided by the reinforcing fiber strands included in the annulus 44 may (i) allow the web 56 to be rigid in the radial direction and flexible in the axial direction to act as an interference layer in the interference-layer damping system. And (ii) allow a significantly faster rotational speed while maintaining compression of the annular portion 44.
    9 shows a second embodiment showing an annular portion 44A having three arc-shaped grooves 76 spaced apart at three constant angles corresponding to the size and shape of three arc-shaped tabs 63 spaced apart. Yes. Thus, the annulus 44A has the ability to align itself in place, regardless of the armature disk clamping force. In addition, the radial cross section is increased in the embodiment to improve the burst strength without (i) increasing the axial thickness and (ii) increasing the modulus of elasticity of the assembly. In addition, the positive alignment arrangement provided by the arcuate tabs 63 in combination with the arcuate grooves 76 is to maintain the annular portion leaving the pad or boss 60 during assembly.
    Fig. 10 shows a third embodiment, namely the acoustic attenuation annular portion 44B. During operation of the coupling 10, in particular during radial rotational speed of the armature assembly 38, radial forces cause the inner and outer diameter portions of the annular portion to expand radially outward. As the annulus expands thinly due to the radial force, the act of thinning may cause compression loss in the annulus, which in turn lowers the efficacy of the annulus 44, such as acoustic attenuation. In order to reduce the influence of the centrifugal force, the third embodiment 44B has a ring 78 molded or attached to the inner diameter (or optionally the outer diameter--not shown) of the annular portion 44B. . The ring reinforces the annulus 44B to resist radial forces, thus resisting or counteracting the "thinning" of the annulus 44B during high speed rotation. Thus, compression is maintained.
    11 and 12 show the fourth and fifth embodiments of the annular portion 44, that is, the annular portion 44C and the annular portion 44D, respectively. The annular portion 44C is formed with a leg 80 of a considerably thicker thickness at its inner diameter portion. In this embodiment the hub assembly 40, in particular the spider 48, is formed without the arcuate tab 63. Effectively, a thick inner forming leg 80 replaces the function of the arcuate tab 63. The structure of the annular portion 44C is a structure that increases its burst strength without increasing the thickness in the axial direction and without increasing the elastic modulus of the assembly.
    The annular portion 44D shown in FIG. 12 is similar to the annular portion 44C shown in FIG. 11 except that a fairly thin leg 82 formed in its inner diameter portion is formed. In this embodiment, three arc-shaped tabs 63 extend in the other direction to form a continuous circular rib, and the thin legs 82 are installed between the ribs and the inner diameter of the armature disc 42 at the time of assembly. It is of the size that becomes. In the embodiment shown in FIG. 11, the annular portion 44D becomes strong without increasing the length in the axial direction or with increasing the axial package, and the forming leg 82 is also used in which the annular portion 44D causes the extrusion loss. It suppresses high RPM extrusion and has an acoustic attenuation effect.
    Fig. 13 shows another sixth embodiment of the annular portion 44, that is, the annular portion 44E. In this embodiment, the molded mesh tab 84 is formed when the annular portion 44E is manufactured. That is, the annulus 44E is shaped such that, for example, the mesh tab of the glass fiber extends beyond the face of the annulus itself. The annular portion 44E enables an improved method of manufacturing the armature assembly. Specifically, the annular portion 44E in which the forming mesh tabs are formed may be disposed in the injection molding cavity in which the spider 48 is molded to the tubular hub 46. Plastic (eg, the material from which the spider is formed) flows around the extension tabs 84 to secure the annulus 44E to the hub assembly 40, particularly to the web 56 of the spider 48. This auxiliary assembly, which includes the hub 46, the spider 48, and the acoustic damping annulus 44E, is then loaded into the rivet area, for example, and secured to the armature disk 42 without degrading production. As an additional advantage, the annulus 44E made of acoustic attenuation material maintains the correct angular direction during assembly. This embodiment can simplify the assembly process and minimize the slow-down associated with the direction in which the annular portion 44 is directed to the hub assembly 40, such that the acoustically damped annular portion 44E during manufacturing ) Is to ensure correct positioning.
    14 shows an additional embodiment of an annular portion 44, ie annular portion 44F, having a layer of adhesive portion 86 on one side thereof. This embodiment also allows a method of manufacturing an improved armature assembly, wherein the annular portion 44F is arranged with an adhesive side facing the inner direction side of the spider 48. Further, the adhesive portion may be applied to the armature side of the annular portion 44E. (Not shown) Further, the adhesive portion may be applied to the spider 48 and / or the armature 42 with the same effect. Again, this auxiliary assembly is for example loaded into a riveting zone and secured to the armature disk 42 without a decrease in production or slow motion. Again, annulus 44F maintains the correct and necessary angular position relative to the spider of hub assembly 40 suitable for assembly.
    The armature assembly of the present invention also has the advantage of having a reduced axial length in relation to conventional armature assemblies in which an interference-layer damping technique is employed. In addition, the armature assembly according to the present invention has a reduced weight relative to the conventional armature assembly using the interference-layer damping technique since no back plate is used.
    Although the present invention has been described through specific embodiments, the foregoing description of the present application has been described for the purpose of illustrating the present invention, and is not intended to limit the present invention, which is intended to be limited only by the appended claims. Changes and corrections may be made by those skilled in the art within the spirit and scope of the present invention.
    权利要求:
    Claims (17)
    [1" claim-type="Currently amended] In an armature assembly for selectively coupling and disengaging electromagnet coupling, the armature assembly comprises:
    A hub with a central axis;
    A spider made of elastic yieldable plastic having a sleeve portion, a web portion, and a sleeve portion compliant with the web portion in an axial forward and backward direction with respect to the sleeve and an integral hinge means with the web portion;
    An annular armature disk made of a material having a relatively low magnetoresistance and spaced axially from the web portion;
    An annular portion having a fiber strand and made of a compressible acoustic damping material sandwiched between the web portion of the spider and the armature disk;
    Means for securing the armature disk and the spider to each other while placing the annular portion in a constant axial compression section between the disk and the web portion;
    And the sleeve portion is telescopic over the hub and captures rotational and axial movement with respect to the hub, the web portion projecting radially from the sleeve.
    [2" claim-type="Currently amended] The armature assembly of claim 1, wherein the annular portion comprises an elastomeric material and the strand comprises a polyester material.
    [3" claim-type="Currently amended] 3. The armature assembly of claim 2, wherein the strands of polyester form a polyester mesh.
    [4" claim-type="Currently amended] 4. The armature assembly of claim 3, wherein the strands intersect at an angle of about 45 degrees.
    [5" claim-type="Currently amended] The armature assembly of claim 1, wherein the annular portion comprises an elastomeric material and the strand comprises a fiberglass material.
    [6" claim-type="Currently amended] 6. The armature assembly of claim 5, wherein the fiberglass strands form a fiberglass mesh.
    [7" claim-type="Currently amended] 7. The web of claim 6 wherein the web portion has a plurality of spaced apart tabs and the annular portion has a corresponding plurality of spaced apart tongues defining a plurality of grooves formed sized to receive the tabs individually. An armature assembly, characterized in that.
    [8" claim-type="Currently amended] 2. The web of claim 1, wherein the web portion has a plurality of spaced apart tabs, and the annular portion comprises an elastomeric material and is spaced at a predetermined number of corresponding plurality formed to receive the tabs individually. An armature assembly having a groove.
    [9" claim-type="Currently amended] 2. The web of claim 1 wherein the web portion has a circular rib and the annular portion comprises an elastomeric material and has an outer diameter and an inner diameter portion, wherein the annular portion is additionally associated with its radial extension. An armature assembly having a ring extending from at least one of the outer and inner diameter portions for facing operation.
    [10" claim-type="Currently amended] 2. The annular portion of claim 1 wherein the annular portion comprises an elastomeric material and has an inner diameter and an outer diameter, the inner diameter extending radially axially extending radially between the sleeve and the inner diameter of the armature disc. An armature assembly, characterized in that to form a leg.
    [11" claim-type="Currently amended] 2. The armature disk of claim 1, wherein the web portion has a circular rib and the annular portion comprises an elastomeric material and has an inner diameter portion and an outer diameter portion, wherein the inner diameter portion extends in an axial direction to form an inner side of the armature disk. An armature assembly defining a leg extending radially between the diameter and the rib.
    [12" claim-type="Currently amended] 18. A method of manufacturing an armature assembly having an armature disc, an annular portion of acoustically damped material, and a hub assembly having a web portion.
    (A) forming an annular portion made of an acoustic damping material with integral attachment means;
    (B) securing the annular portion to the web portion of the hub assembly using attachment means;
    (C) securing the armature disk to the web portion of the hub assembly to compress the annular portion.
    [13" claim-type="Currently amended] The method of claim 12, wherein step (A) comprises:
    Forming one of the fiberglass mesh and the polyester mesh with forming tabs protruding therefrom forming an attachment means;
    Placing the one mesh in a first mold;
    Introducing an elastomeric material into the first mold to form an annular portion.
    [14" claim-type="Currently amended] The method of claim 13, wherein step (B) comprises:
    Placing the annulus in a second mold that is structured to produce a hub assembly such that the forming tab extends into an area of the second mold to form a web portion;
    Introducing plastic into the second mold to form a hub assembly;
    The shaping tab secures the annular portion to the web portion.
    [15" claim-type="Currently amended] The method of claim 12, wherein step (C) comprises:
    And securing the armature disk to the web portion of the hub assembly.
    [16" claim-type="Currently amended] 13. The method of claim 12, wherein step (A) is implemented by applying an adhesive that defines an attachment mesh on one side of the annular portion.
    [17" claim-type="Currently amended] The method of claim 16, wherein step (B) comprises:
    Positioning the annular portion in the required angular direction relative to the web portion with the adhesive side in the direction towards the web portion;
    And attaching the annular portion to one of the armature and the web portion by applying an adhesive force to one side of the annular portion opposite to the bonding side.
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    US6591477B1|2003-07-15|
    JPH11280794A|1999-10-15|
    GB9904390D0|1999-04-21|
    FR2775503B1|2000-12-22|
    GB2339861B|2002-07-24|
    FR2775503A1|1999-09-03|
    DE19908439A1|1999-09-02|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    法律状态:
    1998-02-27|Priority to US09/032,572
    1998-02-27|Priority to US09/032,572
    1998-02-27|Priority to US9/032,572
    1999-02-25|Application filed by 수 에이 그리핀, 데이나코포레이션
    1999-09-27|Publication of KR19990072921A
    2005-10-05|Application granted
    2005-10-05|Publication of KR100519028B1
    优先权:
    申请号 | 申请日 | 专利标题
    US09/032,572|1998-02-27|
    US09/032,572|US6194803B1|1998-02-27|1998-02-27|Sound damping armature assembly for an electromagnetic coupling|
    US9/032,572|1998-02-27|
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