SHOCK ABSORBER AND METAL COVER

Abstract

A shock absorber and a metal cover reduce contact noise generated as a shock absorbing member hits a collar and have higher vibration damping performance. A shock absorber absorbing vibration to a heat insulator covering an exhaust manifold as a vibration source includes a collar, a grommet, an annular compression mesh including a shock absorbing material, and a spiral spring overlaid on a compression mesh. The compression mesh has a center hole loosely receiving a collar shaft. The spiral spring spiral in a plan view has a spring constant equal to or smaller than that of the compression mesh. The compression mesh includes a restriction ridge along a lower large-diameter portion to restrict radial movement of the spiral spring relative to the compression mesh. The circumferential contact area X of the lower large-diameter portion with the restriction ridge ranges between 40% and 55%.

Claims

1. A shock absorber for connecting a vibration member as a vibration source and a covering member for covering the vibration member to absorb vibration from the vibration member to the covering member, the shock absorber comprising: a collar including a substantially tubular collar shaft to be fastened to the vibration member with a fastener, and annular flanges protruding radially outward from two axial ends of the collar shaft; an annular fixing member fixable to the covering member; an annular shock absorbing member located between the collar and the fixing member with a radially outer peripheral portion of the shock absorbing member fixed to the fixing member, the shock absorbing member comprising a shock absorbing material; and a spring located between at least one of the flanges on the collar and the shock absorbing member, and overlaid on the shock absorbing member, wherein the shock absorbing member includes a radially inner peripheral portion loosely fitted on the collar shaft at least in a radial direction, the spring has a spring constant equal to or smaller than a spring constant of the shock absorbing member, the shock absorbing member includes a movement restrictor in contact with the spring to restrict radial movement of the spring relative to the shock absorbing member, and the spring has a radially outer portion in contact with 40% to 55% of a circumference of the movement restrictor.

2. The shock absorber according to claim 1, wherein the spring is spiral in a plan view, and the movement restrictor extends along and is in contact with the radially outer portion that is radially outward in the spring spiral in a plan view.

3. The shock absorber according to claim 1, wherein the movement restrictor is adjacent to the spring on the shock absorbing member, and includes a movement restriction ridge having an outwardly-curved cross section.

4. The shock absorber according to claim 1, wherein the spring is substantially truncated in a side view, and has a larger diameter in a portion nearer the shock absorbing member than in a portion nearer the at least one of the flanges.

5. The shock absorber according to claim 4, wherein the spring substantially truncated in a side view has a height greater than a distance between the shock absorbing member in contact with one of the flanges on the two axial ends and another of the flanges.

6. A metal cover, comprising: the shock absorber according to claim 1 attached to a covering member for covering a vibration member.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0046] FIG. 1 is a schematic perspective view of a shock absorber.

[0047] FIG. 2 is a schematic cross-sectional view of the shock absorber.

[0048] FIG. 3 is an exploded perspective view of the shock absorber.

[0049] FIG. 4 is a horizontal cross-sectional view of the shock absorber.

[0050] FIG. 5 is an enlarged partial perspective view of an insulator base with the shock absorber.

[0051] FIG. 6 is a schematic front view of a shock absorber-attached heat insulator mounted on an engine.

[0052] FIG. 7 is a schematic cross-sectional view of the shock absorber attached.

[0053] FIG. 8 is a view of the shock absorber describing the operation.

[0054] FIG. 9 is a view of shock absorbers used in damping evaluation tests.

[0055] FIG. 10 is a view of shock absorbers used in damping evaluation tests.

[0056] FIG. 11 is a view of shock absorbers used in damping evaluation tests.

[0057] FIG. 12 is a photograph of shock absorbers showing the damping evaluation test conditions.

[0058] FIG. 13 is a schematic cross-sectional view of shock absorbers.

DETAILED DESCRIPTION

[0059] A shock absorber 10 according to one or more embodiments of the present invention and its damping will be described with reference to FIGS. 1 to 12.

[0060] FIG. 1 is a schematic perspective view of the shock absorber 10. FIG. 2 is a schematic vertical cross-sectional view of the shock absorber 10. In FIG. 1, front parts of the components of the shock absorber 10 are cut away to show the internal structure of the shock absorber 10. In the figure, a collar 20 and a grommet 30 are cut away by larger parts than a compression mesh 40 and a spiral spring 50.

[0061] FIG. 3 is an exploded perspective view of the shock absorber 10. In FIG. 3, front parts of the components of the shock absorber 10 are cut away to show the internal structure of the shock absorber 10. For easy understanding of the shock absorber 10 being attached, the broken lines in FIG. 3 indicate an insulator base 100 that receives the shock absorber 10.

[0062] FIG. 4 is a horizontal cross-sectional view of the shock absorber 10. In detail, FIG. 4 is a cross-sectional view in the direction indicated by arrows along line a-a in FIG. 2 without showing the grommet 30.

[0063] FIG. 5 is an enlarged partial perspective view of the insulator base 100 to be the heat insulator 1 with the shock absorber 10. FIG. 6 is a schematic front view of a shock absorber-attached heat insulator 1A mounted on an engine 2. FIG. 7 is a schematic cross-sectional view of the shock absorber 10 attached. FIG. 8 is a view of the shock absorber 10 attached. In detail, FIG. 8(a) is a schematic vertical cross-sectional view of the shock absorber 10 under no load, and FIG. 8(b) is a schematic vertical cross-sectional view of the shock absorber 10 under a load.

[0064] The term upward refers to the top in FIGS. 3 to 8, and the term downward refers to the bottom in these figures.

[0065] FIGS. 9 to 11 are views of shock absorbers used in damping evaluation tests. FIG. 12 is a photograph showing the damping evaluation test conditions.

[0066] In detail, FIG. 9(a) is a horizontal cross-sectional view of a shock absorber 10A, FIG. 9(b) is a horizontal cross-sectional view of a shock absorber 10B, FIG. 9(c) is a horizontal cross-sectional view of the shock absorber 10, and FIG. 9(d) is a horizontal cross-sectional view of a shock absorber 10C. FIG. 10(a) is a horizontal cross-sectional view of a shock absorber 10D, FIG. 10(b) is a horizontal cross-sectional view of a shock absorber 10E, FIG. 10(c) is a horizontal cross-sectional view of a shock absorber 10F, and FIG. 10(d) is a horizontal cross-sectional view of a shock absorber 10G. FIG. 11(a) is a horizontal cross-sectional view of a shock absorber 10H, and FIG. 11(b) is a horizontal cross-sectional view of a shock absorber 10J.

[0067] As described later, the shock absorber 10 is a mounting fixture for mounting the heat insulator 1 onto the engine 2. As shown in FIGS. 1 and 2, the shock absorber 10 includes the substantially annular collar 20 located at the center in a plan view, the radially outward grommet 30, and the compression mesh 40 and the spiral spring 50 located between the collar 20 and the grommet 30.

[0068] The collar 20 is substantially tubular and has a smaller height than its diameter. The collar 20 is formed from an iron-based material, such as steel plate cold commercial (SPCC). The collar 20 includes a tubular collar shaft 21 extending vertically to receive a fastening bolt 110 (refer to FIG. 7) and annular flanges 22 (23, 24) protruding radially outward from the upper and lower ends of the collar shaft 21. The collar shaft 21 and the flanges 22 are integral with each other.

[0069] More specifically, as shown in FIG. 3, the collar 20 includes a collar part 25 including the collar shaft 21 and the upper flange 23 that are integral with each other, and the toroidal lower flange 24 having a fitting hole 24a at the center in a plan view for receiving the lower end of the collar shaft 21. The upper flange 23 and the lower flange 24 are disks with the same diameter. The collar part 25 has a bolt hole 25a extending vertically from the upper flange 23 to the lower end of the collar shaft 21.

[0070] The collar shaft 21 in the collar part 25 integrally including the collar shaft 21 and the upper flange 23 has the lower end fitted in the fitting hole 24a at the center of the lower flange 24 in a plan view. The collar shaft 21 has the lower end swaged to integrate the collar part 25 and the lower flange 24 together, forming the collar 20.

[0071] In the present embodiment, the collar shaft 21 is tubular and has a diameter of 10 mm. The distance between the flanges 22 on the upper and lower ends, or more specifically, the vertical length from the bottom surface of the upper flange 23 to the upper surface of the lower flange 24 is, but not limited to, about 4 mm, which is about one-third of the diameter of the collar shaft 21.

[0072] The grommet 30 is a ring member that is annular in a plan view, and formed from a metal plate processed into a substantially S-shape in a half cross section. The grommet 30 includes a first fixing section 31 for holding the heat insulator 1 radially outward, a second fixing section 32 for holding a radially outer peripheral portion 42 of the compression mesh 40 radially inward, and a connecting section 33 radially connecting the lower end of the first fixing section 31 and the upper end of the second fixing section 32. The first fixing section 31, the connecting section 33, and the second fixing section 32 are arranged in the stated order from above and integral with one another.

[0073] The first fixing section 31 is formed by folding, radially outward, an upper portion of a metal plate corresponding to a radially inward portion from the connecting section 33. The first fixing section 31 has a substantially lateral U shape open radially outward in half cross section. The first fixing section 31 fixes the heat insulator 1 together with the connecting section 33 by swaging.

[0074] The second fixing section 32 is formed by folding, radially inward, a lower portion of a metal plate corresponding to a radially outward portion from the connecting section 33. The second fixing section 32 has a substantially lateral U shape open radially inward in half cross section. The second fixing section 32 fixes the radially outer peripheral portion 42 of the compression mesh 40 (described later) together with the connecting section 33 by swaging.

[0075] The grommet 30 with the above ring structure has an inner diameter larger than the outer diameter of the collar 20 (or the outer diameters of the flanges 22) and a height substantially the same as the distance between the flanges 22 on the collar 20.

[0076] The compression mesh 40, which mainly provides shock absorbing performance in the shock absorber 10, is formed from wires knitted and compressed together into a ring with a center hole 41 in a plan view for receiving the collar shaft 21. The radially outer peripheral portion 42 is fixed to the second fixing section 32 of the grommet 30 by swaging. The compression mesh 40 with the radially outer peripheral portion 42 fixed to the second fixing section 32 is vertically bendable and compressible.

[0077] More specifically, the compression mesh 40 is formed from stainless steel (SUS316) wires knitted together, with stockinette stitch, into a substantially tubular shape. The wires have circular cross sections with a diameter of 0.2 mm. The tubular mesh is compressed into an annular shape with a thickness of 1.0 mm, which is less than the distance between the upper flange 23 and the lower flange 24. The compression mesh 40 is thus elastically deformable, or bendable and compressible, and has a spring constant of about 20 N/mm.

[0078] The center hole 41 has an inner diameter slightly larger than the diameter of the collar shaft 21 of the collar 20. The center hole 41 is circular in a plan view and extends through the compression mesh 40 vertically.

[0079] In the present embodiment, the compression mesh 40 radially connecting the collar 20 and the grommet 30 has an outer diameter of 28 mm and an inner diameter of 12 mm. However, the diameter of the wires forming the compression mesh 40, the dimensions of the compression mesh 40, and the spring constant are not limited and may be set as appropriate. The compression mesh 40 with the performance described above may undergo no compression process.

[0080] The compression mesh 40 has, on its upper surface, a restriction ridge 43 extending along the circumference of a lower large-diameter portion 51 of the spiral spring 50 (described later). The restriction ridge 43 is circular in a plan view and protrudes upward.

[0081] As shown in an enlarged view of an area a in FIG. 2, the restriction ridge 43 protrudes upward from the surface of the compression mesh 40 with a smooth curve along the outer circumferential surface of the lower large-diameter portion 51 in a vertical cross section. In some embodiments, the restriction ridge 43 may be a separate member fixed on the surface of the compression mesh 40, or may have non-rounded corners in a vertical cross section.

[0082] The spiral spring 50 is formed from a wire having a circular cross section wound radially and upward to be spiral in a plan view and substantially truncated in a side view. The spiral spring 50 has diameters larger in lower portions than in upper portions. The lowermost portion having a larger diameter is referred to as the lower large-diameter portion 51, whereas the uppermost portion having a smaller diameter is referred to as an upper small-diameter portion 52.

[0083] More specifically, the spiral spring 50 has the lower large-diameter portion 51 corresponding substantially to one turn along the circumference at the lower end, the upper small-diameter portion 52 corresponding substantially to one turn along the circumference at the upper end, and an effective spring portion 53 between the lower large-diameter portion 51 and the upper small-diameter portion 52.

[0084] The lower large-diameter portion 51 and the upper small-diameter portion 52 are wound on a plane substantially perpendicular to the axial direction (vertical direction), or more specifically, on a horizontal plane. As described above, the lower large-diameter portion 51 extends along the inner circumference of the restriction ridge 43 on the upper surface of the compression mesh 40. The upper small-diameter portion 52 is less loosely fitted on the collar shaft 21 of the collar 20.

[0085] The equilibrium length of the spiral spring 50, or more specifically, the height of the spiral spring 50 under no load, that is, the vertical distance between the lower large-diameter portion 51 and the upper small-diameter portion 52, is greater than the distance between the flanges 22 on the collar 20 described above, or more specifically, the vertical height between the bottom surface of the upper flange 23 and the upper surface of the lower flange 24.

[0086] In the present embodiment, the spiral spring 50 with the above structure includes the lower large-diameter portion 51 with a diameter of 26 mm and the upper small-diameter portion 52 with a diameter of 10 mm. The effective spring portion 53 between the lower large-diameter portion 51 and the upper small-diameter portion 52 includes two turns. The spiral spring 50 is truncated in a side view and has a height (equilibrium length) of 6.6 mm under no load.

[0087] The diameters of the lower large-diameter portion 51 and the upper small-diameter portion 52, the number of turns included in the effective spring portion 53, and the height of the spiral spring 50 are not limited to the values described above, and may be determined to provide appropriate dimensions and an intended elastic force. The spring constant of the spiral spring 50 may be set to, but not limited to, about 0.5 N/mm, which is 1/40 to ½ of the spring constant of the compression mesh 40 (about 20 N/mm).

[0088] A method for assembling the shock absorber 10 including the collar 20, the grommet 30, the compression mesh 40, and the spiral spring 50 described above will now be described. The radially outer peripheral portion 42 of the compression mesh 40 is fixed to the second fixing section 32 of the grommet 30 with the connecting section 33 by swaging to fix the grommet 30 and the compression mesh 40 together.

[0089] As shown in FIG. 3, the spiral spring 50 is vertically overlaid on the compression mesh 40. From above the spiral spring 50 vertically overlaid on the compression mesh 40, the collar shaft 21 of the collar part 25 is placed through the opening defined by upper small-diameter portion 52 of the spiral spring 50 and through the center hole 41 in the compression mesh 40. The lower end of the collar shaft 21 is swaged in the fitting hole 24a in the lower flange 24 on the bottom surface of the compression mesh 40 to be integral with the lower flange 24. The compression mesh 40 may be fixed to the grommet 30 before or after the collar 20 is fixed to the compression mesh 40 and the spiral spring 50 vertically overlaid on each other.

[0090] In the structure including the collar 20 and the compression mesh 40 and the spiral spring 50 vertically overlaid on each other, the spiral spring 50 is vertically compressed with the upper small-diameter portion 52 restricted by the upper flange 23 at the top and tightly fitted on the collar shaft 21. In the present embodiment, the spiral spring 50 with a height of 6.6 mm under no load (equilibrium length) is attached in a manner compressed to have a vertical height of about 3 mm. The vertical height may be a different length.

[0091] The lower large-diameter portion 51 extends along the radially inner circumference of the restriction ridge 43 on the upper surface of the compression mesh 40, which is fixed to the grommet 30 with the radially outer peripheral portion 42 swaged to the second fixing section 32. The lower large-diameter portion 51 urges the compression mesh 40 downward. More specifically, as shown in FIG. 4, the lower large-diameter portion 51 extends along 55% of the radially inner circumference of the restriction ridge 43. The area of the lower large-diameter portion 51 circumferentially in contact with the restriction ridge 43 is referred to as a contact area X.

[0092] The shock absorber 10 assembled in the above manner is attached at a predetermined position on the heat insulator 1 to provide a shock absorber-attached heat insulator 1A.

[0093] More specifically, the shock absorber 10 is placed in an installation hole 101 (refer to FIG. 3) at a predetermined position on the heat insulator 1 to be the shock absorber-attached heat insulator 1A. The circumferential edge of the installation hole 101 and the first fixing section 31 are swaged together to fix the shock absorber 10 to the insulator base 100.

[0094] In FIG. 5, the insulator base 100 is flat. In some embodiments, the insulator base 100 may be corrugated. Although the shock absorber 10 is fixed on the flat insulator base 100 in FIG. 5, the insulator base 100 having the installation hole 101 at a predetermined position is first processed into the three-dimensional heat insulator 1, and then the installation hole 101, which is used to mount the heat insulator 1 onto the engine 2, receives the shock absorber 10 to form the shock absorber-attached heat insulator 1A.

[0095] As shown in FIG. 6, the shock absorber-attached heat insulator 1A with the above structure is mounted on the engine 2 for a vehicle, such as an automobile, to cover the exhaust manifold 3 that discharges a combustion exhaust gas.

[0096] More specifically, as shown in FIG. 7, the exhaust manifold 3 includes a boss 3a at a predetermined position determined in accordance with the vibration characteristics of the engine 2. The shock absorber 10 attached in the shock absorber-attached heat insulator 1A is placed on the boss 3a. The fastening bolt 110 is placed through the bolt hole 25a defined in the collar shaft 21 included in the shock absorber 10 and screwed onto the boss 3a in the exhaust manifold 3 for fastening.

[0097] In the shock absorber-attached heat insulator 1A fixed to the exhaust manifold 3 as described above, the vibration of the exhaust manifold 3 from driving the engine 2 is input to the collar 20 through the boss 3a. The compression mesh 40 and the spiral spring 50 located between the collar 20 and the grommet 30 damp vibration input through the collar 20, thus reducing vibration input to the heat insulator 1 through the grommet 30. In other words, the shock absorber 10 can damp vibration input from the exhaust manifold 3.

[0098] As described above, the shock absorber 10 for connecting the exhaust manifold 3 as a vibration source and the heat insulator 1 for covering the exhaust manifold 3 to absorb vibration from the exhaust manifold 3 to the heat insulator 1 includes the collar 20 including the substantially tubular collar shaft 21 to be fastened to the exhaust manifold 3 with the fastening bolt 110, and the annular flanges 22 protruding radially outward from the two axial ends of the collar shaft 21, the annular grommet 30 fixable to the heat insulator 1, the annular compression mesh 40 located between the collar 20 and the grommet 30 with the radially outer peripheral portion of the compression mesh 40 fixed to the grommet 30 and including a shock absorbing material, and the spiral spring 50 located between the upper flange 23 on the collar 20 and the compression mesh 40, and overlaid on the compression mesh 40. The compression mesh 40 has a center hole 41 loosely receiving the collar shaft 21 at least in the radial direction. The spiral spring 50 has a spring constant equal to or smaller than the spring constant of the compression mesh 40 and is spiral in a plan view. The compression mesh 40 includes the restriction ridge 43 along and in contact with the lower large-diameter portion 51 radially outward in the spiral spring 50 spiral in a plan view. The restriction ridge 43 restricts radial movement of the spiral spring 50 relative to the compression mesh 40. The spiral spring 50 has the lower large-diameter portion 51 in contact with 55% of the circumference of the restriction ridge 43, which falls within the range of 40% to 55%. The shock absorber 10 thus has higher vibration damping performance while reducing contact noise generated as the compression mesh 40 hits the collar 20.

[0099] In detail, the annular compression mesh 40 located between the collar 20 and the grommet 30 with the radially outer peripheral portion 42 fixed to the grommet 30 and including a shock absorbing material is axially bendable and thus deforms elastically. This reduces the vibration from the exhaust manifold 3 transmitted to the grommet 30 through the collar 20, thus reducing the vibration from the exhaust manifold 3 propagating to the heat insulator 1, or in other words, absorbing such vibration.

[0100] The center hole 41 in the compression mesh 40 loosely receives the collar shaft 21 at least in the radial direction. The compression mesh 40 thus moves at least radially relative to the collar 20 that vibrates as the exhaust manifold 3 vibrates. This structure can damp vibration, and reduces vibration propagating to the compression mesh 40.

[0101] The spiral spring 50 located between the upper flange 23 on the collar 20 and the compression mesh 40 and overlaid on the compression mesh 40 has a lower spring constant than the compression mesh 40. The elastically deformable spiral spring 50 thus absorbs at least radial movement of the compression mesh 40 relative to the vibrating collar 20 as described above. This reduces contact noise generated as the compression mesh 40 moves relative to the collar 20 under vibration propagating to the collar 20, without lowering the shock absorbing performance of the compression mesh 40.

[0102] The compression mesh 40 includes the restriction ridge 43 in contact with the lower large-diameter portion 51 radially outward in the spiral spring 50 spiral in a plan view. The contact area X of the lower large-diameter portion 51 with the restriction ridge 43 is in the range of 40% to 55%. In this structure, friction between the restriction ridge 43 and the lower large-diameter portion 51 further damps vibration input to the shock absorber 10, in addition to damping with the spiral spring 50.

[0103] A structure with the contact area X of the lower large-diameter portion 51 with the restriction ridge 43 less than 40% cannot have such friction between the restriction ridge 43 and the lower large-diameter portion 51 that allows damping described above, and may have substantially the same damping as obtained with the spiral spring 50 fixed to the compression mesh 40, or in other words, damping with the spiral spring 50 alone.

[0104] As described above, the structure with the circumferential contact area X of the lower large-diameter portion 51 with the restriction ridge 43 in a range of 40% to 55% provides further damping with friction between the restriction ridge 43 and the lower large-diameter portion 51, in addition to damping with the spiral spring 50. The shock absorber 10 can thus further damp input vibration, providing high vibration damping performance.

[0105] The restriction ridge 43 on the compression mesh 40 adjacent to the spiral spring 50 has an outwardly-curved cross section. The restriction ridge 43 can be formed easily to generate friction with the lower large-diameter portion 51 of the spiral spring 50, thus damping the vibration further.

[0106] In detail, the restriction ridge 43 having an outwardly-curved cross section and located on the compression mesh 40 adjacent to the spiral spring 50 reliably prevents radial movement of the spiral spring 50 relative to the compression mesh 40 and also reliably comes in contact with the lower large-diameter portion 51 to generate intended friction. The shock absorber 10 thus has increased damping, or more specifically, high vibration damping performance.

[0107] The compression mesh 40 includes metal wires knitted together. This increases friction between the restriction ridge 43 and the lower large-diameter portion 51 to further increase damping, thus providing the shock absorber 10 having higher vibration damping performance.

[0108] The spiral spring 50 is substantially truncated in a side view and has a larger diameter in a portion nearer the compression mesh 40 than in a portion nearer the upper flange 23. The spiral spring 50 thus axially compresses by a greater degree than a coil spring having the same diameter from the upper to lower ends. This structure provides space for movement of the compression mesh 40 relative to the collar 20 for deforming elastically and absorbing vibration, and reliably prevents the compression mesh 40 from lowering the absorbing performance.

[0109] This structure also prevents wire portions included in the spiral spring 50 from coming in contact with each other when the spiral spring 50, which is spiral in a plan view and substantially truncated in a side view, compresses under a load.

[0110] The spiral spring 50 is substantially truncated in a side view and has a height greater than the distance between the compression mesh 40 in contact with the lower flange 24 and the upper flange 23. The spiral spring 50 is attached in a manner compressed against the axial urging force, or in other words, the spiral spring 50 is attached in a prestressed manner. The spiral spring 50 thus reliably reduces contact noise generated as the compression mesh 40 hits the collar 20, and increases friction between the spiral spring 50 and the restriction ridge 43 in contact with each other, thus further improving damping of the shock absorber 10.

[0111] The spiral spring 50 has a spring constant of 0.5 N/mm, which is 1/40 to ½ of the spring constant of the compression mesh 40 (about 20 N/mm). This allows damping with friction between the restriction ridge 43 and the lower large-diameter portion 51.

[0112] In detail, when the spiral spring 50 has a spring constant smaller than 1/40 of the spring constant of the compression mesh 40, the compression mesh 40 mainly performs damping. This reduces friction between the restriction ridge 43 and the lower large-diameter portion 51, without providing sufficient damping with friction between the restriction ridge 43 and the lower large-diameter portion 51. When the spiral spring 50 has a spring constant larger than ½ of the spring constant of the compression mesh 40, the compression mesh 40 is mostly bent, without providing sufficient damping with friction between the restriction ridge 43 and the lower large-diameter portion 51. When the spiral spring 50 has a spring constant in a range of 1/40 to ½ (about 0.5 N/mm) of the spring constant of the compression mesh 40 (about 20 N/mm), the friction between the restriction ridge 43 and the lower large-diameter portion 51 provides sufficient damping.

[0113] The shock absorber 10 is attached to the heat insulator 1 for covering the exhaust manifold 3 to provide the shock absorber-attached heat insulator 1A. The shock absorber 10 absorbs vibration from the exhaust manifold 3 and prevents the heat insulator 1 from being a vibration source by resonating with the exhaust manifold 3. The shock absorber-attached heat insulator 1A reduces contact noise between the collar 20 and the compression mesh 40, and improves damping to provide high vibration damping performance.

[0114] Damping evaluation tests for damping achieved by the spiral spring 50 in the shock absorber 10 with the above advantageous effects will now be described with reference to FIGS. 9 to 12.

[0115] Under the test conditions shown in FIG. 12, test specimens each simulating the shock absorber-attached heat insulator 1A including three shock absorbers were used in the damping evaluation tests. The vibration of each specimen was measured under a predetermined vibration. The damping ratios were evaluated and compared.

[0116] The shock absorbers used in the tests include a shock absorber 10A (refer to FIG. 9(a)) replacing the compression mesh 40 with an annular iron plate 40a to which the lower large-diameter portion 51 of the spiral spring 50 is fixed, a shock absorber 10B (refer to FIG. 9(b)) including a compression mesh 40b with no restriction ridge 43, the shock absorber 10 described above (refer to FIG. 9(c)) having the circumferential contact area X of the lower large-diameter portion 51 with the restriction ridge 43 of 55% (corresponding to 190°), a shock absorber 10C (refer to FIG. 9(d)) with a contact area Xc of 51.7% (corresponding to 178°), a shock absorber 10D (refer to FIG. 10(a)) with a contact area Xd of 48.4% (corresponding to) 167°, a shock absorber 10E (refer to FIG. 10(b)) with a contact area Xe of 44.5% (corresponding to 153°), a shock absorber 10F (refer to FIG. 10(c)) with a contact area Xf of 40.3% (corresponding to 139°), a shock absorber 10G (refer to FIG. 10(d)) with a contact area Xg of 27.5% (corresponding to 95°), a shock absorber 10H (refer to FIG. 11(a)) with a contact area Xh of 62.7% (corresponding to 216°), and a shock absorber 10J (refer to FIG. 11(b)) with a contact area Xj of 68.75% (corresponding to 237°).

Table 1 shows the results.

TABLE-US-00001 TABLE 1 Shock absorber 10 10C 10D 10E 10F 10G 10H 10J 10A 10B (55%) (52%) (48%) (45%) (40%) (28%) (63%) (69%) Damping 0.18 0.27 0.35 0.3 0.32 0.32 0.22 0.18 0.19 0.19 ratio

[0117] The shock absorber 10A replacing the compression mesh 40 with the iron plate 40a to which the lower large-diameter portion 51 of the spiral spring 50 is fixed can yield the ratio of the radial damping provided by the spiral spring 50. The shock absorber 10B including the compression mesh 40b with no restriction ridge 43 can yield the damping ratio with no radial positional restriction by the restriction ridge 43. More specifically, the shock absorber 10B yields the damping ratio to be obtained when the spiral spring 50 overlaid on the compression mesh 40 absorbs the vertical vibration of the compression mesh 40 alone relative to the collar 20.

[0118] The results show that the shock absorbers 10G to 10J have substantially the same damping ratios as the shock absorber 10A under the conditions described above. This reveals that the contact area X of less than 40% provides no damping with friction between the restriction ridge 43 and the lower large-diameter portion 51 in contact with each other and the contact area X of greater than 55% does not provide sufficient damping due to the longer lower large-diameter portion 51 in contact with the restriction ridge 43.

[0119] In other words, the tests reveals that the contact area X in a range of 40% to 55%, or more specifically, the lower large-diameter portion 51 in contact with 40% to 55% of the circumference of the restriction ridge 43 provides damping with friction between the restriction ridge 43 and the lower large-diameter portion 51 in contact with each other.

[0120] The shock absorbers with the contact area X in a range of 45% to 55%, or more specifically, the shock absorber 10 and the shock absorbers 10C to 10E, provided more effective damping with friction between the restriction ridge 43 and the lower large-diameter portion 51 in contact with each other than the shock absorbers 10A and 10B. This reveals that the circumferential contact area X of the lower large-diameter portion 51 with the restriction ridge 43 may be in a range of 45% to 55% to provide intended damping.

[0121] The aspects of present invention correspond to the embodiment in the manner described below: the vibration member in the aspects of the invention corresponds to the exhaust manifold 3,

[0122] the covering member to the heat insulator 1,

[0123] the shock absorber to the shock absorber 10,

[0124] the fastener to the fastening bolt 110,

[0125] the collar shaft to the collar shaft 21,

[0126] the flange to the flange 22,

[0127] the collar to the collar 20,

[0128] the fixing member to the grommet 30,

[0129] the shock absorbing member to the compression mesh 40,

[0130] the spring to the spiral spring 50,

[0131] the radially outer portion to the lower large-diameter portion 51,

[0132] the movement restrictor and the movement restriction ridge each to the restriction ridge 43, and

[0133] the metal cover to the shock absorber-attached heat insulator 1A.

[0134] However, the aspects of the invention may be implemented in many embodiments other than the embodiments described above.

[0135] In the above embodiment, the lower large-diameter portion 51 is in contact with the restriction ridge 43. In some embodiments, the lower large-diameter portion 51 may be slightly apart from the restriction ridge 43 to immediately come in contact with the restriction ridge 43 under an external force applied radially. The restriction ridge 43 may be replaced with multiple restriction ridges 43 arranged at predetermined intervals to retain the contact area X in the range of 40% to 55% or specifically in the range of 45% to 55%, rather than extending continuously on the circumference.

[0136] Although the restriction ridge 43 described above is circular in a plan view, the restriction ridge 43 may be spiral in a plan view with a variable curvature, in accordance with the lower large-diameter portion 51 spiral in a plan view. The contact area X in this structure will be greater than the contact area X of the lower large-diameter portion 51 with the circular restriction ridge 43 in a plan view. This increases damping with friction between the restriction ridge 43 and the lower large-diameter portion 51.

[0137] However, the spiral lower large-diameter portion 51 and the spiral restriction ridge 43 in a plan view may be properly aligned to come in contact with each other to increase damping with friction. The spiral spring 50 is to be attached in a properly oriented manner with respect to the compression mesh 40. The compression mesh 40 and the spiral spring 50 attached in an improperly oriented manner may not provide intended damping. To allow any orientation of these components to provide predetermined damping, the circular restriction ridge 43 and the spiral lower large-diameter portion 51 in a plan view may be circumferentially in contact with each other to have the contact area X in a range of 40% to 55%, or specifically 45% to 55%.

[0138] In the above embodiment, the restriction ridge 43 having an outwardly-curved shape is on the surface of the compression mesh 40 as a restrictor for restricting radial movement of the lower large-diameter portion 51 of the spiral spring 50. As shown in FIG. 13, the restrictor may be of any of various shapes. FIG. 13 is a half cross-sectional view of shock absorbers 10X, 10Y, and 10Z.

[0139] In the shock absorber 10 in the above embodiment, the restriction ridge 43 on the surface of the compression mesh 40 is aligned along the radially outer surface of the lower large-diameter portion 51. As shown in FIG. 13(a), an inner restriction ridge 43X aligned along the radially inner surface of the lower large-diameter portion 51 may be on the surface of a compression mesh 40X.

[0140] In the shock absorber 10X including the compression mesh 40X, the inner restriction ridge 43X is in contact with the radially inner surface of the lower large-diameter portion 51. The inner restriction ridge 43X and the radially inner surface of the lower large-diameter portion 51 together generate friction to increase damping.

[0141] The shock absorber 10Y shown in FIG. 13(b) includes both the inner restriction ridge 43X and the restriction ridge 43 on the surface of the compression mesh 40 to hold the lower large-diameter portion 51 with the radially inner and outer surfaces. The lower large-diameter portion 51 is in contact with the inner restriction ridge 43X on its radially inner surface and with the restriction ridge 43 on its radially outer surface.

[0142] The shock absorber 10Y including the compression mesh 40Y can also further increase damping with friction between the inner restriction ridge 43X and the radially inner surface of the lower large-diameter portion 51 and friction between the restriction ridge 43 and the radially outer surface of the lower large-diameter portion 51.

[0143] The shock absorber 10Z shown in FIG. 13(c) may include a groove restrictor 43Z having a channel cross section on the surface of the compression mesh 40Z for receiving the lower large-diameter portion 51.

[0144] The lower large-diameter portion 51 is fitted in the groove restrictor 43Z having a channel cross section on the surface of the compression mesh 40Z. The lower large-diameter portion 51 in contact with the inner surfaces of the groove restrictor 43Z having a channel cross section generates friction to increase damping.

[0145] In this example, the radially outer surface of the lower large-diameter portion 51 may be in contact with the radially outward inner surface of the groove restrictor 43Z having a channel cross section as shown in FIG. 13(c), or the radially inner surface of the lower large-diameter portion 51 may be in contact with the radially inward inner surface of the groove restrictor 43Z having a channel cross section.

[0146] In another example, a separate restrictor may be fixed on the surface of the compression mesh 40, rather than the restriction ridge 43 on the compression mesh 40.

[0147] In the above embodiment, the spiral spring 50 spiral in a plan view has a spirally increasing height toward the center and is truncated as a whole in a side view, but may have a constant height, i.e., has a plane shape.

[0148] In the shock absorber 10 described above, the spiral spring 50 is located on the surface of the compression mesh 40 nearer the upper flange 23. In some embodiments, the spiral spring 50 may be located on the surface of the compression mesh 40 nearer the lower flange 24, or located on each surface of the compression mesh 40 nearer the upper flange 23 or nearer the lower flange 24.

[0149] The grommet 30 in the shock absorber 10 has the first fixing section 31, the connecting section 33, and the second fixing section 32 arranged in the stated order from above, and holds the compression mesh 40 and the heat insulator 1 vertically in this order from where the exhaust manifold 3 is located. However, the grommet 30 may have the second fixing section 32, the connecting section 33, and the first fixing section 31 arranged in this order from above, and may hold the heat insulator 1 and the compression mesh 40 vertically in this order from where the exhaust manifold 3 is located.

[0150] In this case as well, the spiral spring 50 may be located on the surface of the compression mesh 40 nearer the upper flange 23 or on the surface nearer the lower flange 24, or on each surface nearer the upper flange 23 or nearer the lower flange 24. Also, the spiral spring 50 may have a flat shape in a side view.

REFERENCE SIGNS LIST

[0151] 1 heat insulator [0152] 1A shock absorber-attached heat insulator [0153] 3 exhaust manifold [0154] 10 shock absorber [0155] 20 collar [0156] 21 collar shaft [0157] 22 flange [0158] 30 grommet [0159] 40 compression mesh [0160] 43 restriction ridge [0161] 50 spiral spring [0162] 51 lower large-diameter portion [0163] 110 fastening bolt