Torsional Vibration Damper with Axially Compressed Spring
20230092982 · 2023-03-23
Assignee
Inventors
Cpc classification
F16H2055/366
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
The invention discloses a novel method for constructing a torsional vibration damper where the spring damper system is aligned axially with the axis of the device, and it is put into compression by axially reducing its width and simultaneously preventing radial expansion. The assembly of the torsional vibration damper occurs in two progressive controlled stages by torquing a set of fasteners, thereby minimizing the shear strain on the elastomer during assembly, enhancing structural robustness, modally stability, and serviceability in the field.
Claims
1. A torsional vibration damper comprising: a compound hub further comprising: a first part further comprising: a first axis-symmetric surface bounding its radially distal periphery; a second axis-symmetric surface adjacent to the first axis-symmetric surface extending radially outward and bounding its axial periphery; and a plurality of axially oriented through holes; a second part further comprising: a third axis-symmetric surface bounding its radially distal periphery; a fourth axis-symmetric surface adjacent to the third axis-symmetric surface extending radially outward and bounding its axial periphery and opposing the second axis-symmetric surface; and a plurality of axially oriented threaded holes aligned with, and axially opposed to, the plurality of axially oriented holes in the first part of the hub; a monolithic ring positioned radially outward to the hub further comprising: a first axis-symmetric surface bounding its radially proximate periphery that is parallel to the compound surface created by the first and the third surfaces of the first and second part of the hub respectively after assembly; a monolithic spring positioned centrally between the hub and the ring further comprising: a first axis-symmetric surface bounding its radially proximate periphery; a second axis-symmetric surface bounding its radially distal periphery; a third axis-symmetric surface bounding its axial periphery and adjacent to the first and second surfaces; and a fourth axis-symmetric surface bounding its axial periphery adjacent to the first and second surfaces, and opposing the third surface; a plurality of bolts that pass through the plurality of holes in the first part of the hub and engage with the plurality of threaded holes in the second part of the hub; wherein partial torquing of the plurality of the bolts causes the first and second parts of the hub to come axially closer to each other thereby partially compressing the centrally positioned spring when the second and fourth surfaces of the first and second part of the hub push against the third and fourth surfaces of the spring respectively, and the first and third surfaces of the of the first and second part hub radially restrict the inward expansion of the spring forcing it to expand radially outward such that the deformed second surface of the spring forms a slip fit with the first surface of the ring; and the complete torquing of the plurality of bolts causes the first and second parts of the hub to come into mutual contact and axially compress the centrally positioned spring when the second and fourth surfaces of the first and second part of the hub push against the third and fourth surfaces of the spring respectively, and the first and third surfaces of the hub and the first surface of the ring restrict the radial expansion of the first and second axis-symmetric surfaces of the spring thereby causing it to compress and occupy the compound partially enclosed channel defined by the first, second, third, and fourth surfaces of the first and second part of the hub respectively and the first surface of the ring.
2. The torsional vibration damper of claim 1 where the spring is replaced by a compound spring comprising of two or more separate sections.
3. The torsional vibration damper of claim 1 where the first surface of the ring is not parallel to the compound surface created by the first and the third surfaces of the first and second part of the hub respectively after assembly.
4. The torsional vibration damper of claim 1 where the second part of the hub has a plurality of holes centered around each a plurality of nuts is rigidly attached for receiving the bolts that pass through the plurality of holes in the first and second parts of the hub respectively.
5. The torsional vibration damper of claim 1 where the ring is positioned radially proximate to the hub.
6. A torsional vibration damper comprising: a compound ring further comprising: a first part further comprising: a first axis-symmetric surface bounding its radially proximate periphery; a second axis-symmetric surface adjacent to the first axis-symmetric surface extending radially inward bounding its axial periphery; and a plurality of axially oriented through holes; a second part further comprising: a third axis-symmetric surface bounding its radially proximate periphery; a fourth axis-symmetric surface adjacent to the third axis-symmetric surface extending radially inward bounding its axial periphery and opposing the second axis-symmetric surface; and a plurality of axially oriented threaded holes aligned with, and axially opposed to, the plurality of axially oriented holes in the first part of the ring; a monolithic hub positioned radially inward to the ring further comprising: a first axis-symmetric surface bounding its radially distal periphery that is parallel to the compound surface created by the first and the third surfaces of the first and second part of the ring respectively after assembly; a monolithic spring positioned centrally between the hub and the ring further comprising: a first axis-symmetric surface bounding its radially proximate periphery; a second axis-symmetric surface bounding its radially distal periphery; a third axis-symmetric surface bounding its axial periphery and adjacent to the first and second surfaces; and a fourth axis-symmetric surface bounding its axial periphery adjacent to the first and second surfaces, and opposing the third surface; a plurality of bolts that pass through the plurality of holes in the first part of the ring and engage with the plurality of threaded holes in the second part of the ring; wherein partial torquing of the plurality of the bolts causes the first and second parts of the ring to come axially closer to each other thereby partially compressing the centrally positioned spring when the second and fourth surfaces of the first and second part of the ring push against the third and fourth surfaces of the spring respectively, and the first and third surfaces of the first and second part of the ring radially restrict the outward expansion of the spring forcing it to expand radially inward such that the deformed first surface of the spring forms a slip fit with the first surface of the hub; and the complete torquing of the plurality of bolts causes the first and second parts of the ring to come into mutual contact and axially compress the centrally positioned spring when the second and fourth surfaces of the first and second part of the ring push against the third and fourth surfaces of the spring respectively, and the first and third surfaces of the ring and the first surface of the hub restrict the radial expansion of the first and second axis-symmetric surfaces of the spring thereby causing it to compress and occupy the compound partially enclosed channel defined by the first, second, third, and fourth surfaces of the first and second part of the ring respectively and the first surface of the hub.
7. The torsional vibration damper of claim 6 where the spring is replaced by a compound spring comprising of two or more separate sections.
8. The torsional vibration damper of claim 6 where the first surface of the hub is not parallel to the compound surface created by the first and the third surfaces of the first and second part of the respectively after assembly.
9. The torsional vibration damper of claim 6 where the ring is positioned radially proximate to the hub.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
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[0032] In stage 1 of the assembly process, part 1c is placed on a horizontal surface followed by slipping the spring 3c over the half channel defined by surface 11c and surface 12c that support spring 3c axially and radially respectively. Spring 3c is designed such that it diametrically slips over the partial channel defined by surface 12c and rests on surface 11c in the unassembled position. Part 1c′ is then slipped under spring 3c such that it axially opposes part 1c and surface 11c′ and surface 12c′ support spring 3c axially and radially respectively. The plurality of bolts 4c are chosen such that their length is sufficient to pass through the plurality of through holes 5c and 5c′ and engage with the threads of the plurality of welded nuts 6c. The plurality of bolts 4c are partially torqued to a pre-determined value such that outermost diametric surface of spring 3c can slip under the entirety of surface 21c of ring 2c. The ring 2c is then slipped over spring 3c such that it aligns axially with the compound hub subassembly. This concludes stage 1 of the assembly process.
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[0035] In stage 1 of the assembly process, part 2e is placed on a horizontal surface followed by slipping the spring 3e under the partial channel defined by surface 21e and surface 22e that support spring 3e axially and radially respectively. Spring 3e is designed such that it diametrically slips over the partial channel defined by surface 21e and rests on surface 21e in the unassembled position. Part 2e′ is then slipped over spring 3e such that it axially opposes part 2e and side wall 21e′ and bottom wall 22e′ support spring 3e axially and radially respectively. The plurality of bolts 4e are chosen such that their length is sufficient to pass through the plurality of through holes 5e′ and engage with the threads in the plurality of holes 5e. The plurality of bolts 4e are partially torqued to a pre-determined value such that innermost diametric surface of spring 3e slips over the entirety of surface 11e of hub 1e. The hub 1e is then slipped under spring 3e such that it aligns axially with the compound ring subassembly. This concludes the stage 1 of the assembly process.
[0036] In stage 2 of the assembly process, the plurality of bolts 4e are fully torqued to a predetermined value such that parts 1d and 1d′ come into mutual contact with each other and a compound channel is formed by surface 21e and 21e′ and surface 22e and 22e′. The spring 3e is compressed axially by surfaces 21e and 21e′ and is simultaneously not allowed to expand radially outward by surfaces 22e and 22e′ respectively. Spring 3e is thereby forced to expand radially inward and clamp on surface 11e of hub 1e. The hub surface 11e and compound surface defined by 22e and 22e′ are designed with a geometric configuration that allows hub 1d to self-center axially and radially with respect to the compound ring formed by parts 2e, 2e′ after stage 2 of the assembly.
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[0042] The advantages yielded by the invention over the illustrated prior art stems from the novel method of compressing the spring by reducing its axial width as opposed to its radial thickness. This allows the construction of an axially oriented TVD that: (1) minimizes shear strain on the spring during assembly, thereby putting the spring into compression without damaging it structurally; (2) increases the volume of the spring thereby enhancing its structural robustness to undertake greater shear stress and improve power dissipation; (3) force the first mode-shape of the TVD to be torsional in nature and adequately decouples the modal frequencies therefore enhancing NVH response; and (4) Allows the damper to be serviced in the filed if/when the spring fails by merely loosening the bolts, separating the metallic components, replacing the damaged spring with a new spring, and reassembling the TVD without disengaging the hub from the rotating shaft, and consequently reducing machine downtime and eliminating unnecessary expense of replacing the hub and the ring.