This invention relates to torsional vibration dampers. In particular, this invention relates to apparatus for tuning tubular torsional viscous dampers.
U.S. Pat. No. 10,837,497 (Hauptmann et al.) describes a torsional viscous damper having an inertial mass in the form of a tubular member that is applicable for removing destructive torsional vibration in power transmitting shaft assemblies (a “tube-type” damper). A viscous fluid contained between the inertial mass and its outer housing is sheared, thereby producing frictional heat which is dissipated to the ambient surroundings. The torsional vibration energy is thereby removed, resulting in a corresponding reduction in torsional vibration amplitudes.
U.S. Pat. No. 4,160,390 (Spaetgens) discloses an apparatus for tuning a conventional, “disc-type” damper, wherein an inertial disc is connected to a surrounding housing with an elastic (spring) member. Spaetgens also mentions the possibility of additional tuning through an elastic connection between the damper housing and a hub attached to the driveshaft. However, Spaetgens is silent as to how this additional (hub-to-housing) tuning is to be accomplished.
There is a general desire for apparatus and methods for tuning torsional viscous dampers such as those disclosed in Hauptmann et al., for example.
The foregoing examples of the related art and limitations related thereto are intended to be illustrative and not exclusive. Other limitations of the related art will become apparent to those of skill in the art upon a reading of the specification and a study of the drawings.
The following embodiments and aspects thereof are described and illustrated in conjunction with systems, tools and methods which are meant to be exemplary and illustrative, not limiting in scope. In various embodiments, one or more of the above-described problems have been reduced or eliminated, while other embodiments are directed to other improvements.
One aspect of the invention provides a vibration absorber apparatus for a mechanical system comprising a rotating machine part. The vibration absorber apparatus comprises a tube-type torsional damper that is attached, by a hub, to the rotating machine part for rotation with the machine part about an axis of rotation, the tube-type torsional damper having a housing that is spaced apart radially from the axis, that extends circumferentially around the axis and that has a longitudinal extension having a dimension L in a longitudinal direction parallel to the axis, at least one elastic member connecting the hub to the housing for tuning the tube-type torsional damper, wherein the at least one elastic member has an effective torsional stiffness kT given by kT=(ω11)2J, where J is an overall polar moment of inertia of the tube-type torsional damper and ω11 is a resonant frequency of the mechanical system.
The at least one elastic member may comprise a disc-shaped member that extends around the axis and is disposed between, and connected to, the hub and the housing.
The disc-shaped member may be shaped to define a plurality of cut-outs, the plurality of cut-outs having the same shape, equally sized, equally radially spaced apart from the axis and equally angularly spaced apart from one another about the axis.
The disc-shaped member may be shaped to define a second plurality of cut-outs, the second plurality of cut-outs having the same shape, equally sized, equally radially spaced apart from the axis and equally angularly spaced apart from one another about the axis. The second plurality of cut-outs may have a size that is different from that of the plurality of cut-outs. The second plurality of cut-outs may have a shape that is different from that of the plurality of cut-outs. The angular spacing between the second plurality of cut-outs may be different than the angular spacing between the plurality of cut-outs. The radial spacing from the axis of the second plurality of cut-outs may be different than the radial spacing from the axis of the plurality of cut-outs.
The at least one elastic member may comprise a plurality of disc-shaped members, each disc-shaped member extending around the axis and disposed between, and connected to, the hub and the housing.
The plurality of disc-shaped members may be spaced apart from one another in the longitudinal direction.
A spacing in the longitudinal direction between an adjacent pair of the plurality of disc-shaped members may be less than the dimension L of the housing in the longitudinal direction.
The plurality of disc-shaped members may be identical to one other.
The disc-shaped member may be shaped to define one or more cut-outs with a spiral shape about the axis.
The at least one elastic member may comprise a plurality of spokes that are angularly spaced apart from one another about the axis and that extend between, and are connected to, the hub and the housing.
Each of the plurality of spokes may extend in a radial direction relative to the axis from the hub to the housing.
The spokes may be removably connected to the hub and to the housing.
The spokes may have dimensions in the longitudinal direction that are at least five times their arcuate dimension about the axis.
The spokes may have a serpentine shape as they extend between the hub and the housing.
The at least one elastic member may comprise a second plurality of spokes that are angularly spaced apart from one another about the axis and that extend between, and are connected to, the hub and the housing. The second plurality of spokes may be spaced apart from the plurality of spokes in the longitudinal direction. The plurality of spokes and the second plurality of spokes may be identical.
The at least one elastic member may be shaped to connect to the hub and to the housing at locations that are spaced apart in the longitudinal direction from one another.
The at least one elastic member may comprise one or more hub-coupling members connected to the hub at a first longitudinal direction location, one or more housing-coupling members connected to the housing at a second longitudinal direction location that is spaced apart in the longitudinal direction from the first longitudinal direction location, and a plurality of longitudinally-extending elastic members that extend between, and are connected to, the one or more hub-coupling members and the one or more housing-coupling members.
The plurality of longitudinally-extending elastic members may extend in longitudinal directions between the one or more hub-coupling members and the one or more housing-coupling members.
A torsional stiffness of the one or more hub-coupling members may be at least 10 times a torsional stiffness of the plurality of second elastic members. A torsional stiffness of the one or more housing-coupling members may be at least 10 times a torsional stiffness of the plurality of second elastic members.
The one or more hub-coupling members may comprise a plurality of spokes that are angularly spaced apart from one another about the axis and that extend from the hub in directions that have a directional component that is radial relative to the axis.
The plurality of longitudinally-extending elastic members may be connected to a corresponding one of the spokes at a location that is spaced apart from the hub in a radial direction relative to the axis.
The one or more hub-coupling members may comprise a hub-coupling ring that extends around the axis at a location that is spaced apart from the hub in a radial direction relative to the axis.
Each of the plurality of longitudinally-extending elastic members may be connected to the hub-coupling ring at a location that is spaced apart from the hub in a radial direction relative to the axis.
The one or more hub-coupling members may comprise a disc-shaped member that extends from the hub in radial directions relative to the axis.
The one or more housing-coupling members may comprise a housing-coupling ring that extends around the axis at a location that is spaced apart from the axis in a radial direction.
The at least one elastic member may comprise one or more hub-coupling members connected to the hub at a first longitudinal direction location, one or more housing-coupling members connected to the housing at a second longitudinal direction location that is spaced apart in the longitudinal direction from the first longitudinal direction location, the one or more hub-coupling members comprising a plurality of hub arms extending from the first longitudinal direction location in a first longitudinal direction, the plurality of hub arms equally angularly spaced apart from one another about the axis, the one or more housing-coupling members comprising a plurality of housing arms extending from the second longitudinal direction location in in a second longitudinal direction, the second longitudinal direction opposed to the first longitudinal direction, the plurality of housing arms equally angularly spaced apart from one another about the axis and wherein each housing arm is located at an angular location about the axis that is between a pair of hub arms, and a plurality of coil springs that extend in arcuate directions about the axis, each coil spring extending between a corresponding one of the plurality of hub arms and a corresponding one of the of the plurality of housing arms.
A torsional stiffness of the one or more hub-coupling members may be at least 10 times a torsional stiffness of the plurality of coil springs. A torsional stiffness of the one or more housing-coupling members may be at least 10 times a torsional stiffness of the plurality of coil springs.
The one or more hub-coupling members may comprise a plurality of spokes that are angularly spaced apart from one another about the axis and that extend from the hub in directions that have a directional component that is radial relative to the axis.
The plurality of hub arms may be connected to a corresponding one of the spokes at a location that is spaced apart from the hub in a radial direction relative to the axis.
The one or more hub-coupling members may comprise a hub-coupling ring that extends around the axis at a location that is spaced apart from the hub in a radial direction relative to the axis.
The plurality of hub arms may be connected to the hub-coupling ring at a location that is spaced apart from the hub in a radial direction relative to the axis.
The one or more hub-coupling members may comprise a disc-shaped member that extends from the hub in radial directions relative to the axis.
The one or more housing-coupling members may comprise a housing-coupling ring that extends around the axis at a location that is spaced apart from the axis in a radial direction.
Another aspect of the invention provides a vibration absorber apparatus for a mechanical system comprising a rotating machine part. The vibration absorber apparatus comprises a tube-type torsional damper that is attached, by a hub, to the rotating machine part for rotation with the machine part about an axis of rotation, the tube-type torsional damper having a housing that is spaced apart radially from the axis, that extends circumferentially around the axis and that has a longitudinal extension having a dimension L in a longitudinal direction parallel to the axis, at least one elastic member connecting the hub to the housing for tuning the tube-type torsional damper, the at least one elastic member shaped to connect to the hub and to the housing at locations that are spaced apart in the longitudinal direction from one another.
The at least one elastic member may comprise one or more hub-coupling members connected to the hub at a first longitudinal direction location, one or more housing-coupling members connected to the housing at a second longitudinal direction location that is spaced apart in the longitudinal direction from the first longitudinal direction location, and a plurality of longitudinally-extending elastic members that extend between, and are connected to, the one or more hub-coupling members and the one or more housing-coupling members.
The plurality of longitudinally-extending elastic members may extend in longitudinal directions between the one or more hub-coupling members and the one or more housing-coupling members.
A torsional stiffness of the one or more hub-coupling members may be at least 10 times a torsional stiffness of the plurality of longitudinally-extending elastic members. A torsional stiffness of the one or more housing-coupling members may be at least 10 times a torsional stiffness of the plurality of longitudinally-extending elastic members.
The one or more hub-coupling members may comprise a plurality of spokes that are angularly spaced apart from one another about the axis and that extend from the hub in directions that have a directional component that is radial relative to the axis.
The plurality of longitudinally-extending elastic members may be connected to a corresponding one of the spokes at a location that is spaced apart from the hub in a radial direction relative to the axis.
The one or more hub-coupling members may comprise a hub-coupling ring that extends around the axis at a location that is spaced apart from the hub in a radial direction relative to the axis.
Each of the plurality of longitudinally-extending elastic members may be connected to the hub-coupling ring at a location that is spaced apart from the hub in a radial direction relative to the axis.
The one or more hub-coupling members may comprise a disc-shaped member that extends from the hub in radial directions relative to the axis.
The one or more housing-coupling members may comprise a housing-coupling ring that extends around the axis at a location that is spaced apart from the axis in a radial direction.
Another aspect of the invention provides a method for damping vibrations in a mechanical system comprising a rotating machine part. The method comprises providing a tube-type torsional damper that is attached, by a hub, to the rotating machine part for rotation with the machine part about an axis of rotation, the tube-type torsional damper having a housing that is spaced apart radially from the axis, that extends circumferentially around the axis and that has a longitudinal extension having a dimension L in a longitudinal direction parallel to the axis, connecting at least one elastic member to the hub and to the housing, wherein the at least one elastic member has an effective torsional stiffness kT given by kT=(ω11)2J, where J is an overall polar moment of inertia of the tube-type torsional damper and ω11 is a resonant frequency of the mechanical system.
The method may comprise method steps or features corresponding to any of the features recited above or elsewhere herein.
Another aspect of the invention provides a method for damping vibrations in a mechanical system comprising a rotating machine part. The method comprises providing a tube-type torsional damper that is attached, by a hub, to the rotating machine part for rotation with the machine part about an axis of rotation, the tube-type torsional damper having a housing that is spaced apart from the axis, that extends circumferentially around the axis and that has a longitudinal extension having a dimension L in a longitudinal direction parallel to the axis, connecting at least one elastic member to the hub and to the housing, wherein connecting the at least one elastic member to the hub and to the housing comprises connecting the at least one elastic member to the hub and to the housing at locations that are spaced apart in the longitudinal direction from one another.
The method may comprise method steps or features corresponding to any of the features recited above or elsewhere herein.
In addition to the exemplary aspects and embodiments described above, further aspects and embodiments will become apparent by reference to the drawings and by study of the following detailed descriptions. It is emphasized that the invention relates to all combinations and sub-combinations of the above features and other features described herein, even if these are recited in different claims or claims with different dependencies.
Exemplary embodiments are illustrated in referenced figures of the drawings. It is intended that the embodiments and figures disclosed herein are to be considered illustrative rather than restrictive.
Throughout the following description specific details are set forth in order to provide a more thorough understanding to persons skilled in the art. However, well known elements may not have been shown or described in detail to avoid unnecessarily obscuring the disclosure. Accordingly, the description and drawings are to be regarded in an illustrative, rather than a restrictive, sense.
It is known generally to tune and to damp rotational systems to address vibration.
Looking more closely at
The inventors have determined that using the principles of tuning out problematic natural frequencies might also be used to improve the performance of “tube” type dampers, such as those described in U.S. Pat. No. 10,837,497 (Hauptmann et al.), which is hereby incorporated herein by reference.
Referring to
Inertia tube 16 is concentric with and rotatable about axis of rotation 13A and extends longitudinally (in direction 13) along axis of rotation 13A. Inertia tube 16 is viscously coupled to rotate with housing 12.
Inertia tube 16 may be characterized by one or more of the following:
Referring to
The clearance between inertia tube 16 and each of inner housing part 22 and outer housing part 24 forms inner and outer gaps 18a and 18b respectively. When viscous damper 10 is assembled, inner and outer gaps 18a and 18b are filled with a viscous fluid, such as siloxane, silicone and/or the like. Seals, such as O-rings 30, retain the fluid. For example, O-rings 30 fit into slots between inner and outer housing parts 22, 24 and end cap 20a and between inner and outer housing parts 22, 24 and end cap 20b. O-rings 30 assist in preventing leaking of high-viscosity fluid from between end caps 20a, 20b and housing parts 22, 24. Bearings 40a and 40b may be provided between the axial ends of inertia tube 16 and respective end caps 20a, 20b.
Aspect of various embodiments of the invention provide vibration absorbers comprising tube-type dampers like tube-type damper 10 (of
Vibration absorbers 100, 200 may be “tuned” (i.e. to provide tuning to tube-type damper 10) in a manner which is not contemplated in previous tube-type damper designs.
In particular embodiments, vibration absorbers 100, 200 are tuned by designing their corresponding elastic members 104, 204 to have an effective (combined) torsional stiffness kT [Nm/rad] given by:
k
T=(ω11)2J (1)
where J [kgm2] is an overall polar moment of inertia of tube-type torsional damper 10 and ω11 is the problematic or resonant frequency of the mechanical system (absent vibration absorber 100, 200). As discussed above in connection with
In general, the combined torsional stiffness kT of the one or more elastic members 104, 204 of vibration absorbers 100, 200 can be controlled to meet the equation (1) criteria by varying a number of physical parameters, such as: the material composition (and corresponding elasticity) of elastic members 104, 204, the physical dimensions of (and corresponding elasticity) of elastic members 104, 204, locations of elastic members 104, 204, spacing between elastic members 104, 204, a number of elastic members 104, 204 and/or the like. For example, in the case of the
In general, for higher values of the problematic torsional frequency ω11, it will be recognized that elastic members 104, 204 of vibration absorbers 100, 200 must have a higher torsional stiffness kT in accordance with the equation (1) relationship described above. In addition to torsional stiffness (kT), another mechanical design factor to be considered is the working stress in elastic members 104, 204. The stiffness and working stress level are opposing design objectives; stiffer elastic members 104, 204 will generally experience lower working stresses, while lower stiffness elastic members 104, 204 will generally experience higher working stresses. Designing elastic members 104, 204 to have low stiffness while carrying low or moderate working stresses presents a design challenge.
To illustrate these design challenges, consider vibration absorbers 200, 200B shown in
Many modern, high-speed reciprocating compressors have problematic natural frequencies, typically in the 50 to 80 Hz range. The above-discussed vibration absorbers 100, 200, 300, 400 having elastic members with the desired (equation (1)) torsional stiffness kt to dampen these problematic natural frequencies, that is, relatively low torsional stiffness kt, would be correspondingly highly stressed. Elastic members 104, 204, 304, 404 of vibration absorbers 100, 200, 300, 400 extend between hub 102 and housing 12 in predominantly the radial direction. That is, connection of elastic members 104, 204, 304, 4040 to hub 102 and to housing 12 is substantially planar. However, tube-type dampers 10 have a longitudinal-direction length L (see
As described above, some embodiments may comprise a plurality of elastic members of the types described above which may be spaced apart from (and/or abutting against) one another along axial/longitudinal direction 13 (e.g. along the length L of tube-type damper 10).
In some embodiments, hub coupling ring 506 may be omitted and cantilever spring elements (longitudinally-extending elastic members) 508 may extend in longitudinal directions 13 (or with directional components that extend in longitudinal directions 13) directly from each of the stiffened spokes 507A. Housing-coupling component(s) (e.g. housing-coupling) ring 510 may be mounted to an interior surface 15 of housing 12 as shown in the illustrated embodiment. In other embodiments, housing-coupling component(s) 510 may be mounted to an outer surface 17 of housing 12 or to a longitudinally-facing edge 19 of housing 12. In these other embodiments, the location at which elastic member 504 is mounted or connected to hub 102 is spaced apart (in longitudinal direction 13) from the location at which elastic member 504 is mounted or connected to housing 12 of tube type damper 10.
In some embodiments, longitudinally-extending cantilever spring elements (longitudinally-extending elastic members) 508 are thin strips. In some embodiments, longitudinally-extending cantilever spring elements 508 are circular rods. Cantilever spring elements 508 may be metallic or another material with suitable elastic properties. The material composition, physical dimensions, cross-sectional shape, angular spacing, number and/or the like of the cantilever spring elements 508 may be selected to tune elastic member 504 to the desired (equation (1)) torsional stiffness kt while also ensuring the working stress is not undesirably high. Hub 102, spokes 507A, hub-coupling ring 506 and housing-coupling ring 510 may be significantly stiffer than the cantilever spring elements (longitudinally-extending elastic members) 508 so as to ensure low working stresses in these stiffer components. For example, the stiffness of hub 102, spokes 507A, hub coupling ring 506 and housing coupling ring 510 may be 10 times or 100 times higher than the stiffness of the cantilever spring elements 508. In other respects, vibration absorber 500 of
In summary, the invention provides apparatus comprising elastic members for tuning tube-type torsional viscous dampers to improve the ability of the tube-type damper to reduce problematic torsional vibrations. The torsional stiffness of the elastic members is selected, as shown in the exemplary embodiments described above, to meet the equation (1) design criteria.
Those of skill in the art will appreciate that a variety of means are described for tuning a torsional viscous damper of the tube-type in order to improve its ability to reduce problematic torsional vibrations. The torsional stiffness kT of the hub-to-housing connection can be arranged as described herein to satisfy this relationship between the frequency ω11 to be removed and the polar moment of inertia J of the stated housing and damper assembly.
Unless the context clearly requires otherwise, throughout the description and the claims:
Words that indicate directions such as “vertical”, “transverse”, “horizontal”, “upward”, “downward”, “forward”, “backward”, “inward”, “outward”, “left”, “right”, “front”, “back”, “top”, “bottom”, “below”, “above”, “under”, and the like, used in this description and any accompanying claims (where present), depend on the specific orientation of the apparatus described and illustrated. The subject matter described herein may assume various alternative orientations. Accordingly, these directional terms are not strictly defined and should not be interpreted narrowly.
Where a component (e.g. a hub, assembly, assembly, shaft, device, etc.) is referred to above, unless otherwise indicated, reference to that component (including a reference to a “means”) should be interpreted as including as equivalents of that component any component which performs the function of the described component (i.e., that is functionally equivalent), including components which are not structurally equivalent to the disclosed structure which performs the function in the illustrated exemplary embodiments of the invention.
Specific examples of systems, methods and apparatus have been described herein for purposes of illustration. These are only examples. The technology provided herein can be applied to systems other than the example systems described above. Many alterations, modifications, additions, omissions, and permutations are possible within the practice of this invention. This invention includes variations on described embodiments that would be apparent to the skilled addressee, including variations obtained by: replacing features, elements and/or acts with equivalent features, elements and/or acts; mixing and matching of features, elements and/or acts from different embodiments; combining features, elements and/or acts from embodiments as described herein with features, elements and/or acts of other technology; and/or omitting combining features, elements and/or acts from described embodiments.
It is therefore intended that the following appended claims and claims hereafter introduced are interpreted to include all such modifications, permutations, additions, omissions, and sub-combinations as may reasonably be inferred. The scope of the claims should not be limited by the preferred embodiments set forth in the examples, but should be given the broadest interpretation consistent with the description as a whole.
1. A vibration absorber apparatus for a mechanical system comprising a rotating machine part, the vibration absorber apparatus comprising:
2. The apparatus of aspect 1 or any other aspect herein wherein the at least one elastic member comprises a disc-shaped member that extends around the axis and is disposed between, and connected to, the hub and the housing.
3. The apparatus of aspect 2 or any other aspect herein wherein the disc-shaped member is shaped to define a plurality of cut-outs, the plurality of cut-outs having the same shape, equally sized, equally radially spaced apart from the axis and equally angularly spaced apart from one another about the axis.
4. The apparatus of aspect 3 or any other aspect herein wherein the disc-shaped member is shaped to define a second plurality of cut-outs, the second plurality of cut-outs having the same shape, equally sized, equally radially spaced apart from the axis and equally angularly spaced apart from one another about the axis.
5. The apparatus of aspect 4 or any other aspect herein wherein the second plurality of cut-outs has a size that is different from that of the plurality of cut-outs.
6. The apparatus of any one of aspects 4 and 5 or any other aspect herein wherein the second plurality of cut-outs has a shape that is different from that of the plurality of cut-outs.
7. The apparatus of any one of aspects 4 to 6 or any other aspect herein wherein the angular spacing between the second plurality of cut-outs is different than the angular spacing between the plurality of cut-outs.
8. The apparatus of any one of aspects 4 to 7 or any other aspect herein wherein the radial spacing from the axis of the second plurality of cut-outs is different than the radial spacing from the axis of the plurality of cut-outs.
9. The apparatus of any one of aspects 2 to 8 or any other aspect herein wherein the at least one elastic member comprises a plurality of disc-shaped members, each disc-shaped member extending around the axis and disposed between, and connected to, the hub and the housing.
10. The apparatus of aspect 9 or any other aspect herein wherein the plurality of disc-shaped members are spaced apart from one another in the longitudinal direction.
11. The apparatus of aspect 10 or any other aspect herein wherein a spacing in the longitudinal direction between an adjacent pair of the plurality of disc-shaped members is less than the dimension L of the housing in the longitudinal direction.
12. The apparatus of any one of aspects 9 to 11 or any other aspect herein wherein the plurality of disc-shaped members are identical to one other.
13. The apparatus of aspect 2 or any other aspect herein wherein the disc-shaped member is shaped to define one or more cut-outs with a spiral shape about the axis.
14. The apparatus of any one of aspects 1 to 13 or any other aspect herein wherein the at least one elastic member comprises a plurality of spokes that are angularly spaced apart from one another about the axis and that extend between, and are connected to, the hub and the housing.
15. The apparatus of aspect 14 or any other aspect herein wherein each of the plurality of spokes extends in a radial direction relative to the axis from the hub to the housing.
16. The apparatus of any one of aspects 14 to 15 or any other aspect herein wherein the spokes are removably connected to the hub and to the housing.
17. The apparatus of any one of aspects 14 to 16 or any other aspect herein wherein the spokes have dimensions in the longitudinal direction that are at least five times their arcuate dimension about the axis.
18. The apparatus of any one of aspects 14 to 17 or any other aspect herein wherein the spokes have a serpentine shape as they extend between the hub and the housing.
19. The apparatus of any one of aspects 14 to 18 or any other aspect herein wherein the at least one elastic member comprises a second plurality of spokes that are angularly spaced apart from one another about the axis and that extend between, and are connected to, the hub and the housing.
20. The apparatus of aspect 19 or any other aspect herein wherein the second plurality of spokes is spaced apart from the plurality of spokes in the longitudinal direction.
21. The apparatus of any one of aspects 19 to 20 or any other aspect herein wherein the plurality of spokes and the second plurality of spokes are identical.
22. The apparatus of aspect 1 or any other aspect herein wherein the at least one elastic member is shaped to connect to the hub and to the housing at locations that are spaced apart in the longitudinal direction from one another.
23. The apparatus of aspect 22 or any other aspect herein wherein the at least one elastic member comprises:
24. The apparatus of aspect 23 or any other aspect herein wherein the plurality of longitudinally-extending elastic members extend in longitudinal directions between the one or more hub-coupling members and the one or more housing-coupling members.
25. The apparatus of any one of aspects 23 to 24 or any other aspect herein wherein a torsional stiffness of the one or more hub-coupling members is at least 10 times a torsional stiffness of the plurality of second elastic members.
26. The apparatus of any one of aspects 23 to 25 or any other aspect herein wherein a torsional stiffness of the one or more housing-coupling members is at least 10 times a torsional stiffness of the plurality of second elastic members.
27. The apparatus of any one of aspects 23 to 26 or any other aspect herein wherein the one or more hub-coupling members comprise a plurality of spokes that are angularly spaced apart from one another about the axis and that extend from the hub in directions that have a directional component that is radial relative to the axis.
28. The apparatus of aspect 27 or any other aspect herein wherein each of the plurality of longitudinally-extending elastic members are connected to a corresponding one of the spokes at a location that is spaced apart from the hub in a radial direction relative to the axis.
29. The apparatus of aspect 27 or any other aspect herein wherein the one or more hub-coupling members comprise a hub-coupling ring that extends around the axis at a location that is spaced apart from the hub in a radial direction relative to the axis.
30. The apparatus of aspect 29 or any other aspect herein wherein each of the plurality of longitudinally-extending elastic members are connected to the hub-coupling ring at a location that is spaced apart from the hub in a radial direction relative to the axis.
31. The apparatus of any one of aspects 23 to 26 or any other aspect herein wherein the one or more hub-coupling members comprise a disc-shaped member that extends from the hub in radial directions relative to the axis.
32. The apparatus of any one of aspects 23 to 31 or any other aspect herein wherein the one or more housing-coupling members comprise a housing-coupling ring that extends around the axis at a location that is spaced apart from the axis in a radial direction.
33. The apparatus of aspect 22 or any other aspect herein wherein the at least one elastic member comprises:
34. The apparatus of aspect 33 or any other aspect herein wherein a torsional stiffness of the one or more hub-coupling members is at least 10 times a torsional stiffness of the plurality of coil springs.
35. The apparatus of any one of aspects 33 to 34 or any other aspect herein wherein a torsional stiffness of the one or more housing-coupling members is at least 10 times a torsional stiffness of the plurality of coil springs.
36. The apparatus of any one of aspects 33 to 35 or any other aspect herein wherein the one or more hub-coupling members comprise a plurality of spokes that are angularly spaced apart from one another about the axis and that extend from the hub in directions that have a directional component that is radial relative to the axis.
37. The apparatus of aspect 36 or any other aspect herein wherein each of the plurality of hub arms are connected to a corresponding one of the spokes at a location that is spaced apart from the hub in a radial direction relative to the axis.
38. The apparatus of aspect 36 or any other aspect herein wherein the one or more hub-coupling members comprise a hub-coupling ring that extends around the axis at a location that is spaced apart from the hub in a radial direction relative to the axis.
39. The apparatus of aspect 38 or any other aspect herein wherein each of the plurality of hub arms are connected to the hub-coupling ring at a location that is spaced apart from the hub in a radial direction relative to the axis.
40. The apparatus of any one of aspects 33 to 35 or any other aspect herein wherein the one or more hub-coupling members comprise a disc-shaped member that extends from the hub in radial directions relative to the axis.
41. The apparatus of any one of aspects 33 to 40 or any other aspect herein wherein the one or more housing-coupling members comprise a housing-coupling ring that extends around the axis at a location that is spaced apart from the axis in a radial direction.
42. A vibration absorber apparatus for a mechanical system comprising a rotating machine part, the vibration absorber apparatus comprising:
43. The apparatus of aspect 42 or any other aspect herein wherein the at least one elastic member comprises:
44. The apparatus of aspect 43 or any other aspect herein wherein the plurality of longitudinally-extending elastic members extend in longitudinal directions between the one or more hub-coupling members and the one or more housing-coupling members.
45. The apparatus of any one of aspects 43 to 44 or any other aspect herein wherein a torsional stiffness of the one or more hub-coupling members is at least 10 times a torsional stiffness of the plurality of longitudinally-extending elastic members.
46. The apparatus of any one of aspects 43 to 45 or any other aspect herein wherein a torsional stiffness of the one or more housing-coupling members is at least 10 times a torsional stiffness of the plurality of longitudinally-extending elastic members.
47. The apparatus of any one of aspects 43 to 46 or any other aspect herein wherein the one or more hub-coupling members comprise a plurality of spokes that are angularly spaced apart from one another about the axis and that extend from the hub in directions that have a directional component that is radial relative to the axis.
48. The apparatus of aspect 47 or any other aspect herein wherein each of the plurality of longitudinally-extending elastic members are connected to a corresponding one of the spokes at a location that is spaced apart from the hub in a radial direction relative to the axis.
49. The apparatus of aspect 47 or any other aspect herein wherein the one or more hub-coupling members comprise a hub-coupling ring that extends around the axis at a location that is spaced apart from the hub in a radial direction relative to the axis.
50. The apparatus of aspect 49 or any other aspect herein wherein each of the plurality of longitudinally-extending elastic members are connected to the hub-coupling ring at a location that is spaced apart from the hub in a radial direction relative to the axis.
51. The apparatus of any one of aspects 43 to 46 or any other aspect herein wherein the one or more hub-coupling members comprise a disc-shaped member that extends from the hub in radial directions relative to the axis.
52. The apparatus of any one of aspects 43 to 51 or any other aspect herein wherein the one or more housing-coupling members comprise a housing-coupling ring that extends around the axis at a location that is spaced apart from the axis in a radial direction.
53. A method for damping vibrations in a mechanical system comprising a rotating machine part, the method comprising:
54. The method of aspect 53 comprising method features corresponding to the features of any of aspects 1 to 51.
55. A method for damping vibrations in a mechanical system comprising a rotating machine part, the method comprising:
56. The method of aspect 55 comprising method features corresponding to the features of any of aspects 1 to 51.
57. Apparatus comprising any features, combinations of features and/or sub-combinations of features disclosed herein.
58. Methods comprising any features, combinations of features and/or sub-combinations of features disclosed herein.
This application is a continuation of Patent Cooperation Treaty (PCT) application No. PCT/CA2022/050900 having an international filing date of 3 Jun. 2022 which in turn claims priority from, and for the purposes of the United States the benefit under 35 USC 119 in connection with, U.S. Patent Application No. 63/202,284 filed on 4 Jun. 2021. All of the applications referred to in this paragraph are hereby incorporated herein by reference.
Number | Date | Country | |
---|---|---|---|
63202284 | Jun 2021 | US |
Number | Date | Country | |
---|---|---|---|
Parent | PCT/CA2022/050900 | Jun 2022 | US |
Child | 18527228 | US |