CA1299592C - Vibration damper and isolator - Google Patents
Vibration damper and isolatorInfo
- Publication number
- CA1299592C CA1299592C CA000565201A CA565201A CA1299592C CA 1299592 C CA1299592 C CA 1299592C CA 000565201 A CA000565201 A CA 000565201A CA 565201 A CA565201 A CA 565201A CA 1299592 C CA1299592 C CA 1299592C
- Authority
- CA
- Canada
- Prior art keywords
- bellows
- fluid
- spring
- coupled
- retainer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 239000012530 fluid Substances 0.000 claims abstract description 49
- 238000013016 damping Methods 0.000 claims abstract description 13
- 238000002955 isolation Methods 0.000 claims abstract description 9
- 230000008878 coupling Effects 0.000 claims description 6
- 238000010168 coupling process Methods 0.000 claims description 6
- 238000005859 coupling reaction Methods 0.000 claims description 6
- 230000036316 preload Effects 0.000 claims description 2
- 238000000926 separation method Methods 0.000 claims description 2
- 230000008030 elimination Effects 0.000 abstract 1
- 238000003379 elimination reaction Methods 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 230000007613 environmental effect Effects 0.000 description 3
- 229910001220 stainless steel Inorganic materials 0.000 description 3
- 239000010935 stainless steel Substances 0.000 description 3
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 108010036050 human cationic antimicrobial protein 57 Proteins 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- UQEAIHBTYFGYIE-UHFFFAOYSA-N hexamethyldisiloxane Chemical class C[Si](C)(C)O[Si](C)(C)C UQEAIHBTYFGYIE-UHFFFAOYSA-N 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 239000003190 viscoelastic substance Substances 0.000 description 1
Landscapes
- Fluid-Damping Devices (AREA)
Abstract
A B S T R A C T
A vibration damping and isolation apparatus wherein in damping is obtained by purely viscous fluid shear forces. The fluid is sealed in two chambers divided by a orifice to permit fluid flow. Chamber containment of the fluid and chamber volume change is provided by metal bellows which are arranged to provided a constant overall volume. Coulomb forces are avoided by the elimination of rubbing surfaces.
A vibration damping and isolation apparatus wherein in damping is obtained by purely viscous fluid shear forces. The fluid is sealed in two chambers divided by a orifice to permit fluid flow. Chamber containment of the fluid and chamber volume change is provided by metal bellows which are arranged to provided a constant overall volume. Coulomb forces are avoided by the elimination of rubbing surfaces.
Description
5~
BACKGROUND OF THE INVENTION
1. Field oE the Invention The invention relates to the field of vibration isolation and more particularly to vibration damping and isolation for devices having extremely low vibration specifications.
BACKGROUND OF THE INVENTION
1. Field oE the Invention The invention relates to the field of vibration isolation and more particularly to vibration damping and isolation for devices having extremely low vibration specifications.
2. Description of the Prior Art Reaction wheel assemblies on pointing control systems are crucial elements of a telescopic system. These assemblies, however, significantly contribute vibration components to the system during operation. Since telescopes have stringent pointing requirement~ there is a need to isolate the vibration induced by the reaction wheel, most significantly of which are caused by the axial forces attributable to the bearing of the ball on the inner and outer races and imperfections in the ball itself.
One prior art solution to the problem, known as a wire rope, utilizes several stranded wîres wrapped in a circle and attached at one end to a base or ground and at the other end to the device or payload to be isolated.
Compliance and isolation are provided by the flexibility of the wire and Coulomb damping or energy absorption i~ provided by the wires rubbing together. This device has several short coming which include, low damping and stiffness characteristics which are variable with the magnitude of the input vibration level, performance changes with environmental ~2~
1 variations, and mathematical complexities that require an iteration procedure of design and test before reaching a final configuration.
A second solution of the prior art utilizes viscoelastic materials as the isolating element. These devices though capable of providing isolation for most applications, exhibit excessive sensitivity to temperature and other environmental conditions.
SUMMARY OF THE INVENTION
In accordance with the present invention vibration isolation and dampiny is achieved with an arrangement of bellows, coil spring, and fluid which eliminate rubbing surfaces, thereby Coulomb forces, and provide a stiffness that i5 independent of the vibration level. Firs-t and seeond bellows are positioned in axial alignment and fluidly sealed at opposite ends by an end piece and base respectlvely to form inner chambers. A shaft extending along the common axis i~ attached to the end piece and base to maintain a fixed ZO separation distance therebetween. A piston having an axial bore hole and a flange extending therefrom for coupling to a payload is positioned about the shaft in a coaxial relationship, forming a fluid gap between it and the shaft.
This fluid gap couples fluid chambers in the first and second bellows that are formed between the piston, the inner walls of the bellows, and the flange extension from the piston to which the previously unsealed ends of the bellows are sealed to provide for fluid containment. This arrangement obtains damping by purely viscous fluid shear forces and completely 1 avoidR any rubbiny surfaces, thereby eliminating Coulomb forces. The fluid i5 sealed in the two fluid chambers and the gap formed between the piston and the shaft. As the payload moves, the volume of one chamber increases while the volume of the second decreases. The overall volu~e, due to the fixed distance between the end piece of the first bellows and the base piece of the second bellows maintained by the shaft, remains constant. Thus, fluid of constant volume ~hat is contained within the two chambers and the gap is distributed to the chambers in accordance with the movement of the load. Damping coefficients for the invention vary as a function of fluid viscosity and the radial lenyth of the gap, increasing as the viscosity increases and the radial length decreases. A spring externally coiled about the bellows supports the flange and provides stiffness to the vibration isolator.
Temperature compensation may be achieved by providing a third bellows which is axially aligned with the first and second bellows, and has a fluid chamber therewithin coupled to the fluid system of the first and second bellows to provide for the e~change of ~luid between the temperature compensator and the main vibration isolator. This fluid e~change causes a constant fluid pressure to be maintained in the system with temperature variations. A spring externally coiled about the temperature compensating bellows maintains an axial force thereon to achieve a positive pressure on the internal fluid over the temperature range of interest independent of the environmental pressure.
?5~3Z
72558~16 The vl~ratlon lsolatlon and damplng apparatus of the inventlon has a first bellows, one end of whlch is fluldly sealed by an end piece and a second bellows coaxlally allgned with the first bellows, one end of whlch ls fluldly sealed by a base plece.
A shaft of predetermined length ls coupled to the end and base pleces and is coaxlally posltloned with the flrst and second bellows so that a flxed predetermlned separatlon ls malntalned between the end and base pleces. A plston, having an axlal bore coaxlally posltloned wlth the shaft, has a flange extenslon that ls coupled to the open ends of the flrst and second bellows ln a manner to establish fluld seals with the first and second bellows.
Thls flange extenslon lB constructed to allow the coupling of the apparatus to a payload~ The plston forms a flrst fluld chamber wlth the flrst bellows and a second fluid chamber, with the second bellow~. A fluld fllls the flrst and second fluid chamberq and a radlal gap between the plston and the shaft provldes fluld coupling between the chambers. Springs colled a~out the first bellows between the flange extenslon and the end plece and coiled about the second bellows between the flange extenslon and the base plece provlde radlal and a~lal stiffness. A thermal compensator bellows wlth a fluid fllled lnner chamber ls fluidly coupled to the radlal gap and to the flrst and second fluld chambers. A
pressure mechanism ls coupled to the thermal compensator bellows ln a manner to establish positlv~ pressure on the fluid with variatlons of atmospherlc pressure condltions. The thermal compensator bellows expand~ wlth expansion of the fluld and cooperates wlth the pressure mechanlsm to malntaln constant system pressure.
3a B
Figure 1 i5 a cutaway view of a vibration damper and isolator, including a temperature compensatlng element, constructed in accordance with the principles of the invention.
Figure 2 is a schematic diagram of the vibration damper and isolator of Figure 1.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
The invention will be describecl with respect to Figure 1. A vibration damper and isolator 10 includes a cover 11 enclosing a upper bellows 13 with an end piece 15 bonded at one end to provide a fluid seal and structural integrity. A lower bellows 1~ with a base piece 19 bonded to one end, also to provide a fluid seal and structural integrity is positioned in axial alignment with the upper bellows. Each bellows may have a wall thickness o~ 75 micrometers and may be electroplated. A rigid shaft 21, coaxial with the upper and lower bellows, is bonded to the end piece 15 and the base 19 to maintain a fixed distance therebetween and thereby, a constant volume within the bellows assembly. A piston 23, having an axial bore and flange 25 extending therefrom, is coaxially positioned about the shaft 21 to create a radial gap 27 therebetween. The section of the upper bellows opposite the end piece is bonded to an upper surface 29 of the flange extension of the piston, while the section of the lower bellows opposite the base piece 19 is bonded to a lower surface 31 of the flange extension. An upper fluid reservoir 33 and a lower 1uid 1 reservoir 35 are respectively formed by the upper and lower bellows iII combination with the flange extension and the outer surface of the piston wall. Fluid, which may be Dow corning 200 Series silicone, is installecl in the system to completely fill the reservoirs 33, 35, and the gap 27. This fluid, during vibration, is forced between the upper reservoir 33 and the lower reservoir 35 via the damping gap 2~. Though the volume of the upper and lower reservoirs 33, 35 may change with the motion of the payload attached to the flange, the total reservoir volume remains constant due to the fixed distance maintained by the shaft 21 between the end pièce 15 and the base piece 19. Con~e~uently, motion by the payload and flange 25 must produce equal but opposite volume changes in the upper and lower reservoirs 33, 35.
16 An upper stainless steel spring 3~ is coiled about the outer surface of the upper bellows 13 between the upper surface 39 of the flange extension 25 and a spring retainer 41 bolted -to the end piece 15. A lower stainless steel spring 43 is coiled about the outer surface o~ the lower bellows 1~ between the lower surface 45 of the flange extension and a spring retainer surface 4~ formed in the skirt 49 extending from the base 19. These springs provide appropriate radial and axially stiffness for the vibration damper and isolator.
Refer now to the schematic diagram of the vibration damper and isolator shown in Figure 2, wherein elements previously cited bear the initially assigned reference numerals. In Figure 2 it is schematically shown that the end piece 15 and the base piece 19 are maintained at a fixed 1 5eparation distance by a rigid shaft 21. A pis'ton 23, with an axial bore, is coaxially positioned about the shaft 21.
Extending from the piston is a flange 25 for attachment to the load. The upper bellows 13 is bonded to the end piece 15 and to the upper surface 29 o~ the flange extension, while the lower bellows 17 is bonded to the base 19 and the lower surface 31 of the flange extension. It i9 apparent from Figure 2 that the total volume of the fluid contained betweer the end piece 15, the base 19, the upper bellows 13 and the lower bellows 17 is constant. Assume an upward force is exerted on the base 19, decreasing the volume of the lower reservoir 35. Thi~ causes the volume of the upper reservoir 33 to increase and a fluid flow through the damping gap 27 from the lower reservoir 35 to the upper reservoir 33, equalizing the forces on the upper and lower surfaces of the flange extension, thereby causing the flange to remain stationary.
Referring again to Figure 1. Temperature compensation for fluid volume variation with temperature is provided by coupling thermal compensator bellows 51 through relief gap 53 and fluid channel 55 to the upper bellows 13.
The thermal co~pensator bellows 51 is fluidly sealed by a cap 57 and the internal region of the bellows 51, the thermal compensator relief gap 53 and the relief channel 55 are filled with fluid to eliminate all air gaps in the system.
An "0" ring 58 between the thermal compensator bellows 51 and the upper bellows 13 completes the fluid seal. Fluid expansion due to a temperature increase causes the thermal compensator bellows 51 to expand, thereby relievin~ an over 1 pressure condition in the reservoirs 33, 35 and damping gap 2~ of the vibration damper and isolator to maintain constant system pressure.
An axial force is maintained on the thermal compensator bellow~ 51 by a stainless steel preload spring 59 ~ to establish a positive pressure on the internal fluid over a wide range of atmospheric pressure conditions. Spring 59 is held in place by a lower retainer 61 coupled to the cap 57 and bolted to the spring retainer ~1 and an upper retainer 63 extending for a predetermined distance above the lower retainer and also bolted to the spring retainer 41.
While the invention has been described in its preferred embodiments, it is to be understood that the word~
which have been used are words of description rather than limitation and that changes may be made within the purview of the appended claims without departing form the true scope and spirit of the invention in its broader aspects.
One prior art solution to the problem, known as a wire rope, utilizes several stranded wîres wrapped in a circle and attached at one end to a base or ground and at the other end to the device or payload to be isolated.
Compliance and isolation are provided by the flexibility of the wire and Coulomb damping or energy absorption i~ provided by the wires rubbing together. This device has several short coming which include, low damping and stiffness characteristics which are variable with the magnitude of the input vibration level, performance changes with environmental ~2~
1 variations, and mathematical complexities that require an iteration procedure of design and test before reaching a final configuration.
A second solution of the prior art utilizes viscoelastic materials as the isolating element. These devices though capable of providing isolation for most applications, exhibit excessive sensitivity to temperature and other environmental conditions.
SUMMARY OF THE INVENTION
In accordance with the present invention vibration isolation and dampiny is achieved with an arrangement of bellows, coil spring, and fluid which eliminate rubbing surfaces, thereby Coulomb forces, and provide a stiffness that i5 independent of the vibration level. Firs-t and seeond bellows are positioned in axial alignment and fluidly sealed at opposite ends by an end piece and base respectlvely to form inner chambers. A shaft extending along the common axis i~ attached to the end piece and base to maintain a fixed ZO separation distance therebetween. A piston having an axial bore hole and a flange extending therefrom for coupling to a payload is positioned about the shaft in a coaxial relationship, forming a fluid gap between it and the shaft.
This fluid gap couples fluid chambers in the first and second bellows that are formed between the piston, the inner walls of the bellows, and the flange extension from the piston to which the previously unsealed ends of the bellows are sealed to provide for fluid containment. This arrangement obtains damping by purely viscous fluid shear forces and completely 1 avoidR any rubbiny surfaces, thereby eliminating Coulomb forces. The fluid i5 sealed in the two fluid chambers and the gap formed between the piston and the shaft. As the payload moves, the volume of one chamber increases while the volume of the second decreases. The overall volu~e, due to the fixed distance between the end piece of the first bellows and the base piece of the second bellows maintained by the shaft, remains constant. Thus, fluid of constant volume ~hat is contained within the two chambers and the gap is distributed to the chambers in accordance with the movement of the load. Damping coefficients for the invention vary as a function of fluid viscosity and the radial lenyth of the gap, increasing as the viscosity increases and the radial length decreases. A spring externally coiled about the bellows supports the flange and provides stiffness to the vibration isolator.
Temperature compensation may be achieved by providing a third bellows which is axially aligned with the first and second bellows, and has a fluid chamber therewithin coupled to the fluid system of the first and second bellows to provide for the e~change of ~luid between the temperature compensator and the main vibration isolator. This fluid e~change causes a constant fluid pressure to be maintained in the system with temperature variations. A spring externally coiled about the temperature compensating bellows maintains an axial force thereon to achieve a positive pressure on the internal fluid over the temperature range of interest independent of the environmental pressure.
?5~3Z
72558~16 The vl~ratlon lsolatlon and damplng apparatus of the inventlon has a first bellows, one end of whlch is fluldly sealed by an end piece and a second bellows coaxlally allgned with the first bellows, one end of whlch ls fluldly sealed by a base plece.
A shaft of predetermined length ls coupled to the end and base pleces and is coaxlally posltloned with the flrst and second bellows so that a flxed predetermlned separatlon ls malntalned between the end and base pleces. A plston, having an axlal bore coaxlally posltloned wlth the shaft, has a flange extenslon that ls coupled to the open ends of the flrst and second bellows ln a manner to establish fluld seals with the first and second bellows.
Thls flange extenslon lB constructed to allow the coupling of the apparatus to a payload~ The plston forms a flrst fluld chamber wlth the flrst bellows and a second fluid chamber, with the second bellow~. A fluld fllls the flrst and second fluid chamberq and a radlal gap between the plston and the shaft provldes fluld coupling between the chambers. Springs colled a~out the first bellows between the flange extenslon and the end plece and coiled about the second bellows between the flange extenslon and the base plece provlde radlal and a~lal stiffness. A thermal compensator bellows wlth a fluid fllled lnner chamber ls fluidly coupled to the radlal gap and to the flrst and second fluld chambers. A
pressure mechanism ls coupled to the thermal compensator bellows ln a manner to establish positlv~ pressure on the fluid with variatlons of atmospherlc pressure condltions. The thermal compensator bellows expand~ wlth expansion of the fluld and cooperates wlth the pressure mechanlsm to malntaln constant system pressure.
3a B
Figure 1 i5 a cutaway view of a vibration damper and isolator, including a temperature compensatlng element, constructed in accordance with the principles of the invention.
Figure 2 is a schematic diagram of the vibration damper and isolator of Figure 1.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
The invention will be describecl with respect to Figure 1. A vibration damper and isolator 10 includes a cover 11 enclosing a upper bellows 13 with an end piece 15 bonded at one end to provide a fluid seal and structural integrity. A lower bellows 1~ with a base piece 19 bonded to one end, also to provide a fluid seal and structural integrity is positioned in axial alignment with the upper bellows. Each bellows may have a wall thickness o~ 75 micrometers and may be electroplated. A rigid shaft 21, coaxial with the upper and lower bellows, is bonded to the end piece 15 and the base 19 to maintain a fixed distance therebetween and thereby, a constant volume within the bellows assembly. A piston 23, having an axial bore and flange 25 extending therefrom, is coaxially positioned about the shaft 21 to create a radial gap 27 therebetween. The section of the upper bellows opposite the end piece is bonded to an upper surface 29 of the flange extension of the piston, while the section of the lower bellows opposite the base piece 19 is bonded to a lower surface 31 of the flange extension. An upper fluid reservoir 33 and a lower 1uid 1 reservoir 35 are respectively formed by the upper and lower bellows iII combination with the flange extension and the outer surface of the piston wall. Fluid, which may be Dow corning 200 Series silicone, is installecl in the system to completely fill the reservoirs 33, 35, and the gap 27. This fluid, during vibration, is forced between the upper reservoir 33 and the lower reservoir 35 via the damping gap 2~. Though the volume of the upper and lower reservoirs 33, 35 may change with the motion of the payload attached to the flange, the total reservoir volume remains constant due to the fixed distance maintained by the shaft 21 between the end pièce 15 and the base piece 19. Con~e~uently, motion by the payload and flange 25 must produce equal but opposite volume changes in the upper and lower reservoirs 33, 35.
16 An upper stainless steel spring 3~ is coiled about the outer surface of the upper bellows 13 between the upper surface 39 of the flange extension 25 and a spring retainer 41 bolted -to the end piece 15. A lower stainless steel spring 43 is coiled about the outer surface o~ the lower bellows 1~ between the lower surface 45 of the flange extension and a spring retainer surface 4~ formed in the skirt 49 extending from the base 19. These springs provide appropriate radial and axially stiffness for the vibration damper and isolator.
Refer now to the schematic diagram of the vibration damper and isolator shown in Figure 2, wherein elements previously cited bear the initially assigned reference numerals. In Figure 2 it is schematically shown that the end piece 15 and the base piece 19 are maintained at a fixed 1 5eparation distance by a rigid shaft 21. A pis'ton 23, with an axial bore, is coaxially positioned about the shaft 21.
Extending from the piston is a flange 25 for attachment to the load. The upper bellows 13 is bonded to the end piece 15 and to the upper surface 29 o~ the flange extension, while the lower bellows 17 is bonded to the base 19 and the lower surface 31 of the flange extension. It i9 apparent from Figure 2 that the total volume of the fluid contained betweer the end piece 15, the base 19, the upper bellows 13 and the lower bellows 17 is constant. Assume an upward force is exerted on the base 19, decreasing the volume of the lower reservoir 35. Thi~ causes the volume of the upper reservoir 33 to increase and a fluid flow through the damping gap 27 from the lower reservoir 35 to the upper reservoir 33, equalizing the forces on the upper and lower surfaces of the flange extension, thereby causing the flange to remain stationary.
Referring again to Figure 1. Temperature compensation for fluid volume variation with temperature is provided by coupling thermal compensator bellows 51 through relief gap 53 and fluid channel 55 to the upper bellows 13.
The thermal co~pensator bellows 51 is fluidly sealed by a cap 57 and the internal region of the bellows 51, the thermal compensator relief gap 53 and the relief channel 55 are filled with fluid to eliminate all air gaps in the system.
An "0" ring 58 between the thermal compensator bellows 51 and the upper bellows 13 completes the fluid seal. Fluid expansion due to a temperature increase causes the thermal compensator bellows 51 to expand, thereby relievin~ an over 1 pressure condition in the reservoirs 33, 35 and damping gap 2~ of the vibration damper and isolator to maintain constant system pressure.
An axial force is maintained on the thermal compensator bellow~ 51 by a stainless steel preload spring 59 ~ to establish a positive pressure on the internal fluid over a wide range of atmospheric pressure conditions. Spring 59 is held in place by a lower retainer 61 coupled to the cap 57 and bolted to the spring retainer ~1 and an upper retainer 63 extending for a predetermined distance above the lower retainer and also bolted to the spring retainer 41.
While the invention has been described in its preferred embodiments, it is to be understood that the word~
which have been used are words of description rather than limitation and that changes may be made within the purview of the appended claims without departing form the true scope and spirit of the invention in its broader aspects.
Claims (3)
1. A vibration isolation and damping apparatus comprising a first bellows having a first end with an end piece thereat forming a fluid seal and a second end, a second bellows coaxially aligned with said first bellows and having a first end with a base piece thereat forming a fluid seal and a second end, a shaft of predetermined length coaxially positioned with said first and second bellows and coupled to said end and base pieces thereby maintaining a fixed predetermined separation therebetween and characterized in that it further comprises a piston having an axial bore coaxially positioned with said shaft and having a flange extension coupled to said second end of said first bellows and to said second end of said second bellows to establish fluid seals with said first and second bellows, said flange extension having flange means for coupling said apparatus to a payload, said piston forming a first fluid chamber with said first bellows, a second fluid chamber with said second bellows, and a radial gap with said shaft, said radial gap providing fluid coupling between said first and second fluid chambers, a fluid filling said first and second fluid chambers and said radial gap, spring means coiled about said first and second bellows positioned between said flange extension and said end piece and between said flange extension and said base piece for providing radial axial stiffness, a thermal compensator bellows having an inner chamber fluid filled and fluidly coupled to said radial gap and to said first and second fluid chambers, and pressure means coupled for said thermal compensator bellows for establishing positive pressure on said fluid with variations of atmospheric pressure conditions, said thermal compensator bellows expanding with expansions of said fluid and cooperating with said pressure means to maintain constant system pressure.
2. A vibrant isolation and damping apparatus in accordance with Claim 1 wherein said spring means includes a first spring retainer coupled to said end piece, a first spring coiled about said first bellows and positioned between said first spring retainer and said flange extension, a second spring retainer coupled to said base piece, and a second spring coiled about said second bellows and positioned between said second spring retainer and said flange extension.
3. A vibration isolation and damping apparatus in accordance with Claims 1 or 2 wherein said pressure means includes a first retainer coupled to said end piece, a second retainer coupled to said first retainer and extending a predetermined distance above said first retainer, and a preload spring positioned between said first and second retainers and coiled about said thermal compensator bellows.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA000565201A CA1299592C (en) | 1988-04-27 | 1988-04-27 | Vibration damper and isolator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA000565201A CA1299592C (en) | 1988-04-27 | 1988-04-27 | Vibration damper and isolator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1299592C true CA1299592C (en) | 1992-04-28 |
Family
ID=4137915
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA000565201A Expired - Fee Related CA1299592C (en) | 1988-04-27 | 1988-04-27 | Vibration damper and isolator |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA1299592C (en) |
-
1988
- 1988-04-27 CA CA000565201A patent/CA1299592C/en not_active Expired - Fee Related
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| MKLA | Lapsed |