GB2298018A - Elastomeric vibration-damping bushing with hydraulic damping - Google Patents
Elastomeric vibration-damping bushing with hydraulic damping Download PDFInfo
- Publication number
- GB2298018A GB2298018A GB9503187A GB9503187A GB2298018A GB 2298018 A GB2298018 A GB 2298018A GB 9503187 A GB9503187 A GB 9503187A GB 9503187 A GB9503187 A GB 9503187A GB 2298018 A GB2298018 A GB 2298018A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bushing
- channel
- block
- chambers
- inner sleeve
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F13/00—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs
- F16F13/04—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs comprising both a plastics spring and a damper, e.g. a friction damper
- F16F13/06—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs comprising both a plastics spring and a damper, e.g. a friction damper the damper being a fluid damper, e.g. the plastics spring not forming a part of the wall of the fluid chamber of the damper
- F16F13/08—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs comprising both a plastics spring and a damper, e.g. a friction damper the damper being a fluid damper, e.g. the plastics spring not forming a part of the wall of the fluid chamber of the damper the plastics spring forming at least a part of the wall of the fluid chamber of the damper
- F16F13/14—Units of the bushing type, i.e. loaded predominantly radially
- F16F13/1463—Units of the bushing type, i.e. loaded predominantly radially characterised by features of passages between working chambers
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Combined Devices Of Dampers And Springs (AREA)
Abstract
The bushing (10) comprises an inner sleeve (12); an outer sleeve substantially coaxial with the inner sleeve; a block (16) of resilient material retained between the inner sleeve and the outer sleeve, and shaped to define two associated pairs working chambers (18,20;18'20') that are filled with hydraulic fluid a first channel (22) interconnects one pair of associated chambers (18,20) for fluid flow therebetween; and a second channel (22') interconnects the other pair of associated chambers (18',20') for fluid flow therebetween. Improved isolation to vibrations over 360 degrees is thus provided.
Description
A BUSHING
The present invention relates to a bushing for use on a motor vehicle to suppress vibrations.
Vibration damping bushings are used on motor vehicles in association with suspension systems, steering systems, and engine and transmission mounting systems. A basic design of bushing comprises inner and outer coaxial metallic sleeves with a moulded elastomeric block therebetween. A development of this arrangement provided the formation of two working chambers in the elastomeric block with a channel interconnecting the chambers. Hydraulic fluid substantially fills the chambers. During vibration damping action of the bushing, fluid is pumped between the two chambers by way of the channel. An example of this prior art can be found in US Patent No. 5178375.
An example of a similar arrangement for engine mounts is disclosed in US Patent No. 4720086. These known arrangements provide little or no isolation to vibrations over 360 degrees.
It is an object of the present invention to overcome the above mentioned disadvantage.
To this end, a bushing in accordance with the present invention comprises an inner sleeve; an outer sleeve substantially coaxial with the inner sleeve; a block of resilient material retained between the inner sleeve and the outer sleeve, and being shaped to define two associated pairs working chambers that are substantially filled with hydraulic fluid; a first channel interconnecting one pair of associated chambers for fluid flow therebetween; and a second channel interconnecting the other pair of associated chambers for fluid flow therebetween.
The present invention provides isolation to vibrations in low frequency range over 360 degrees excitation.
The present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
Figure 1 is a cross-section view on the line
I-I of Figure 2 of a bushing in accordance with the present invention;
Figure 2 is a cross-sectional view on the line II-II of Figure 1;
Figure 3 is a perspective view of the inner sleeve and elastomeric block of the bushing of Figure 1;
Figure 4 is a schematic presentation of the channel and the fluid restriction passage of the bushing of Figure 1;
Figure 5 is a graph of dynamic stiffness against frequency for a bushing in accordance with the present invention;
Figure 6 is a graph of phase angle against frequency for a bushing in accordance with the present invention; and
Figure 7 is a graph of damping energy against frequency for a bushing in accordance with the present invention.
Referring to Figures 1 to 3, a bushing 10 in accordance with the present invention comprises an inner sleeve 12, an outer sleeve 14, and a block 16 of resilient material therebetween. The inner and outer sleeves 12 and 14 are substantially cylindrical and coaxial, and formed from any suitable metallic material. Although shown as circular in crosssection, the inner sleeve may have another other suitable cross-section. The block 16 is moulded from elastomeric material onto the inner sleeve 12, with the outer sleeve 14 being attached thereafter. Formed within the block 16 are two working chambers comprising a pumping chamber 18 and a release chamber 20. The pumping chamber 18 has a smaller volume than the release chamber 20. The longitudinally extending walls 19,21 of each chamber 18,20 respectively curve outwardly from the inner sleeve 12 to the outer sleeve 14.The chambers 18,20 are substantially filled with hydraulic fluid. A channel 22 is formed in the outer surface 23 of the block 16, extends circumferentially, and is connected at either end by openings 24,26 with the pumping chamber 18 and the release chamber 20 respectively. During damping operation of the bushing 10, the inner and outer sleeves 12,14 move relative to one another to cause hydraulic fluid to be pumped from one chamber 18,20 to the other chamber by way of the channel 22. As so far described, the bushing 10 is known to those skilled in the art.
Also formed within the block 16 are two additional working chambers comprising a pumping chamber 18' and a release chamber 20'. The pumping chamber 18' has a smaller volume than the release chamber 20'. The longitudinally extending walls 19',21' of each chamber 18',20' respectively curve outwardly from the inner sleeve 12 to the outer sleeve 14. The chambers 18',20' are substantially filled with hydraulic fluid. A channel 22' is formed in the outer surface 23 of the block 16, extends circumferentially, and is connected at either end by openings 24',26' with the pumping chamber 18' and the release chamber 20' respectively. During damping operation of the bushing 10 hydraulic fluid is also pumped from one chamber 18',20' to the other chamber by way of the channel 22'.
Preferably positioned within the channel 22 is a flow restriction passage 28. The passage 28 is preferably moulded integrally with the block 16.
Alternatively, an additional metal sleeve (not shown) may be positioned between the outer sleeve 14 and the block 16 to provide a metallic lining for the channel and to define the flow restriction passage. The presence of the passage 28 in the channel 22 provides better damping at low frequency vibrations for the bushing 10. A similar flow restriction passage 28' is preferably positioned in the channel 22'.
The channel 22 is preferably formed with a predetermined length L and a predetermined maximum diameter or width D (see Figure 4) either side of the flow restriction passage 28. In a preferred arrangement, the ratio of L/D lies in the range of 1 to 18. Further, the passage 28 is preferably formed with a predetermined length 1 and a predetermined maximum diameter or width d (see Figure 4). In a preferred arrangement, the ratio of l/d also lies in the range of 1 to 18, and is preferably the same as the ratio of L/D. The values for L, D, 1 and d are predetermined to provide the required compliance verses vibration frequency characteristics and the required dynamic stiffness verses vibration frequency characteristics for the bushing 10. The passage 28 is preferably situated at the mid-point of the channel 22.It is possible that the maximum diameter or width of the channel 22 may be different on either side of the passage 28. However, it is preferable that the maximum diameter or width of the channel 22 remains substantially constant along the length of the channel. The cross-sectional shape of the channel 22 is preferably substantially V-shape as shown, or semicircular. The channel 22' is preferably substantially the same as the channel 22.
The graphs of Figures 5 to 7 indicate plots of dynamic stiffness K*, phase angle , and damping energy or compliance C, respectively, against frequency f for the bushing 10 of Figures 1 to 4. The critical operating frequency is indicated by the line fcrit- fcrit is an intermediate frequency at which the dynamic stiffness K* increases rapidly, and so the damping energy C is much larger and the phase angle + is at a maximum. Increasing L will move the peak of graph + against f to the left as viewed in Figure 6 and as indicated by the dashed line f(L). Increasing
D will move the peak of graph Q against f to the right as viewed in Figure 6 and as indicated by the dashed line f(D). Any such movement affects the critical frequency crit, and hence, the dynamic stiffness and compliance of the bushing 10. It will be appreciated, therefore, that the bushing 10 can be tuned to meet any predetermined requirements for damping.
As an alternative to the above described arrangement, the block may be formed from any suitable plastics material.
Attention is drawn to our patent application nos. (Ref. No. MJD/H-182114) and
(Ref. No. MJD/H-187270), filed the same day as the present application, the disclosures in which are incorporated herein by reference.
Claims (10)
1. A bushing comprising an inner sleeve; an outer sleeve substantially coaxial with the inner sleeve; a block of resilient material retained between the inner sleeve and the outer sleeve, and being shaped to define two associated pairs working chambers that are substantially filled with hydraulic fluid; a first channel interconnecting one pair of associated chambers for fluid flow therebetween; and a second channel interconnecting the other pair of associated chambers for fluid flow therebetween.
2. A bushing as claimed in Claim 1, wherein each channel has a flow restriction passage positioned therein to restrict the flow of fluid through each channel between the associated pairs of chambers.
3. A bushing as claimed in Claim 2, wherein each channel has a predetermined length and a predetermined maximum diameter either side of its flow restriction passage.
4. A bushing as claimed in Claim 3, wherein the ratio of the predetermined length to the predetermined maximum diameter of each channel lies in the range of 1 to 18.
5. A bushing as claimed in any one of
Claims 2 to 4, wherein each passage has a predetermined length and a predetermined maximum diameter.
6. A bushing as claimed in Claim 5, wherein the ratio of the predetermined length to the predetermined maximum diameter of each passage lies in the range of 1 to 18.
7. A bushing as claimed in any one of
Claims 2 to 6, wherein each passage is situated substantially at the mid-point of the total length of its channel.
8. A bushing as claimed in any one of
Claims 1 to 7, wherein each channel extends circumferentially around the outer surface of the block.
9. A bushing as claimed in any one of
Claims 1 to 8, wherein the block is moulded from elastomeric material and wherein the block and each channel are moulded as an integral formation.
10. A bushing substantially as herein described with reference to, and as shown in, the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9503187A GB2298018B (en) | 1995-02-18 | 1995-02-18 | A bushing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9503187A GB2298018B (en) | 1995-02-18 | 1995-02-18 | A bushing |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9503187D0 GB9503187D0 (en) | 1995-04-05 |
GB2298018A true GB2298018A (en) | 1996-08-21 |
GB2298018B GB2298018B (en) | 1997-05-07 |
Family
ID=10769812
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9503187A Expired - Fee Related GB2298018B (en) | 1995-02-18 | 1995-02-18 | A bushing |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2298018B (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2322427A (en) * | 1997-02-25 | 1998-08-26 | Avon Vibration Man Syst Ltd | Hydraulically damped mounting device |
US6276671B1 (en) | 1998-10-29 | 2001-08-21 | Avon Vibration Management Systems Limited | Hydraulically damped mounting device |
GB2386170A (en) * | 2002-03-04 | 2003-09-10 | Avon Vibration Man Syst Ltd | A hydraulically damped mounting device of the bush type |
GB2394524A (en) * | 2002-03-04 | 2004-04-28 | Avon Vibration Man Syst Ltd | A hydraulically damped mounting device of the bush type |
US7798477B2 (en) | 2006-01-09 | 2010-09-21 | Dtr Vms Limited | Hydraulically damped mounting device |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2193553A (en) * | 1986-07-08 | 1988-02-10 | Btr Plc | Vibration absorbing mountings |
US4971456A (en) * | 1988-10-08 | 1990-11-20 | Tokai Rubber Industries, Ltd. | Fluid-filled elastic center bearing mount |
US4982938A (en) * | 1988-03-26 | 1991-01-08 | Boge Ag | Hydraulic damping elastic bearing |
US5123633A (en) * | 1990-02-27 | 1992-06-23 | Tokai Rubber Industries, Ltd. | Fluid-filled elastic rotational coupling having two fluid chambers on each side of wing members |
-
1995
- 1995-02-18 GB GB9503187A patent/GB2298018B/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2193553A (en) * | 1986-07-08 | 1988-02-10 | Btr Plc | Vibration absorbing mountings |
US4982938A (en) * | 1988-03-26 | 1991-01-08 | Boge Ag | Hydraulic damping elastic bearing |
US4971456A (en) * | 1988-10-08 | 1990-11-20 | Tokai Rubber Industries, Ltd. | Fluid-filled elastic center bearing mount |
US5123633A (en) * | 1990-02-27 | 1992-06-23 | Tokai Rubber Industries, Ltd. | Fluid-filled elastic rotational coupling having two fluid chambers on each side of wing members |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2322427A (en) * | 1997-02-25 | 1998-08-26 | Avon Vibration Man Syst Ltd | Hydraulically damped mounting device |
GB2322427B (en) * | 1997-02-25 | 1998-12-30 | Avon Vibration Man Syst Ltd | Hydraulically damped mounting device |
DE19807949B4 (en) * | 1997-02-25 | 2004-08-12 | Avon Vibration Management Systems Ltd., Chippenham | Hydraulically damped storage facility |
US6276671B1 (en) | 1998-10-29 | 2001-08-21 | Avon Vibration Management Systems Limited | Hydraulically damped mounting device |
GB2386170A (en) * | 2002-03-04 | 2003-09-10 | Avon Vibration Man Syst Ltd | A hydraulically damped mounting device of the bush type |
GB2386170B (en) * | 2002-03-04 | 2004-04-28 | Avon Vibration Man Syst Ltd | Hydraulically damped mounting device |
GB2394524A (en) * | 2002-03-04 | 2004-04-28 | Avon Vibration Man Syst Ltd | A hydraulically damped mounting device of the bush type |
GB2394524B (en) * | 2002-03-04 | 2004-06-16 | Avon Vibration Man Syst Ltd | Hydraulically damped mounting device |
US7798477B2 (en) | 2006-01-09 | 2010-09-21 | Dtr Vms Limited | Hydraulically damped mounting device |
Also Published As
Publication number | Publication date |
---|---|
GB2298018B (en) | 1997-05-07 |
GB9503187D0 (en) | 1995-04-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20100218 |