GB2298018A - Elastomeric vibration-damping bushing with hydraulic damping - Google Patents

Elastomeric vibration-damping bushing with hydraulic damping Download PDF

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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
Application number
GB9503187A
Other versions
GB9503187D0 (en
GB2298018B (en
Inventor
Giacomo Sciortino
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Delphi Automotive Systems France
ACG France SAS
Original Assignee
Delphi Automotive Systems France
ACG France SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Delphi Automotive Systems France, ACG France SAS filed Critical Delphi Automotive Systems France
Priority to GB9503187A priority Critical patent/GB2298018B/en
Publication of GB9503187D0 publication Critical patent/GB9503187D0/en
Publication of GB2298018A publication Critical patent/GB2298018A/en
Application granted granted Critical
Publication of GB2298018B publication Critical patent/GB2298018B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F13/00Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs
    • F16F13/04Units 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
    • F16F13/06Units 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
    • F16F13/08Units 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
    • F16F13/14Units of the bushing type, i.e. loaded predominantly radially
    • F16F13/1463Units of the bushing type, i.e. loaded predominantly radially characterised by features of passages between working chambers

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)

Claims:
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.
GB9503187A 1995-02-18 1995-02-18 A bushing Expired - Fee Related GB2298018B (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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
GB9503187D0 (en) 1995-04-05
GB2298018B (en) 1997-05-07

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 20100218