GB2292434A - Vibration-damping bush - Google Patents

Vibration-damping bush Download PDF

Info

Publication number
GB2292434A
GB2292434A GB9515481A GB9515481A GB2292434A GB 2292434 A GB2292434 A GB 2292434A GB 9515481 A GB9515481 A GB 9515481A GB 9515481 A GB9515481 A GB 9515481A GB 2292434 A GB2292434 A GB 2292434A
Authority
GB
United Kingdom
Prior art keywords
bush
sleeve
fastening screw
bush according
bore
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
GB9515481A
Other versions
GB9515481D0 (en
GB2292434B (en
Inventor
Bruno Hezel
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.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
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 Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of GB9515481D0 publication Critical patent/GB9515481D0/en
Publication of GB2292434A publication Critical patent/GB2292434A/en
Application granted granted Critical
Publication of GB2292434B publication Critical patent/GB2292434B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

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
    • F16F1/00Springs
    • F16F1/36Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/373Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape
    • F16F1/3732Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape having an annular or the like shape, e.g. grommet-type resilient mountings
    • 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
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B43/00Washers or equivalent devices; Other devices for supporting bolt-heads or nuts
    • F16B43/001Washers or equivalent devices; Other devices for supporting bolt-heads or nuts for sealing or insulation
    • 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
    • F16F7/00Vibration-dampers; Shock-absorbers
    • 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
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Bolts, Nuts, And Washers (AREA)
  • Dowels (AREA)
  • Vibration Prevention Devices (AREA)
  • Springs (AREA)
  • Insulators (AREA)

Abstract

A bush (10) for receiving a fastening screw (40) is proposed, which bush serves for connecting a first component (20) to a second component (30). The bush (10) has a metallic sleeve (11), onto the outer circumferential surface (13) of which a flexible sheathing (16) of an elastomer is vulcanized. <IMAGE>

Description

Vibration-dampina bush Prior art The invention relates to a vibration-damping bush for a fastening screw of the generic type of the main claim. When fitting in particular components which are capable of resonating onto machine elements, there is the requirement to damp the transmission of vibrations of the machine elements to the component capable of resonating or to isolate the component acoustically. Owing to the low thermal stability of plastic components, there is also the requirement for a thermal isolation of these components. It is generally known for the vibration damping or acoustic isolation between component and machine element to attach vibration damping elements, such as for example rubber discs or the like.For absorbing axial stresses of the fastening screws, shims which to the greatest extent cannot be deformed are necessary in addition to the rubber discs.
Advantages of the invention The invention with the characterizing features of the main claim has the advantage that a single component can be used both for the vibration damping and for the absorption of the axial stresses of the fastening screws.
Advantageous developments of the invention are possible by the measures specified in the subclaims. Of particular advantage is the captiveness of fastening screw and bush. The captiveness of bush, fastening screw and component contributes furthermore, to the fact that the component can be used in the preassembled state.
Drawing An exemplary embodiment of the invention is explained in more detail in the drawing and in the following description. Figure 1 shows a sectional representation of a bush according to the invention and Figure 2 shows a sectional representation of a second embodiment of the bush according to the invention in interaction with components to be connected.
Exemplary embodiment The bush 10 according to Figure 1 has a sleeve 11 with a bore 12 and a circumferential surface 13, the bush 10 having a height h. Formed onto the sleeve 11 is a disc 14, which in the present exemplary embodiment is realized, for example, by pressing the sleeve 11 onto a single disc. At the other end face 15', the sleeve 11 is configured with a wall thickening 15, which serves for increasing the bearing surface of the sleeve 11.
The outer circumferential surface 13 is provided with a flexible sheathing 16, which is pro.duced by vulcanizing an elastomer, for example rubber, onto the sleeve 11. Understood here by elastomer are any types of flexible plastics. The sheathing 16 is taken up to the disc 14 and has there a thickening 17. On the remaining circumferential surface 13 of the sleeve 11, the sheathing 16 is uniformly formed. In this region of the sheathing 16, there may be formed on, according to Figure 2, a bead 18, which is configured for example in a circumferential form.
The bore 12 serves for receiving a fastening screw 40 according to Figure 2. The surface of the bore 12 is provided with a flexible lining 19. The lining 19 has a clear width d1 and reaches, for example, down to a depth t1, so that the remaining section of the bore 12, with a depth t2, has no lining, t2 being equal to h - t,.
The clear width d, is slightly smaller than the thread diameter of the fastening screw, so that the fastening screw 40 can be inserted through the bore 12 with little expenditure of force. Like the sheathing 16, the lining 19 is produced by vulcanizing on an elastomer. The partial lining of the bore 12 makes it possible for the thread of the fastening screw 40 inserted into the bore 12 to be able to be pushed back to the greatest extent into the bore 12 and at the same time is held captively in the bore 12.
Figure 2 shows a first component 20, which is connected to the fastening screw 40 by a second component 30. The fastening screw 40 has a screw head 41, a screw shank 42, with a diameter D1, and a thread 43, with a thread diameter D2.
The first component 20 has a depression 21, which is adjoined by a through-hole 22. Formed between depression 21 and through-hole 22 is an axial shoulder 23, which is expediently configured as a slope descending towards the through-hole 22. On the side opposite the depression 21, the through-hole 22 is adjoined by a relief 24. The second component 30 has a threaded bore 31, into which the thread 43 of the fastening screw 40 is screwed.
In the case of the bush 10 according to Figure 2, the lining 19 extends over the entire surface of the bore 12, including over the end face 15' of the sleeve 11, in this case the thread 43 not being able to be pushed back into the bore 12, as in the case of the sleeve according to Figure 1.
The bush 10 is inserted, according to Figure 2, into the through-hole 22, the thickening 17 supporting itself on the axial shoulder 23. The height h of the bush 10 is in this case chosen such that the bush 10 protrudes slightly out of the first component 20, so that in the fitted state the bush 10 supports itself by the annular surface 15', or by the elastomer covering the annular surface 15', on the second component 30.
The diameter of the through-hole 22 is in this case chosen such that the bead 18 can, on account of its flexible action, be pressed through with little expenditure of force and the bead 18 positions itself in the depression 24. This ensures that the bush 10 is held captively in the component 20. The fastening screw 40, guided in the bore 12 of the sleeve 10, rests by the screw head 41 on the disc 14. Upon screwing of the fastening screw 40 into the threaded bore 31 of the second component 30, the thickening 17 is pressed onto the axial shoulder 23, so that, on account of the flexible action of the sheathing 16 against the axial shoulder 23, a seal can be realized between component 20 and bush 10.

Claims (9)

Claims
1. Vibration-damping bush for receiving a fastening screw, characterized in that a flexible sheathing (16) of an elastomer is vulcanized at least partially onto the outer circumferential surface (13) of a metallic sleeve (11).
2. Bush according to Claim 1, characterized in that the sleeve (11) has on the bearing surface of the fastening screw (40) a disc-shaped formation (14).
3. Bush according to Claim 2, characterized in that, adjoining the disc-shaped formation (14), the flexible sheathing (16) has a thickening (17).
4. Bush according to Claim 1, characterized in that the through-bore (12) of the sleeve (11) is configured at least partially with a flexible lining (19).
5. Bush according to Claim 4, characterized in that the lining 19 has a clear width d1 which is slightly smaller than the thread diameter of the fastening screw (40).
6. Bush according to Claim 4, characterized in that the lining (19) is configured down to a depth t of the through-bore (12) of the sleeve (11) and in that the remaining depth t2 corresponds approximately to the length of the thread (43) of the fastening screw (40).
7. Bush according to Claim 1, characterized in that the sheathing (16) is configured with a bead (18) in such a way that, as captivation, the bead (18) engages behind a through-hole of the part (20) to be connected.
8. Bush according to Claim 1, characterized in that, at the end face opposite the disc-shaped formation (14), the sleeve (11) has a wall thickening (15) for the formation of an enlarged annular surface (15').
9. A vibration damping bush substantially as herein described with reference to the accompanying drawing.
GB9515481A 1994-08-11 1995-07-28 Vibration-damping bush Expired - Fee Related GB2292434B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE9412946U DE9412946U1 (en) 1994-08-11 1994-08-11 Anti-vibration bushing

Publications (3)

Publication Number Publication Date
GB9515481D0 GB9515481D0 (en) 1995-09-27
GB2292434A true GB2292434A (en) 1996-02-21
GB2292434B GB2292434B (en) 1996-11-27

Family

ID=6912261

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9515481A Expired - Fee Related GB2292434B (en) 1994-08-11 1995-07-28 Vibration-damping bush

Country Status (3)

Country Link
DE (1) DE9412946U1 (en)
FR (1) FR2723626B1 (en)
GB (1) GB2292434B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2340794A (en) * 1998-08-20 2000-03-01 Rover Group Subframe mounting
GB2418709B (en) * 2004-09-29 2007-10-10 Rolls Royce Plc Damped assembly
US20150303660A1 (en) * 2014-04-21 2015-10-22 Toyota Jidosha Kabushiki Kaisha In-vehicle structure for inverter and bracket unit for inverter
CN108386427A (en) * 2017-02-02 2018-08-10 福特全球技术公司 Insertion piece for joint element

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10214417C1 (en) * 2002-03-30 2003-08-14 Draebing Kg Wegu Passive vibration absorber has internal diameter of outer shell at least as great as mean of minimum internal diameter and maximum external diameter of main mass body
DE102005009677B4 (en) * 2005-02-28 2007-01-04 Carl Freudenberg Kg vibration absorber
DE102007032934A1 (en) * 2007-07-14 2009-01-15 Zf Friedrichshafen Ag bearing arrangement
DE202009017083U1 (en) 2009-12-19 2010-03-04 Viking Gmbh implement
EP3299639B1 (en) * 2016-09-23 2020-07-22 E. Hawle Armaturenwerke GmbH Compensation element and system for vibration dampening

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3532319A (en) * 1968-04-23 1970-10-06 Outboard Marine Corp Vibration isolating mount
GB1295485A (en) * 1969-12-08 1972-11-08
GB1386163A (en) * 1971-05-25 1975-03-05 Tsunoda K Vibrationdamped tubular casing
GB1390392A (en) * 1971-02-20 1975-04-09 Jorn R Bushing
GB2075440A (en) * 1980-03-26 1981-11-18 Chalmers Wallace Gordon Vehicle suspension spigot assembly
US4410610A (en) * 1979-10-04 1983-10-18 Ab Tudor Pole bushing for batteries
GB2122555A (en) * 1982-05-13 1984-01-18 Porsche Ag An assembly for the vibration isolation attachment of a subframe or component holder to the main frame of a vehicle
US4667943A (en) * 1984-07-16 1987-05-26 Tokai Rubber Industries, Ltd. Resilient bushing
US4767108A (en) * 1985-07-18 1988-08-30 Toyota Jidosha Kabushiki Kaisha Elastic bushing assembly
WO1988009449A1 (en) * 1987-05-29 1988-12-01 Caterpillar Inc. Resilient load supporting and motion accommodating mounting apparatus
GB2243812A (en) * 1990-04-12 1991-11-13 Daimler Benz Ag A support mounting

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB975240A (en) * 1961-01-03 1964-11-11 Gould William Improvements in or relating to fastener assemblies
US3286577A (en) * 1964-05-13 1966-11-22 Atlas Bolt And Screw Company Shouldered washer and fastening element
JPS6199736A (en) * 1984-10-19 1986-05-17 Hitachi Ltd Vibration-proof device for compressor
EP0307851B1 (en) * 1987-09-14 1992-03-25 Sanden Corporation Mounting mechanism for an automotive air conditioning compressor
JPH0176577U (en) * 1987-11-10 1989-05-24
DE3842351A1 (en) * 1988-12-16 1990-06-28 Netter Gmbh Process and fastening for connecting vibrating objects
JPH02115979U (en) * 1989-03-07 1990-09-17
US4975008A (en) * 1989-03-31 1990-12-04 Illinois Tool Works, Inc. Fastener assembly with sealing grommet
JPH07729Y2 (en) * 1990-04-23 1995-01-11 矢崎総業株式会社 Waterproof ring for screw tightened connector housing

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3532319A (en) * 1968-04-23 1970-10-06 Outboard Marine Corp Vibration isolating mount
GB1295485A (en) * 1969-12-08 1972-11-08
GB1390392A (en) * 1971-02-20 1975-04-09 Jorn R Bushing
GB1386163A (en) * 1971-05-25 1975-03-05 Tsunoda K Vibrationdamped tubular casing
US4410610A (en) * 1979-10-04 1983-10-18 Ab Tudor Pole bushing for batteries
GB2075440A (en) * 1980-03-26 1981-11-18 Chalmers Wallace Gordon Vehicle suspension spigot assembly
GB2122555A (en) * 1982-05-13 1984-01-18 Porsche Ag An assembly for the vibration isolation attachment of a subframe or component holder to the main frame of a vehicle
US4667943A (en) * 1984-07-16 1987-05-26 Tokai Rubber Industries, Ltd. Resilient bushing
US4767108A (en) * 1985-07-18 1988-08-30 Toyota Jidosha Kabushiki Kaisha Elastic bushing assembly
WO1988009449A1 (en) * 1987-05-29 1988-12-01 Caterpillar Inc. Resilient load supporting and motion accommodating mounting apparatus
GB2243812A (en) * 1990-04-12 1991-11-13 Daimler Benz Ag A support mounting

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2340794A (en) * 1998-08-20 2000-03-01 Rover Group Subframe mounting
GB2340794B (en) * 1998-08-20 2002-03-27 Rover Group Subframe mounting
GB2418709B (en) * 2004-09-29 2007-10-10 Rolls Royce Plc Damped assembly
US20150303660A1 (en) * 2014-04-21 2015-10-22 Toyota Jidosha Kabushiki Kaisha In-vehicle structure for inverter and bracket unit for inverter
US9573538B2 (en) * 2014-04-21 2017-02-21 Toyota Jidosha Kabushiki Kaisha In-vehicle structure for inverter and bracket unit for inverter
CN108386427A (en) * 2017-02-02 2018-08-10 福特全球技术公司 Insertion piece for joint element
CN108386427B (en) * 2017-02-02 2022-07-05 福特全球技术公司 Insert for joining components

Also Published As

Publication number Publication date
DE9412946U1 (en) 1995-12-07
GB9515481D0 (en) 1995-09-27
FR2723626A1 (en) 1996-02-16
FR2723626B1 (en) 1996-12-06
GB2292434B (en) 1996-11-27

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20060728