GB2173879A - Torsional vibration damper - Google Patents

Torsional vibration damper Download PDF

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Publication number
GB2173879A
GB2173879A GB08603739A GB8603739A GB2173879A GB 2173879 A GB2173879 A GB 2173879A GB 08603739 A GB08603739 A GB 08603739A GB 8603739 A GB8603739 A GB 8603739A GB 2173879 A GB2173879 A GB 2173879A
Authority
GB
United Kingdom
Prior art keywords
flywheel
cavity
torsional vibration
flyring
damper
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.)
Withdrawn
Application number
GB08603739A
Other versions
GB8603739D0 (en
Inventor
Bernard Bihr
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.)
GKN Driveline International GmbH
Original Assignee
Uni Cardan AG
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 Uni Cardan AG filed Critical Uni Cardan AG
Publication of GB8603739D0 publication Critical patent/GB8603739D0/en
Publication of GB2173879A publication Critical patent/GB2173879A/en
Withdrawn legal-status Critical Current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
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/16Suppression of vibrations in rotating systems by making use of members moving with the system using a fluid or pasty material
    • F16F15/167Suppression of vibrations in rotating systems by making use of members moving with the system using a fluid or pasty material having an inertia member, e.g. ring
    • F16F15/173Suppression of vibrations in rotating systems by making use of members moving with the system using a fluid or pasty material having an inertia member, e.g. ring provided within a closed housing

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Road Signs Or Road Markings (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Mechanical Operated Clutches (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

A torsional vibration damper comprises a flywheel for an internal combustion engine, with a cavity 3 defined in a radially outermost part 1 of the flywheel, containing a flyring 4. A viscous medium is contained in the gap 7 between the flyring and the walls of the cavity 3, to provide damping by shearing in the viscous medium when relative rotation between the flywheel and flyring occurs. The damper is thus provided in the flywheel itself rather than in a separate damper unit. <IMAGE>

Description

SPECIFICATION Torsional vibration damper This invention relates to a torsional vibration damper, for use in damping torsional vibration in the crankshaft of an internal combustion engine. The invention is particularly, although not exclusively, applicable to motor vehicle engines.
A known form of torsional vibration damper comprises a housing, e.g. a hub, adapted to be fitted to the rotary element in which vibration is to be damped, the housing defining an annular cavity within which is contained an annular inertia member (hereinafter termed the flyring) able to move angularly relatively to the housing, the remaining space in the cavity being filled with a viscous medium. The viscous medium damps relative angular movement between the housing and element therein, thereby damping torsional vibration in the rotary part to which the housing is attached.
An example of such a damper for an internal combustion engine is disclosed in DE-OS 2644808. A disadvantage of this damper is that it comprises a separate housing unit which requires to be connected to the engine.
As a result, the weight of the engine is increased as is the space occupied thereby.
This is undesirable for motor vehicle application, where an increase in weight leads to an increase in fuel consumption, and hence light weight and compactness are desirable.
It is an object of the present invention to provide a torsional vibration damper which is incorporated in existing engine components, and hence does not have the above disadvantages attendant on separate dampers, nor require any changes in engine design.
According to the invention, we provide a torsional vibration damper in the form of a flywheel for an internal combustion engine, having a cavity containing an inertia member, guided for angular movement relative to the flywheel about the rotational axis thereof, and a viscous medium.
An advantage of disposing the torsional vibration damper in the flywheel, apart from that of not requiring a separate damper unit, is that the damping takes effect at the point where the power of the engine is delivered.
Preferably the inertia member comprises a flyring disposed in an annular cavity in a radially outermost region of the flywheel.
The invention will now be described by way of example with reference to the accompanying drawing, which is a diagrammatic section through part of a flywheel according to the invention.
The illustrated flywheel is adapted to be connected to the crankshaft of an internal combustion engine in known manner, e.g. by bolts, and to have a clutch assembly (shown diagrammatically in outline in the drawing) connected to it also in known manner. The flywheel is of somewhat cup-shaped configuration, and in its radially outermost part 1 is provided with an annular recess 3. The recess is closed by an annular cover 2 fitted to the flywheel and held in place, e.g. by deformation of the flywheel. The cover 2 has a screwed filler plug 8, which provides for introduction of a suitable viscous medium into the cavity 3.
Within the cavity 3 there is disposed an inertia member in the form of a flyring 4, freely rotatable relative to the flywheel. Guiding rings 6, e.g. of plastics material, guide the flyring 4 in such a way that it cannot contact the walls of the cavity 3. The viscous medium fills the gap 7 between the flyring and the walls of the cavity. It will be appreciated that relative rotational movement between the flywheel and flyring 4 causes shear in the viscous medium filling the cavity 3, thereby exerting a torsional damping effect.
The flywheel carries a starter ring gear 5 in known manner.
Because the flyring 4 is disposed in a radially outermost region of the flywheel, its damping effect on torsional vibration is maximized, without the complications of providing a separate damper as above described.
1. A torsional vibration damper in the form of a flywheel for an internal combustion engine, having a cavity containing an inertia member, guided for angular movement relative to the flywheel about the rotational axis thereof, and a viscous medium.
2. A flywheel according to Claim 1 wherein said inertia member comprises a flyring disposed in an annular cavity in a radially outermost region of the flywheel.
3. A flywheel for an internal combustion engine, substantially as hereinbefore described with reference to the accompanying drawing.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (3)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Torsional vibration damper This invention relates to a torsional vibration damper, for use in damping torsional vibration in the crankshaft of an internal combustion engine. The invention is particularly, although not exclusively, applicable to motor vehicle engines. A known form of torsional vibration damper comprises a housing, e.g. a hub, adapted to be fitted to the rotary element in which vibration is to be damped, the housing defining an annular cavity within which is contained an annular inertia member (hereinafter termed the flyring) able to move angularly relatively to the housing, the remaining space in the cavity being filled with a viscous medium. The viscous medium damps relative angular movement between the housing and element therein, thereby damping torsional vibration in the rotary part to which the housing is attached. An example of such a damper for an internal combustion engine is disclosed in DE-OS 2644808. A disadvantage of this damper is that it comprises a separate housing unit which requires to be connected to the engine. As a result, the weight of the engine is increased as is the space occupied thereby. This is undesirable for motor vehicle application, where an increase in weight leads to an increase in fuel consumption, and hence light weight and compactness are desirable. It is an object of the present invention to provide a torsional vibration damper which is incorporated in existing engine components, and hence does not have the above disadvantages attendant on separate dampers, nor require any changes in engine design. According to the invention, we provide a torsional vibration damper in the form of a flywheel for an internal combustion engine, having a cavity containing an inertia member, guided for angular movement relative to the flywheel about the rotational axis thereof, and a viscous medium. An advantage of disposing the torsional vibration damper in the flywheel, apart from that of not requiring a separate damper unit, is that the damping takes effect at the point where the power of the engine is delivered. Preferably the inertia member comprises a flyring disposed in an annular cavity in a radially outermost region of the flywheel. The invention will now be described by way of example with reference to the accompanying drawing, which is a diagrammatic section through part of a flywheel according to the invention. The illustrated flywheel is adapted to be connected to the crankshaft of an internal combustion engine in known manner, e.g. by bolts, and to have a clutch assembly (shown diagrammatically in outline in the drawing) connected to it also in known manner. The flywheel is of somewhat cup-shaped configuration, and in its radially outermost part 1 is provided with an annular recess 3. The recess is closed by an annular cover 2 fitted to the flywheel and held in place, e.g. by deformation of the flywheel. The cover 2 has a screwed filler plug 8, which provides for introduction of a suitable viscous medium into the cavity 3. Within the cavity 3 there is disposed an inertia member in the form of a flyring 4, freely rotatable relative to the flywheel. Guiding rings 6, e.g. of plastics material, guide the flyring 4 in such a way that it cannot contact the walls of the cavity 3. The viscous medium fills the gap 7 between the flyring and the walls of the cavity. It will be appreciated that relative rotational movement between the flywheel and flyring 4 causes shear in the viscous medium filling the cavity 3, thereby exerting a torsional damping effect. The flywheel carries a starter ring gear 5 in known manner. Because the flyring 4 is disposed in a radially outermost region of the flywheel, its damping effect on torsional vibration is maximized, without the complications of providing a separate damper as above described. CLAIMS
1. A torsional vibration damper in the form of a flywheel for an internal combustion engine, having a cavity containing an inertia member, guided for angular movement relative to the flywheel about the rotational axis thereof, and a viscous medium.
2. A flywheel according to Claim 1 wherein said inertia member comprises a flyring disposed in an annular cavity in a radially outermost region of the flywheel.
3. A flywheel for an internal combustion engine, substantially as hereinbefore described with reference to the accompanying drawing.
GB08603739A 1985-03-08 1986-02-14 Torsional vibration damper Withdrawn GB2173879A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853508237 DE3508237A1 (en) 1985-03-08 1985-03-08 TORQUE DAMPER

Publications (2)

Publication Number Publication Date
GB8603739D0 GB8603739D0 (en) 1986-03-19
GB2173879A true GB2173879A (en) 1986-10-22

Family

ID=6264572

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08603739A Withdrawn GB2173879A (en) 1985-03-08 1986-02-14 Torsional vibration damper

Country Status (5)

Country Link
JP (1) JPS61206843A (en)
DE (1) DE3508237A1 (en)
FR (1) FR2578613A1 (en)
GB (1) GB2173879A (en)
IT (3) IT8505264A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4848183A (en) * 1987-02-17 1989-07-18 Simpson Industries, Inc. Camshaft damper
US5931052A (en) * 1996-06-13 1999-08-03 Simpson International (Uk) Ltd. Crankshaft gear torsional vibration isolator assembly for an engine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3637383A1 (en) * 1986-11-03 1988-05-19 Uni Cardan Ag VIBRATION DAMPING DRIVE ELEMENT

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1504998A (en) * 1975-01-21 1978-03-22 Wallace Murray Corp Torsional vibration damper
GB1597760A (en) * 1977-03-30 1981-09-09 Hasse & Wrede Gmbh Torsional vibration damper housing a viscous damping medium
GB2121914A (en) * 1982-06-09 1984-01-04 Klaus Federn A damped rotary-oscillation or torsional vibration eradicator

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS509950A (en) * 1973-05-28 1975-01-31

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1504998A (en) * 1975-01-21 1978-03-22 Wallace Murray Corp Torsional vibration damper
GB1597760A (en) * 1977-03-30 1981-09-09 Hasse & Wrede Gmbh Torsional vibration damper housing a viscous damping medium
GB2121914A (en) * 1982-06-09 1984-01-04 Klaus Federn A damped rotary-oscillation or torsional vibration eradicator

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4848183A (en) * 1987-02-17 1989-07-18 Simpson Industries, Inc. Camshaft damper
US5931052A (en) * 1996-06-13 1999-08-03 Simpson International (Uk) Ltd. Crankshaft gear torsional vibration isolator assembly for an engine

Also Published As

Publication number Publication date
GB8603739D0 (en) 1986-03-19
IT8505264A0 (en) 1985-12-16
JPS61206843A (en) 1986-09-13
IT8505264A1 (en) 1987-06-16
IT8507158V0 (en) 1985-12-16
IT1187002B (en) 1987-12-16
DE3508237A1 (en) 1986-09-11
FR2578613A1 (en) 1986-09-12

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WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)