GB2162611A - A rotary vibration damper - Google Patents

A rotary vibration damper Download PDF

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Publication number
GB2162611A
GB2162611A GB08518591A GB8518591A GB2162611A GB 2162611 A GB2162611 A GB 2162611A GB 08518591 A GB08518591 A GB 08518591A GB 8518591 A GB8518591 A GB 8518591A GB 2162611 A GB2162611 A GB 2162611A
Authority
GB
United Kingdom
Prior art keywords
vibration damper
rotary vibration
belt pulley
damper
pulley unit
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
GB08518591A
Other versions
GB8518591D0 (en
GB2162611B (en
Inventor
Hans Gebhardt
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.)
MAN AG
Original Assignee
MAN Maschinenfabrik Augsburg Nuernberg 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 MAN Maschinenfabrik Augsburg Nuernberg AG filed Critical MAN Maschinenfabrik Augsburg Nuernberg AG
Publication of GB8518591D0 publication Critical patent/GB8518591D0/en
Publication of GB2162611A publication Critical patent/GB2162611A/en
Application granted granted Critical
Publication of GB2162611B publication Critical patent/GB2162611B/en
Expired 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
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/131Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses
    • F16F15/133Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses using springs as elastic members, e.g. metallic springs
    • F16F15/136Plastics springs, e.g. made of rubber
    • 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
    • F16F15/14Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers
    • F16F15/1407Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers the rotation being limited with respect to the driving means
    • F16F15/1414Masses driven by elastic elements
    • 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
    • F16HGEARING
    • F16H55/00Elements with teeth or friction surfaces for conveying motion; Worms, pulleys or sheaves for gearing mechanisms
    • F16H55/32Friction members
    • F16H55/36Pulleys
    • F16H2055/366Pulleys with means providing resilience or vibration damping

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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)
  • Pulleys (AREA)

Abstract

A rotary vibration damper comprising a primary member (1) mountable on a rotary shaft and a radially-outer secondary member (2) mounted on the primary member (1) by means of a resilient member 3, e.g. of rubber. The secondary member 2 comprises a V-belt pulley unit. In order to allow interchangeability, the secondary member (2) comprises a plurality of parts, i.e. the V-belt pulley unit (5) and a support (4). Optionally the secondary member (2) further comprises an annular mass (6). <IMAGE>

Description

SPECIFICATION A rotary vibration damper This invention relates to a rotary vibration damper.
A torsional vibration damper is disclosed in for example, DE-OS 25 37 390. It consists of a fly wheel-type ring (also called secondary member), a flange (also called primary member) and an intermediate rubber layer. In this arrangement, the primary member is rigidly screwed to a crank shaft and, for compactness, the secondary member is formed as a V-belt pulley (as a single solid part) for driving auxiliary machines (for example a dynamo or a motor-driven water pump). The resilient connection by means of the rubber is free in this damper, i.e. primary and secondary members are joined together non-positively by pressure. The object of the damper is to damp the torsional vibrations of the crank shaft.
To prevent the damper from being actuated in the range of harmless vibrational deflections (unnecessary temperature evolution), the damper is tuned to resonance with the system to be damped.
This is achieved by suitable dimensioning of the secondary member and the rubber mass.
A vibration damper of this type, therefore, begins to operate when resonant speeds occur, the vibratory system being split into a further form of vibration with nodes in the damper by the resilient connection of the secondary member. Harmful resonances can be effectively damped by intentional tuning.
If a spring-mass system tuned and designed for a specific purpose or application is provided with a different moment of inertia, this is usually accompanied by re-determination of the damper.
A further problem resides in the fact that V-belt pulleys of which the effective diameter, belt tracks and belt widths have been altered relative to the original belt pulley make it necessary to re-design the vibration damper.
In other words, the usefulness of a typical damper is based on the following factors: a) Suitability for a specific size of fly wheel (considered from the moment of inertia).
b) suitability for a specific required auxiliary machine V-belt drive.
Compliance with the foregoing points - individually or simultaneously - is synonymous in the current design (the secondary member acting as a Vbelt pulley is formed as a single solid part) with redesign of the damper, i.e. a new damper with primary member and adapted secondary member now have to be connected and attached using the rubber layer. The composition and storage of the damper are correspondingly expensive.
An object of the invention is to provide a rotary vibration damper which is more suitable for the various applications with respect to change of Vbelt pulley unit or with respect to a possible change in the mass of inertia, the conversion and adaptation being achievable in a simple and inexpensive manner. Moreover, the provision and storage of the dampers or of the damper parts should be simplified and this will also reduce costs.
The invention provides a rotary damper as claimed in claim 1.
This division of the secondary member into a plurality of parts according to its function represents a particularly economic solution. The primary member together with the rubber layer and the support may be obtained from a damper manufacturer as one unit in relatively large numbers at a corresponding price. It is necessary to store only this assembly.
Suitable or appropriate V-belt pulley units which are connected in the appropriate manner to the support may be used for the corresponding auxiliary machine drives or for each specific application.
Finally, an additional mass which is connected to the support in the same manner as the V-belt pulley unit can also be provided if necessary. This additional fly wheel-type ring is used if the V-belt pulley unit formed as a solid part does not have sufficient mass or if the damper needs to be used for a mass of inertia which may have been altered.
This additional mass is obviously also used if a Vbelt pulley unit made of sheet metal is used instead of a solid one.
The type of connection of V-belt pulley unit and additional mass to the support may be positive or non-positive (for example as a longitudinal pressure fit or transverse pressure fit) or can be designed as a screw connection.
Embodiments of the invention will now be described with reference to the accompanying drawings, wherein: Figure 1 is a longitudinal section through a first embodiment of a damper.
Figure 2 is a longitudinal section through a second embodiment of a damper.
Figure 3 is a longitudinal section through a third embodiment of a damper.
Figure 4 is a longitudinal section through a fourth embodiment of a damper, and Figure 5 is a longitudinal section through a fifth embodiment of a damper.
In the drawings, a torsional vibration damper comprises a primary member 1 formed as a flange screwed to a crank shaft (not shown), and a secondary member 2 arranged radially outwardly of the primary member 1. A resilient damping layer 3 formed of rubber is provided between the two members 1, 2. There is no physical connection between the rubber layer 3 and the members 1, 2, i.e.
the rubber is only compressed between the members 1, 2.
For compactness in this type of damper, a V-belt pulley unit for driving auxiliary machines is fitted to the secondary member 2. In the past, this was actually formed integrally with the secondary member (fly wheel-type ring).
In accordance with the invention, the secondary member 2 comprises a plurality of parts, i.e. a secondary part support 4, a V-belt pulley unit 5 and an additional mass 6 (additional fly wheel-type ring).
The additional mass 6 is not always necessary, as explained below.
Figure 1 shows a solid V-belt pulley unit 5 which simultaneously acts as a fly wheel-type ring. In Figures 2, 3, 4and 5, a ring 6 is provided in addition to the V-belt pulley unit 5. The additional ring 6 is ,used, for example, if the mass (the moment of inertia) of the V-belt pulley unit selected for the specific application is not sufficient.
The damper will also be adapted to new parameters, for example if the moment of inertia on the fly wheel side is altered, by means of an additional ring. If a V-belt pulley unit made from sheet metal is used (see Figures 4 and 5), the additional ring 6 is invariably required to provide the necessary mo ment of inertia.
The V-belt pulley unit 5 and the additional ring 6 are connected positively or merely by friction to the support 4 forming a unitary assembly with the rubber layer 3 and the primary member 1. The connection may be in the form of e.g. a longitudi nal pressure fit, a transverse pressure fit or a screw connection.
The formation of the secondary member 2 into a number of parts, depending on its function, makes the provision and storage for line assembly and supply of spare parts more economic than in the past. In order to repair "defective dampers" it is necessary to provide only the less expensive as sembly of primary member 1, intermediate rubber layer 3, and support 4. The exchanged parts such as ring mass 6 and V-belt pulley unit 5 can be pressed out and used again.

Claims (7)

1. A rotary vibration damper comprising a pri mary member mountable on a rotary shaft, and a radially-outer secondary member connected to the primary member by means of a resilient damping member, wherein the secondary member is formed of a plurality of parts comprising a support and a V-belt pulley unit.
2. A rotary vibration damper as claimed in claim 1, wherein the support is connected to the primary member by means of the resilient damp ing member.
3. A rotary vibration damper as claimed in claim 1 or 2, wherein the secondary member fur ther comprises an annular mass.
4. A rotary vibration damper as claimed in claim 1, 2 or 3, wherein the V-belt pulley unit or the annular mass is positively or non-positively connected to the support by means of a longitudi nal pressure fit, a transverse fit or a screw connec tion.
5. A rotary vibration damper as claimed in any one of the preceding claims, wherein the V-belt pulley unit is formed from sheet metal.
6. A rotary vibration damper substantially as herein described with reference to any one of the accompanying drawings.
7. A multi-cylinder engine having a crank shaft connected to a rotary vibration damper as claimed in any one of the preceding claims.
GB08518591A 1984-08-04 1985-07-23 A rotary vibration damper Expired GB2162611B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19843428894 DE3428894A1 (en) 1984-08-04 1984-08-04 VIBRATION DAMPER FOR DAMPING ROTATING MASSES

Publications (3)

Publication Number Publication Date
GB8518591D0 GB8518591D0 (en) 1985-08-29
GB2162611A true GB2162611A (en) 1986-02-05
GB2162611B GB2162611B (en) 1987-11-18

Family

ID=6242427

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08518591A Expired GB2162611B (en) 1984-08-04 1985-07-23 A rotary vibration damper

Country Status (2)

Country Link
DE (1) DE3428894A1 (en)
GB (1) GB2162611B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5966996A (en) * 1993-08-21 1999-10-19 Firma Carl Freudenberg Annular vibration damping machine element
US6684735B2 (en) * 2001-03-13 2004-02-03 Fukoku Co., Ltd. Torsional damper
DE102006039362A1 (en) * 2006-08-22 2008-03-06 Schaeffler Kg Drive wheel for ancillary units in IC engine has a two part construction rim or hub with integral space for damping means

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3612370A1 (en) * 1986-04-12 1987-10-15 Bayerische Motoren Werke Ag VIBRATION DAMPER, ESPECIALLY FOR THE CRANKSHAFT OF A PISTON PISTON COMBUSTION ENGINE
EP0283855B1 (en) * 1987-03-10 1992-06-10 Fujikiko Kabushiki Kaisha Auxiliary drive apparatus
DE3816324A1 (en) * 1987-07-07 1989-01-19 Metzeler Gmbh TORQUE DAMPER
DE10209723B4 (en) 2002-03-06 2005-01-27 Claas Selbstfahrende Erntemaschinen Gmbh Device for damping vibrations in traction drives
DE102004035596A1 (en) * 2004-07-22 2006-03-16 Zexel Valeo Compressor Europe Gmbh Moments transferring device for supercharger, has belt pulley components and hub components, where auxiliary mass is assigned to both components, such that relationship of mass inertial moments of both components is increased
FR3014988A1 (en) * 2013-12-18 2015-06-19 Peugeot Citroen Automobiles Sa ACCESSORY PULLEY EQUIPPING AN INTERNAL COMBUSTION ENGINE.

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1312941A (en) * 1970-04-16 1973-04-11 Holset Engineering Co Torsional vibration damper

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1962746A (en) * 1929-06-27 1934-06-12 Chrysler Corp Vibration damper
US1944233A (en) * 1929-06-27 1934-01-23 Chrysler Corp Vibration damper
US1905475A (en) * 1930-02-01 1933-04-25 Chrysler Corp Vibration damper
US1874515A (en) * 1930-04-11 1932-08-30 Continental Motors Corp Vibration damper
DE588245C (en) * 1930-06-11 1933-11-15 Budd Wheel Co Vibration damper
US1949520A (en) * 1931-06-16 1934-03-06 Hudson Motor Car Co Vibration damper
US2828616A (en) * 1955-11-17 1958-04-01 Gen Motors Corp Power transmitting element with damping means
DE2537390A1 (en) * 1975-08-22 1977-07-14 Daimler Benz Ag Vibration damper for engine crankshaft - has convex outer ring retained on hub by humped surface if rubber fails
DE2744406A1 (en) * 1977-10-03 1979-04-12 Daimler Benz Ag Piston engine shaft pulley disc - has closed cover over bearer sleeve face side turned away from shaft fixture

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1312941A (en) * 1970-04-16 1973-04-11 Holset Engineering Co Torsional vibration damper

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5966996A (en) * 1993-08-21 1999-10-19 Firma Carl Freudenberg Annular vibration damping machine element
US6684735B2 (en) * 2001-03-13 2004-02-03 Fukoku Co., Ltd. Torsional damper
DE102006039362A1 (en) * 2006-08-22 2008-03-06 Schaeffler Kg Drive wheel for ancillary units in IC engine has a two part construction rim or hub with integral space for damping means

Also Published As

Publication number Publication date
DE3428894A1 (en) 1986-02-13
GB8518591D0 (en) 1985-08-29
GB2162611B (en) 1987-11-18

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

Effective date: 19940723