GB2153484A - Resonance damper for a rotating body - Google Patents

Resonance damper for a rotating body Download PDF

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Publication number
GB2153484A
GB2153484A GB08402519A GB8402519A GB2153484A GB 2153484 A GB2153484 A GB 2153484A GB 08402519 A GB08402519 A GB 08402519A GB 8402519 A GB8402519 A GB 8402519A GB 2153484 A GB2153484 A GB 2153484A
Authority
GB
United Kingdom
Prior art keywords
rotor
rotating body
damper
inertia
auxiliary rotor
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Withdrawn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
GB08402519A
Other versions
GB8402519D0 (en
Inventor
Douglas James Rogers
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.)
Ferranti International PLC
Original Assignee
Ferranti PLC
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 Ferranti PLC filed Critical Ferranti PLC
Priority to GB08402519A priority Critical patent/GB2153484A/en
Publication of GB8402519D0 publication Critical patent/GB8402519D0/en
Publication of GB2153484A publication Critical patent/GB2153484A/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Withdrawn legal-status Critical Current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
    • F16F15/14Suppression 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
    • F16F15/1435Elastomeric springs, i.e. made of plastic or rubber
    • F16F15/1442Elastomeric springs, i.e. made of plastic or rubber with a single mass

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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)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

A resonance damper for a rotating body 6, 7 (e.g. the overhung rotor of an electric motor) comprises an auxiliary rotor 21 attached to the rotating body by a number of resilient members 22 (e.g. spring strip). A number of damping members 23 (e.g. blocks of rubber) are secured between the rotating body and the auxiliary rotor 21 to absorb vibrations transferred to the auxiliary rotor 21 by the resilient members 22. The axial and radial moments of inertia of the auxiliary rotor 21, and the compliances of the springs and dampers are so chosen that the two dynamic resonant frequencies of the rotating body are damped. <IMAGE>

Description

SPECIFICATION Resonance damper for a rotating body This invention relates to a resonance damper for a rotating body and in particlar for a high-speed motor having an external overhung rotor.
The majority of rotating bodies have a rotor supported on a shaft supported by two bearings for rotation inside a stator. Most, if not all, of the mass of the rotor is usually located between the bearings. This ensures that, if any vibration of the rotor should occur it is adequately restrained by the bearings.
Some types of high-speed motor have an external rotor rotating outside the stator, and in some situations it is necessary to support this rotor on one end of a shaft passing through the centre of the stator. The rotor is such a situation is far more sensitive to vibrations and external forces which, if unrestrained, could cause the stator and rotor to touch or at least cause the alignment of the motor to be impaired. Motors of this types posses one simple resonant frequency when stationary, but when rotation occurs two different resonant frequencies exist, one being higher than the static resonant frequency and the other being lower. The difference between these two resonant frequencies is proportional to the ratio of the axial inertia of the rotor to its radial inertia.
It is an object of the invention to provide a resonance damper for a rotating body which damps the above-mentioned resonant frequencies.
According to the present invention there is provided a resonance damper for a rotating body which includes an auxiliary rotor attached to the rotating body for rotation therewith by a number of resilient members and having a first moment of inertia measured along the axis of rotation and a second moment of inertia measured radially of said axis, and a number of damping members secured between the rotating body and the auxiliary rotor, the ratio between the first and second moments of inertia of the auxiliary rotor and the compliences of the resilient members and of the damping members being such that energy stored in the rotating body due to the resonant frequencies thereof is transferred to the auxiliary rotor by the resilient members and absorbed by the damping members.
The invention will now be described with reference to the accompanying drawings, in which: Figure 1 is a sectional diagram showing the construction of a known type of electric motor having an external overhung rotor; Figure 2 is a similar view of a motor incorporating the invention; and Figure 3 is an end view of the motor of Figure 2, Referring now to Figure 1, the known motor comprises a stator 1 secured to a base 2. Inside the stator 1 are two bearings 3 and 4 supporting a central shaft 5. On this shaft is mounted the rotor comprising a disc portion 6 and a flange portion 7, the latter substantially covering the stator 1. The method of construction will clearly allow some movement of the rotor about an axis passing approximately through the centre of the outer bearing 4, due to resilience of the shaft 5.The rotor has an axial inertia, measured about the axis of rotation, and a radial inertia measured perpendicular to the axis, and the ratio between these two determines the difference between the two resonant frequencies referred to above. The forces resulting from these resonant frequencies may cause sufficient movement of the rotor to allow it to touch the stator when rotating or to cause excessive misalignment, clearly an undesirable situation.
Figures 2 and 3 show how the resonance damper of the invention may be added to the motor of Figure 1 so as to reduce the susceptibility to forced resonances to an acceptable level. The existing motor is modified by the addition of an auxiliary rotor in the form of a tube 21 attached to the flange 7 of the rotor by means of a number of resilient members 22, three being shown in Figure 3.
In addition a number of dampers 23 are provided, these may be blocks of resilient material secured between the tube 21 and the flange 7 of the rotor.
Again, three are shown in Figure 3 equally spaced between the resilient members 22. The resilient members may conveniently be some form of diaphragm spring or spring strip, whilst the damping members may be blocks of resilient energy-absorbing material such as rubber.
The auxiliary rotor 21 should have substantially the same static resonant frequency as the rotor of the motor, and this is obtained by suitable adjustment of the compliance of the resilient members 22.
The compliance of the resilient members may be varied by changing their shape or dimensions, whilst the damping effect of the damping members depends upon their dimensions and the material used.
In operation, since the rotor and the auxiliary rotor 21 have substantially the same resonant frequency, when resonance occurs the auxiliary rotor draws energy from the rotor and dissipates it in the dampers 23. It is, of course, well known to provide a damper which will effectively damp a single resonant frequency in a vibrating body. However, the invention described in this specification makes it possible to damp out simultaneously the two resonant frequencies which exist in any rotating body.
The auxiliary rotor 21 may take a different form, though the tubular shape shown in the drawings is one of the simplest to produce. Alternatively a pair of spaced parallel rings may be used with much the same effect.
The inertias of the auxiliary rotor and of the main rotor need not necessarily be in the 5:1 ratio referred to above. However, if the ratio is much above 10:1 then tuning the resonant frequency of the auxiliary rotor becomes difficult. If the ratio is reduced as low as 1:1 then the need to use a tuned damper is unnecessary and the effect could be achieved by simply placing a damping material between the rotor and auxiliary rotor. In situations where the rotor of the motor might be expected to spin at speeds in excess of 10,000rpm, it is necessary to maintain the ratio of axial to radial inertias of the complete rotating assembly to a value greater than 1.5 to 1, and the ratio of axial to radial inertias of the auxiliary rotor to within 0.1 of this.
In addition, the resonant frequency of the auxiliary rotor at zero spin speed should be between 70% and 110% of that for the complete rotor assembly.
The above description has described a motor in which the auxiliary rotor is attached to the end of the rotor nearest to the disc portion 6. However, with suitable adjustment of its mass and of the compliance of the resilient members 22, the auxiliary rotor may be attached to any desired region of the rotor.
A resonance damper of similar form may be used with other types of motor than those with external rotors. Conventional motors with the rotor inside the stator may have substantial masses located outside the bearings and may therefore require a similar sort of resonance damper. Similarly, the same form of damper may be used with rotating bodies other than electric motors.

Claims (8)

1. A resonance damper for a rotating body, which includes an auxiliary rotor attached to the rotating body for rotation therewith by a number of resilient members and having a first moment of inertia measured along the axis of rotation and a second moment of inertia measured radially of said axis, and a number of damping members secured between the first and second moments of inertia of the auxiliary rotor and the compliences of the resilient members and of the damping members being such that energy stored in the rotating body due to the resonant frequencies thereof is transferred to the auxiliary rotor by the resilient members and absorbed by the damping members.
2. A damper as claimed in Claim 1 in which the auxiliary rotor is in the form of a tube supported coaxially with the rotating body.
3. A damper as claimed in either of Claims 1 or 2 in which the auxiliary rotor is attached to the rotating body by at least three resilient members and at least three damping members.
4. A damper as claimed in any one of Claims 1 to 3 in which the rotating body is the rotor of an electric motor
5. A damper as claimed in any one of the preceding claims in which the motor has an overhung rotor supported at one end by bearings, the auxiliary rotor being attached to the rotor of the motor at the end of the rotor nearest to said bearings.
6. A damper as claimed in any one of the preceding claims in which the ratio of the axial moment of inertia of the rotating body to the radial moment of inertia of the rotating body is greater than 1.5 to 1.
7. A damper as claimed in Claim 6 in which the raio of the axial moment of inertia of the auxiliary rotor to the radial moment of inertia of the auciliary rotor is with 0.1 of the ratio of the inertias of the rotating body.
8. A resonance damper for a rotary electric motor substantially as herein described with reference to Figures 2 and 3 of the accompanying drawings.
GB08402519A 1984-01-31 1984-01-31 Resonance damper for a rotating body Withdrawn GB2153484A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08402519A GB2153484A (en) 1984-01-31 1984-01-31 Resonance damper for a rotating body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08402519A GB2153484A (en) 1984-01-31 1984-01-31 Resonance damper for a rotating body

Publications (2)

Publication Number Publication Date
GB8402519D0 GB8402519D0 (en) 1984-03-07
GB2153484A true GB2153484A (en) 1985-08-21

Family

ID=10555817

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08402519A Withdrawn GB2153484A (en) 1984-01-31 1984-01-31 Resonance damper for a rotating body

Country Status (1)

Country Link
GB (1) GB2153484A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2386779A1 (en) * 2010-05-11 2011-11-16 Converteam Technology Ltd Rotors for electrical machines

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB389065A (en) * 1930-06-06 1933-03-09 Reichsverband Der Automobilind Improvements in vibration damping devices
GB480223A (en) * 1936-05-11 1938-02-18 Maschf Augsburg Nuernberg Ag Improvements in vibration dampers for shafts
GB556849A (en) * 1941-09-20 1943-10-25 Ford Motor Co Improvements in a vibration damper
GB1001105A (en) * 1961-04-24 1965-08-11 Schwitzer Corp Tuned friction damper
GB1048617A (en) * 1963-05-29 1966-11-16 Schwitzer Corp Vibration damper
GB2121913A (en) * 1982-06-11 1984-01-04 Hasse & Wrede Gmbh Torsional vibration damper with viscous damping medium

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB389065A (en) * 1930-06-06 1933-03-09 Reichsverband Der Automobilind Improvements in vibration damping devices
GB480223A (en) * 1936-05-11 1938-02-18 Maschf Augsburg Nuernberg Ag Improvements in vibration dampers for shafts
GB556849A (en) * 1941-09-20 1943-10-25 Ford Motor Co Improvements in a vibration damper
GB1001105A (en) * 1961-04-24 1965-08-11 Schwitzer Corp Tuned friction damper
GB1048617A (en) * 1963-05-29 1966-11-16 Schwitzer Corp Vibration damper
GB2121913A (en) * 1982-06-11 1984-01-04 Hasse & Wrede Gmbh Torsional vibration damper with viscous damping medium

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2386779A1 (en) * 2010-05-11 2011-11-16 Converteam Technology Ltd Rotors for electrical machines
WO2011141126A1 (en) * 2010-05-11 2011-11-17 Converteam Technology Ltd Rotors for electrical machines
US20130057092A1 (en) * 2010-05-11 2013-03-07 Ge Energy Power Conversion Technology Ltd Rotors for electrical machines
CN103026096A (en) * 2010-05-11 2013-04-03 通用电气能源电力转化技术有限公司 Rotors for electrical machines
JP2013526683A (en) * 2010-05-11 2013-06-24 ジーイー エナジー パワー コンバージョン テクノロジー リミティド Rotor for electrical equipment
US9683628B2 (en) * 2010-05-11 2017-06-20 Ge Energy Power Conversion Technology Ltd Vibration damping in rotor assembly

Also Published As

Publication number Publication date
GB8402519D0 (en) 1984-03-07

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