WO1998016760A2 - Vibration attenuation system - Google Patents

Vibration attenuation system Download PDF

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Publication number
WO1998016760A2
WO1998016760A2 PCT/GB1997/002730 GB9702730W WO9816760A2 WO 1998016760 A2 WO1998016760 A2 WO 1998016760A2 GB 9702730 W GB9702730 W GB 9702730W WO 9816760 A2 WO9816760 A2 WO 9816760A2
Authority
WO
WIPO (PCT)
Prior art keywords
mount
stiffness
machine
idle
support
Prior art date
Application number
PCT/GB1997/002730
Other languages
French (fr)
Other versions
WO1998016760A3 (en
Inventor
Ronnie Chi Nang Leung
Original Assignee
The Secretary Of State For Defence
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 The Secretary Of State For Defence filed Critical The Secretary Of State For Defence
Priority to AU45659/97A priority Critical patent/AU4565997A/en
Publication of WO1998016760A2 publication Critical patent/WO1998016760A2/en
Publication of WO1998016760A3 publication Critical patent/WO1998016760A3/en

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
    • F16F7/00Vibration-dampers; Shock-absorbers
    • F16F7/10Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/1005Vibration-dampers; Shock-absorbers using inertia effect characterised by active control of the mass
    • F16F7/1017Vibration-dampers; Shock-absorbers using inertia effect characterised by active control of the mass by fluid means
    • 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
    • F16F15/02Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • 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
    • F16F15/02Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/023Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means
    • F16F15/027Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means comprising control arrangements
    • F16F15/0275Control of stiffness
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/10Applications
    • G10K2210/128Vehicles
    • G10K2210/1282Automobiles
    • G10K2210/12822Exhaust pipes or mufflers
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/30Means
    • G10K2210/301Computational
    • G10K2210/3026Feedback
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/30Means
    • G10K2210/321Physical
    • G10K2210/3227Resonators
    • G10K2210/32271Active resonators
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K2210/00Details of active noise control [ANC] covered by G10K11/178 but not provided for in any of its subgroups
    • G10K2210/50Miscellaneous
    • G10K2210/51Improving tonal quality, e.g. mimicking sports cars

Definitions

  • vibration control may be by isolation of a vibrating source from its support using isolating mounts, or by absorbing vibrations in the body itself by attaching an absorber, e.g. for a machine, to absorb vibrations due to the machine's frequency of operation. In some cases both systems are used.
  • These systems for controlling vibration are expensive in terms of space, weight and materials, because each machine requires its own specialised mount and absorbing mass. This is particularly felt in aircraft and shi ⁇ s where space and weight are at a premium.
  • a vibration attenuation system comprises at least one operative machine, one idle machine and a support; wherein each machine is mounted on the support via respective operative and idle mounts; wherein the stiffness of each mount may be switched between an isolation mode and an abso ⁇ tion mode; and wherein the stiffness of the operative mount is switched to isolation mode and the stiffness of the idle mount is switched to absorption mode, such that vib ation in the support is minimised.
  • the present invention uses an idle machine and its mount to absorb vibrations in another operative machine installed on the same support.
  • the absorption mass and associated mounting of the prior art systems are no longer required, thereby reducing the overall size, weight and cost of the system.
  • each mount may be varied by disconnecting one part of the mount from the support and connecting another part of the mount dependent on the desired mode of operation, but preferably, each of the operative and idle mounts comprise a single mount, the stiffness of which is controllable.
  • each mount comprises controllable means for controlling the stiffness of the mount.
  • the controllable means comprises electro-rheological fluid.
  • the stiffness of the idle mount may be switched to one of a plurality of stiffness values. This allows the idle machine and its mounting to be used as an absorber for machines having different speeds of operation, which are on the same mount.
  • the stiffness of the idle mount in absorption mode is tuned for the operating frequency of the respective operative machine
  • the support is rigid
  • Figure 3 is a first example of a vibration control system according to the invention
  • Figure 4 is a second example of a vibration control system according to the invention
  • Figure 5 shows in more detail a mount for the system of Fig 3 or Fig 4
  • Figure 6 shows in more detail an alternative mount for the system of Fig 3 or Fig 4
  • FIG. 1 A conventional vibration control system is shown in Fig 1 in which a machine 1 is mounted to a support 2, which is fixed at both ends 3
  • the machine 1 has a mass m, and is attached via a first mounting 4 of stiffness ki to the support 2
  • a dummy weight 5 of mass m 2 is attached to the support 2 via a second mounting 6 of stiffness k 2
  • the mass of the dummy weight 5 and the stiffness of the second mounting 6 are chosen such that
  • m mass in kg
  • k stiffness in kgs "2
  • f the frequency to be controlled, such as the fundamental operating frequency of the machine
  • FIG. 2 A more complex vibration control system is shown in Fig 2 in which first and second machines 9,10 are mounted on a support 7 which is fixed at both ends 8
  • the first and second machines 9, 10 are attached to the support via first and second mountings 11 ,12 and first and second dummy weights 13,14 are attached to the support through third and fourth mountings 15,16
  • Such an arrangement may be extended to multiple machines, but it requires a dummy weight and mounting for each machine
  • the disadvantages of the systems shown in Figs 1 and 2 are the extra space, cost and weight associated with the dummy masses and their vibration mountings. This problem is accentuated when a machine is idle and particularly where a machine is a backup for another and thus unlikely to be operating all that often. This is common on aircraft or ships which need backup machines in place, but have limitations on space and weight.
  • FIG. 3 An example of a vibration attenuation system in accordance with the present invention is shown in Fig. 3.
  • the system has a pair of machines 17, 18 mounted via respective mounts 19,20 to a support 21 which is fixed at both ends 22.
  • one of the machines 17 is operative and the other machine 18 is idle.
  • the stiffness of the mount supporting the idle machine 18 is switched to an absorption mode which is adapted to the frequency of operation of the operative machine 17.
  • a mount with variable stiffness may be produced in several ways, such as switching between two mechanical mounts both connected to the idle machine, controlling hydraulic fluid in the mount or using a mount containing electro-rheological fluid which has different stiffness properties according to the voltage applied across it.
  • a support 23 has multiple machines 25 mounted via respective mounts 24.
  • the stiffness of each of these mounts 24 can be varied according to which machine is idle and which is operative, so that where machines are run at different times of day for different pu ⁇ oses, a machine not in use provides vibration abso ⁇ tion for one which is.
  • Fig. 5 shows an example of a mechanical mount for the present invention, e.g. springs or other resilient couplings, such as rubber.
  • Fig. 6 illustrates a mount whose stiffness is controlled using electro-rheological fluid.
  • An example of an electro-rheological fluid is silica spheres in water and glycerol.
  • the mount comprises a flexible housing 33, e.g. a rubber bladder, which contains the electro-rheological fluid 34.
  • This fluid has the property that application of a potential to it causes a change in viscosity. This property can be used to alter the stiffness of the mount according to the function it is to perform.
  • the potential can be made continuously variable by inserting a rheostat 35 in the circuit as shown in Fig. 6a so that the viscosity may be tuned to the stiffness required for a particular machine or a multiway switch 36 as shown in Fig. 6b can be connected to fixed predefined potentials.

Abstract

A vibration attenuation system comprises at least one operative machine (17), one idle machine (18) and a support (21). Each machine (17, 18) is mounted on the support (21) via respective operative and idle mounts (19, 20). The stiffness of each mount (19, 20) may be switched between an isolation mode and an absorption mode. The stiffness of the operative mount is switched to isolation mode and the stiffness of the idle mount is switched to absorption mode to minimise vibration in the support (21). The mounts can be mechanical mounts such as springs, which are connected or disconnected according to which mode is required, or can have variable stiffness, for example a mount whose stiffness is dependent upon a change in potential applied to an electro-rheological fluid causing a change in viscosity of the fluid. The system is particularly suitable for reducing vibration in aircraft or ships.

Description

VIBRATION ATTENUATION SYSTEM
This invention relates to a vibration attenuation system. Conventionally, vibration control may be by isolation of a vibrating source from its support using isolating mounts, or by absorbing vibrations in the body itself by attaching an absorber, e.g. for a machine, to absorb vibrations due to the machine's frequency of operation. In some cases both systems are used. These systems for controlling vibration are expensive in terms of space, weight and materials, because each machine requires its own specialised mount and absorbing mass. This is particularly felt in aircraft and shiϋs where space and weight are at a premium. In accordance with the present invention, a vibration attenuation system comprises at least one operative machine, one idle machine and a support; wherein each machine is mounted on the support via respective operative and idle mounts; wherein the stiffness of each mount may be switched between an isolation mode and an absoφtion mode; and wherein the stiffness of the operative mount is switched to isolation mode and the stiffness of the idle mount is switched to absorption mode, such that vib ation in the support is minimised.
The present invention uses an idle machine and its mount to absorb vibrations in another operative machine installed on the same support. The absorption mass and associated mounting of the prior art systems are no longer required, thereby reducing the overall size, weight and cost of the system.
The stiffness of each mount may be varied by disconnecting one part of the mount from the support and connecting another part of the mount dependent on the desired mode of operation, but preferably, each of the operative and idle mounts comprise a single mount, the stiffness of which is controllable.
This further reduces the degree of redundancy in the system by using the same mount, but altering its stiffness, rather than the mount having two different parts, only one of which is in use at any time.
Preferably, each mount comprises controllable means for controlling the stiffness of the mount.
Preferably, the controllable means comprises electro-rheological fluid. Preferably, the stiffness of the idle mount may be switched to one of a plurality of stiffness values. This allows the idle machine and its mounting to be used as an absorber for machines having different speeds of operation, which are on the same mount. Preferably, the stiffness of the idle mount in absorption mode is tuned for the operating frequency of the respective operative machine
This maximises vibration absorption and allows the stiffness to be tuned to specific machines Preferably, the support is rigid
Examples of a vibration attenuation system in accordance with the present invention will now be described and contrasted with conventional vibration control system with reference to the accompanying drawings in which - Figure 1 is a first conventional vibration control system, Figure 2 is a second conventional vibration control system,
Figure 3 is a first example of a vibration control system according to the invention, Figure 4 is a second example of a vibration control system according to the invention, Figure 5 shows in more detail a mount for the system of Fig 3 or Fig 4, and Figure 6 shows in more detail an alternative mount for the system of Fig 3 or Fig 4
A conventional vibration control system is shown in Fig 1 in which a machine 1 is mounted to a support 2, which is fixed at both ends 3 The machine 1 has a mass m, and is attached via a first mounting 4 of stiffness ki to the support 2 A dummy weight 5 of mass m2 is attached to the support 2 via a second mounting 6 of stiffness k2 Usually, to minimise vibration in the support, the mass of the dummy weight 5 and the stiffness of the second mounting 6 are chosen such that
1/2
(k2)
2πf
1/2
(m2)
where m is mass in kg, k is stiffness in kgs"2 and f is the frequency to be controlled, such as the fundamental operating frequency of the machine
A more complex vibration control system is shown in Fig 2 in which first and second machines 9,10 are mounted on a support 7 which is fixed at both ends 8 The first and second machines 9, 10 are attached to the support via first and second mountings 11 ,12 and first and second dummy weights 13,14 are attached to the support through third and fourth mountings 15,16 Such an arrangement may be extended to multiple machines, but it requires a dummy weight and mounting for each machine The disadvantages of the systems shown in Figs 1 and 2 are the extra space, cost and weight associated with the dummy masses and their vibration mountings. This problem is accentuated when a machine is idle and particularly where a machine is a backup for another and thus unlikely to be operating all that often. This is common on aircraft or ships which need backup machines in place, but have limitations on space and weight.
An example of a vibration attenuation system in accordance with the present invention is shown in Fig. 3. The system has a pair of machines 17, 18 mounted via respective mounts 19,20 to a support 21 which is fixed at both ends 22. In use, one of the machines 17 is operative and the other machine 18 is idle. The stiffness of the mount supporting the idle machine 18 is switched to an absorption mode which is adapted to the frequency of operation of the operative machine 17. A mount with variable stiffness may be produced in several ways, such as switching between two mechanical mounts both connected to the idle machine, controlling hydraulic fluid in the mount or using a mount containing electro-rheological fluid which has different stiffness properties according to the voltage applied across it.
In Fig. 4, a support 23 has multiple machines 25 mounted via respective mounts 24. The stiffness of each of these mounts 24 can be varied according to which machine is idle and which is operative, so that where machines are run at different times of day for different puφoses, a machine not in use provides vibration absoφtion for one which is.
Fig. 5 shows an example of a mechanical mount for the present invention, e.g. springs or other resilient couplings, such as rubber. One spring 27, which has a stiffness suitable for the frequency of operation of an operative machine 30, is connected between a support 29 and an idle machine 28, and another spring 26 is disconnected at one end, by hand or by an automatic switch. On the operative machine an isolation spring 31 is connected and another spring 32 is disconnected. If the operative machine 30 became idle and the idle machine 28 was brought into operation, then the connected springs 27,31 would be disconnected and the other springs 31 ,32 connected. Fig. 6 illustrates a mount whose stiffness is controlled using electro-rheological fluid. An example of an electro-rheological fluid is silica spheres in water and glycerol. The mount comprises a flexible housing 33, e.g. a rubber bladder, which contains the electro-rheological fluid 34. This fluid has the property that application of a potential to it causes a change in viscosity. This property can be used to alter the stiffness of the mount according to the function it is to perform. The potential can be made continuously variable by inserting a rheostat 35 in the circuit as shown in Fig. 6a so that the viscosity may be tuned to the stiffness required for a particular machine or a multiway switch 36 as shown in Fig. 6b can be connected to fixed predefined potentials. When a mount is to act as an isolator, a first potential is applied, but if subsequently the same mount was to act as an absorber, then a different potential is applied and the viscosity of the liquid changes. This type of switching is preferable to the use of different mechanical springs or resilient materials because there is no redundancy, so reducing weight and saving-space.

Claims

1. A vibration attenuation system, the system comprising at least one operative machine (17), one idle machine (18) and a support (21); wherein each machine (17,18) is mounted on the support (21) via respective operative and idle mounts (19,20); wherein the stiffness of each mount may be switched between an isolation mode and an absoφtion mode; and wherein the stiffness of the operative mount (19) is switched to isolation mode and the stiffness of the idle mount (20) is switched to absoφtion mode, such that vibration in the support (21) is minimised.
2. A system according to claim 1 , wherein each of the operative and idle mounts comprise a single mount, the stiffness of which is controllable.
3. A system according to any preceding claim, wherein each mount comprises controllable means for controlling the stiffness of the mount.
4. A system according to claim 3, wherein the controllable means comprises electro-rheological fluid.
5. A system according to claim 4, wherein the electro-rheological fluid comprises silica spheres in water and glycerol.
6. A system according to any preceding claim, wherein the stiffness of the idle mount may be switched to one of a plurality of stiffness values.
7. A system according to any of claims 1 to 6, wherein the stiffness of the idle mount (20) in absoφtion mode is tuned for the operating frequency of the respective operative machine.
8. A system according to any preceding claim, wherein the support (21) is rigid.
PCT/GB1997/002730 1996-10-15 1997-10-06 Vibration attenuation system WO1998016760A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU45659/97A AU4565997A (en) 1996-10-15 1997-10-06 Vibration attenuation system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9621498.6 1996-10-15
GBGB9621498.6A GB9621498D0 (en) 1996-10-15 1996-10-15 Vibration attenuation system

Publications (2)

Publication Number Publication Date
WO1998016760A2 true WO1998016760A2 (en) 1998-04-23
WO1998016760A3 WO1998016760A3 (en) 1998-05-22

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB1997/002730 WO1998016760A2 (en) 1996-10-15 1997-10-06 Vibration attenuation system

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AU (1) AU4565997A (en)
GB (1) GB9621498D0 (en)
WO (1) WO1998016760A2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998049460A3 (en) * 1997-04-26 1999-01-28 Bayer Ag Spring/mass vibratory force coupler
EP0926385A1 (en) * 1997-12-23 1999-06-30 Rover Group Limited A vibration absorbing system

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4930741A (en) * 1987-06-08 1990-06-05 Vibro Dynamics Corporation Power assisted equipment mounting system
EP0412853A2 (en) * 1989-08-11 1991-02-13 Bridgestone Corporation Active-type vibration control apparatus
EP0537927A1 (en) * 1991-10-15 1993-04-21 Lord Corporation Fluid mount with active vibration control
US5267633A (en) * 1991-02-15 1993-12-07 Bridgestone Corporation Electrorheological fluid-applied apparatus, electrorheological fluid-applied vibration controller, and electrorheological fluid-applied fixing apparatus
EP0676558A1 (en) * 1994-04-04 1995-10-11 Applied Power Inc. Stiff actuator active vibration isolation system
WO1995034769A1 (en) * 1994-06-16 1995-12-21 Lord Corporation Active mounts for aircraft engines
US5505871A (en) * 1993-11-23 1996-04-09 General Atomics Electrorheological elastomeric composite materials
US5547049A (en) * 1994-05-31 1996-08-20 Lord Corporation Magnetorheological fluid composite structures

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4930741A (en) * 1987-06-08 1990-06-05 Vibro Dynamics Corporation Power assisted equipment mounting system
EP0412853A2 (en) * 1989-08-11 1991-02-13 Bridgestone Corporation Active-type vibration control apparatus
US5267633A (en) * 1991-02-15 1993-12-07 Bridgestone Corporation Electrorheological fluid-applied apparatus, electrorheological fluid-applied vibration controller, and electrorheological fluid-applied fixing apparatus
EP0537927A1 (en) * 1991-10-15 1993-04-21 Lord Corporation Fluid mount with active vibration control
US5505871A (en) * 1993-11-23 1996-04-09 General Atomics Electrorheological elastomeric composite materials
EP0676558A1 (en) * 1994-04-04 1995-10-11 Applied Power Inc. Stiff actuator active vibration isolation system
US5547049A (en) * 1994-05-31 1996-08-20 Lord Corporation Magnetorheological fluid composite structures
WO1995034769A1 (en) * 1994-06-16 1995-12-21 Lord Corporation Active mounts for aircraft engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998049460A3 (en) * 1997-04-26 1999-01-28 Bayer Ag Spring/mass vibratory force coupler
EP0926385A1 (en) * 1997-12-23 1999-06-30 Rover Group Limited A vibration absorbing system

Also Published As

Publication number Publication date
AU4565997A (en) 1998-05-11
WO1998016760A3 (en) 1998-05-22
GB9621498D0 (en) 1996-12-04

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