CN106594169B - A kind of quasi- zero stiffness inertia actuator - Google Patents

A kind of quasi- zero stiffness inertia actuator Download PDF

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Publication number
CN106594169B
CN106594169B CN201611203638.0A CN201611203638A CN106594169B CN 106594169 B CN106594169 B CN 106594169B CN 201611203638 A CN201611203638 A CN 201611203638A CN 106594169 B CN106594169 B CN 106594169B
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movable part
support member
quasi
pedestal
driving
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CN106594169A (en
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杨铁军
辛和
章凯
张闻启
朱明刚
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Suzhou Donlim Intelligent Vibration And Noise Reduction Technology Co Ltd
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Suzhou Donlim Intelligent Vibration And Noise Reduction Technology Co Ltd
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    • 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
    • F16F15/03Suppression 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 magnetic or electromagnetic 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
    • F16F15/04Suppression 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 elastic means
    • F16F15/08Suppression 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 elastic means with rubber springs ; with springs made of rubber and metal
    • F16F15/085Use of both rubber and metal springs

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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)
  • Electromagnetism (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)

Abstract

The invention discloses a kind of quasi- zero stiffness inertia actuator, including shell, movable part and driving part, movable part is respectively equipped with the first support member and the second support member, first support member flexibly supports movable part along the vertical direction, movable part passes through in the first support member power transmission to pedestal, in driving part power transmission to pedestal, the at least two second support members elastic connection movable part and circumferential direction along movable part is uniformly arranged in the horizontal direction, first support member is that static compress state or dynamic compression stretch alternating state along the vertical direction, second support member is static compress state or dynamic compression state in the horizontal direction.First, support member forms the support component of one high static low dynamic rate, it can reduce by movable part and first, the intrinsic frequency for the component that two support members are constituted, perfect condition can be close to zero-frequency, in the case where not needing to increase volume and input current, increase the low frequency even ultralow frequency power output of actuator.

Description

A kind of quasi- zero stiffness inertia actuator
Technical field
The present invention relates to active damping fields, and in particular to a kind of non-linear support for increasing actuator low frequency power output is used to Property actuator.
Background technique
With the development of industry, requirement of the people to vibration control is higher and higher.Although and traditional passive vibration isolation technology It has the advantages of simple structure and easy realization, but also there is it to be difficult to the shortcomings that overcoming, after vibrating isolation system structure determination, subtract Effect of shaking determines, can not adapt to the variation of outer scrambling rate, while only when driving frequency is greater thanTimes vibrating isolation system it is intrinsic Damping effect could be played when frequency, but too low system frequency will lead to excessive the asking with unstability of quiet deformation when realizing Topic, causes low frequency vibration isolation problem.
Active vibration control technology can overcome the above problem, be developed rapidly.Actuator is the weight of active control Want part comprising driving part, movable part and resilient support, driving part use driving coil, and movable part is constituted One closed magnetic circuit system, on the one hand, the power output size of actuator meets left hand rule, power output size and magnetic field strength, electric current Intensity and conductor length are directly proportional, in order to meet use and installation requirement, the volume and current strength one of existing actuator As should not be too large, and volume again limits magnetic field strength and conductor length, and therefore, the power output of existing actuator is typically small; On the other hand, the power output frequency of actuator is related with resilient support, and power output frequency should be greater than movable part and resilient support structure At component intrinsic frequency, it is a kind of double-deck main passive that Authorization Notice No. is that the Chinese invention patent of CN104500647B discloses Electromechanical integrated form isolation mounting uses spring as resilient support, and since the rigidity of existing spring is low, intrinsic frequency is general It is unable to reach low frequency even ultralow frequency, therefore, the power output frequency of existing actuator is also unable to reach low frequency even ultralow frequency.It is comprehensive On, the low frequency power output of existing actuator is smaller, thus researches and develops a kind of increase actuator the low frequency even inertia of ultralow frequency power output Actuator is of great significance.
Summary of the invention
In order to solve the above technical problems, goal of the invention of the invention is to provide a kind of quasi- zero stiffness inertia actuator, It does not need in the case where increasing volume and input current, increases the low frequency even ultralow frequency power output of actuator.
For achieving the above object, the present invention provides a kind of technical solution below: quasi- zero stiffness inertia actuator, packet Shell, movable part and driving part are included, the shell includes pedestal, upper end cover and side wall, the movable part difference Equipped with the first support member and guiding parts, first support member flexibly supports the movable part, institute along the vertical direction It states guiding parts and is oriented to the movable part along the vertical direction, the movable part passes through the first support member power transmission to institute It states on pedestal, in the driving part power transmission to the pedestal, the movable part constitutes a closed magnetic circuit system, is produced with synchronous The raw active force for driving the driving part vibration and the reaction force for driving its own vibration, the movable part are additionally provided with the Two support members, at least two second support members movable part described in elastic connection and along the activity in the horizontal direction The circumferential direction of component is uniformly arranged, and first support member is that static compress state or dynamic compression stretch alternating along the vertical direction State, second support member are static compress state or dynamic compression state in the horizontal direction.
The intrinsic frequency for the component that the movable part, first support member and second support member are constituted Less than the vibration frequency of the movable part.
Further, first support member use board-like complex spring, the board-like complex spring include connecting plate, Connecting bushing and rubber slab, the connecting plate and the connecting bushing are metal material, and the connecting plate is equipped with middle through-hole, The connecting bushing is co-axially located in the middle through-hole, the rubber slab sulfidization molding in the connecting plate inner side edge and Between the outer wall of the connecting bushing, the connecting plate and the pedestal are relatively fixed, the connecting bushing and the movable part Part is relatively fixed and is vacantly arranged.
Further, the base portion upwardly extends to form annular convex platform, the annular convex platform and the connecting plate phase To fixation.
Further, second support member uses pillar complex spring, and the pillar complex spring connects including inside Connector, outside connector and rubber bar, the inside connector and the outside connector are metal material, and the inside connects Connector and outside connector coaxial arrangement, the rubber bar sulfidization molding are connected in the inside connector with the outside Between head, the inside connector and the movable part are relatively fixed, and the outside connector and the side wall are relatively fixed.
Further, the decrement of the rubber bar in the horizontal direction is adjustable, and the outside connector passes through the side wall Through-hole, the outside connector is also threaded with the adjusting nut for being located at the two sides of the through-hole.
Further, the movable part includes magnetic cylinder, the permanent magnet being arranged in the magnetic cylinder and is arranged in the magnetic The fixed plate of cylinder and the permanent magnet upper side position, the fixed plate is relatively fixed with the magnetic cylinder and the permanent magnet respectively, The driving part includes coil rack and driving coil, and the coil rack is arranged between the magnetic cylinder and the permanent magnet Air gap in and the pedestal that is sequentially connected, the driving coil be wrapped on the coil rack.
Further, the base portion upwardly extends to form cylindrical stent, and the cylindrical stent is as the coil bone Frame.
Further, the permanent magnet is upper, and lower position is also respectively provided with, lower yoke, it is described on, lower yoke point Not between the magnetic cylinder formed on, lower air gap, it is described on, the driving part is respectively set in lower air gap, described in two Driving part is cured as an entirety by epoxy resin set.
Further, the guiding parts includes guiding axis, and the lower end of the guiding axis is connect with the pedestal, described to lead It is connect to the upper end of axis with the upper end cover, is arranged on the guiding axis and linear bearing is installed, the inner ring of the linear bearing Relatively fixed with the guiding axis, the outer ring of the linear bearing and the movable part are relatively fixed, second support portion Part is connected between the side wall and the outer ring of the linear bearing.
Further, the space between the movable part and the upper end cover is slightly larger than the vibration row of the movable part Journey.
Due to the above technical solutions, the present invention has the following advantages over the prior art:
(1) work in the present invention is the first support member and Yan Shui that the present invention passes through that setting flexibly supports along the vertical direction Square to elastic connection the second support member, the first support and the second support form the support of one high static low dynamic rate Component, when movable part is static, the second support member is in horizontality and does not play a supportive role, and the first support member is negative Duty support movable part, at this moment the Static Correction of movable part is small, and when movable part movement, the second support member plays negative stiffness and makees With being equivalent to makes the dynamic rate of the first support become smaller, to realize movable part, the first support member and the second support The resilient support assemblies that component is constituted have the characteristics that high static low dynamic rate, can reduce the intrinsic frequency of movable component, Perfect condition can be close to zero-frequency, therefore, increase the low frequency even ultralow frequency output of actuator;
(2) the power output size f of the actuator in the present invention is synthesized by two power of Ampere force and rigidity power, i.e.,Wherein f=BIL is Ampere force, and k is rigidity, and x is displacement of the movable part about static center, W is Ampere force frequency, wnFor intrinsic frequency, it can be seen that when the frequency of driving force is much smaller than 1 relative to intrinsic frequency, rigidity The denominator of power can be approximated to be -1 therefore rigidity power is approximately equal to-f, and total power output is close to 0, but the frequency for working as driving force is greater than admittedly When having frequency, both rigidity power and Ampere force direction are identical, and total power output is equal to the sum of the two.Made not by reducing intrinsic frequency The range for increasing only power area in the same direction, also increases frequency ratio, increases the power output of low frequency range.And general linear support is when logical Quiet deformation excessive, bad stability can be made by crossing when reduction rigidity reduces intrinsic frequency, and pass through the first support and the second support shape At there is high static low dynamic non-linear support, not only there is high Static stiffness but also with low dynamic stiffness, thus In the case that guarantee system is stablized, reduce intrinsic frequency and be even up to zero intrinsic frequency, increases actuator low frequency power output.
Detailed description of the invention
Fig. 1 is the main view of quasi- zero stiffness inertia actuator disclosed by the invention;
Fig. 2 is the bottom view of quasi- zero stiffness inertia actuator disclosed by the invention;
Fig. 3 is the rear cross sectional view of Section A-A in Fig. 2;
Fig. 4 is the bottom view of section B-B in Fig. 3;
Fig. 5 is the main view of the first support member disclosed by the invention;
Fig. 6 is the top view of the first support member disclosed by the invention;
Fig. 7 is the initial power curve of actuator and the power curve after movable component intrinsic frequency reduction after improvement before improving Comparison diagram.
Wherein, 110, pedestal;111, connecting hole;120, upper end cover;130, side wall;131, first interface;132, it second connects Mouthful;211, magnetic cylinder;212, permanent magnet;213, upper yoke;214, lower yoke;215, fixed plate;220, rubber slab;221, connection lining Set;222, connecting plate;230, stay bolt;240, rubber bar;251, guiding axis;252, linear bearing;253, bolt;310, it drives Coil;320, coil rack.
Specific embodiment
With reference to the accompanying drawings and examples, specific embodiments of the present invention will be described in further detail.The following are with In illustrating a preferred embodiment of the invention, but it is not intended to limit the scope of the invention.
Referring to Fig. 1 to Fig. 6, as shown in legend therein:
A kind of quasi- zero stiffness inertia actuator, comprising:
Shell comprising pedestal 110, upper end cover 120 and side wall 130, pedestal 110 are equipped with and connect with controlled device Connecting hole 111, offer first interface 131 and second interface 132 respectively on side wall 130;
Movable component comprising movable part, the first support member, the second support member and guiding parts,
-- above-mentioned movable part includes magnetic cylinder 211, the permanent magnet being arranged in magnetic cylinder 211 212, is separately positioned on permanent magnet 212 upper, upper, lower yoke 213,214 and the fixed plate that 213 upper side position of magnetic cylinder 211 and upper yoke is set of lower position 215, fixation is worn by bolt between fixed plate 215 and magnetic cylinder 211;
-- above-mentioned first support member uses board-like complex spring, which includes connecting plate 222, connection lining Set 221 and rubber slab 220, connecting plate 222 and connecting bushing 221 are metal material, and connecting plate 222 is equipped with middle through-hole, even It connects bushing 221 to be co-axially located in middle through-hole, 220 sulfidization molding of rubber slab is in the inner side edge and connecting bushing of connecting plate 222 Between 221 outer wall, connecting plate 222 is connected to pedestal 110 and upwardly extends on the annular convex platform to be formed, fixed plate 215, upper yoke 213, permanent magnet 212, lower yoke 214 are worn by a stay bolt 230 and are connected together, and it is short to wear one in the unthreaded hole of connecting bushing 221 Bolt, the unthreaded hole which passes through above-mentioned connecting bushing 221 are threadedly coupled with stay bolt 230, and rubber slab 220 is along the vertical direction Movable part is flexibly supported, rubber slab 220 stretches alternating state along the vertical direction for static compress state or dynamic compression;
-- above-mentioned second support member uses at least two two compound bullets of pillar being circumferentially uniformly arranged along movable part Spring, the pillar complex spring include inside connector, outside connector and rubber bar 240, and inside connector is connected with outside Head is metal material, inside connector and the coaxial arrangement of outside connector, and 240 sulfidization molding of rubber bar is in inside connector and outside Between the connector of side, inside connector is threadedly coupled with movable part, and outside connector is threadedly coupled with side wall 130, rubber bar 240 elastic connection movable parts in the horizontal direction, rubber bar 240 are static compress state or dynamic compression shape in the horizontal direction State;
-- above-mentioned guiding parts includes guiding axis 251 and linear bearing 252, the lower end of guiding axis 251 by bolt 253 with Pedestal 110 connects, and the upper end of guiding axis 251 is connect by bolt with upper end cover 120, and linear bearing 252, which is arranged, is mounted on guiding On axis 251, the inner ring and guiding axis 251 of linear bearing 252 are relatively fixed, the outer ring of linear bearing 252 and magnetic cylinder 211 and/or Fixed plate 215 is relatively fixed, and the other end of rubber torsional spring 240 is threaded on the outer ring of linear bearing 252;
Driving part is separately positioned on two annulars that magnetic cylinder 211 is formed with upper yoke 213 and lower yoke 214 respectively In air gap, including driving coil 310 and coil rack 320, coil rack 320 are arranged in what magnetic cylinder 211 was formed with permanent magnet 212 In air gap and relatively fixed with pedestal 110, driving coil 310 is wrapped on coil rack 320, and two driving parts pass through epoxy Resin set is cured as an entirety.
Wherein, movable part constitutes a closed magnetic circuit system, with the synchronous active force for generating driving driving part vibration and The reaction force for driving its own to vibrate, the intrinsic frequency of above-mentioned movable component are less than the vibration frequency of movable part, movable part Space between part and upper end cover 120 is slightly larger than the vibratility adjustment of above-mentioned movable part.It is not required between movable part and upper end cover Resilient support is added again, saves the invalid distance between movable part and upper end cover, and the whole height of actuator can reduce 20% or so.
Referring to Fig. 7, to improve going out after the preceding initial power curve of actuator reduces with movable component intrinsic frequency after improvement Force curve comparison diagram, (because Figure of description is unable to chromatic colour, I is modified as dotted line red) actuator go out Power size f is synthesized by two power of Ampere force and rigidity power, i.e.,Wherein f=BIL is Ampere force, k For rigidity, x is displacement of the movable part about static center, and w is Ampere force frequency, wnFor intrinsic frequency, it can be seen that work as drive When the frequency of power is much smaller than 1 relative to intrinsic frequency, the denominator of rigidity power can be approximated to be -1 therefore rigidity power is approximately equal to-f, Total power output is close to 0, but when the frequency of driving force is greater than intrinsic frequency, and both rigidity power and Ampere force direction are identical, always Power output be equal to both sum.Diagram dotted line is that reduce intrinsic frequency be the curve after original 1/10th, can by figure To find out, makes the range for not only increasing power area in the same direction by reducing intrinsic frequency, also increase frequency ratio, increase low frequency The power output in area.And general linear support can make excessive, the bad stability of quiet deformation when reducing intrinsic frequency by reducing rigidity, And there is high static low dynamic non-linear support by what the first support and the second support were formed, not only there is high Static stiffness And there is low dynamic stiffness, to make intrinsic frequency reduce even up to zero intrinsic frequency in the case where guaranteeing that system is stablized Rate increases actuator low frequency power output.
In a kind of embodiment, integral structure that coil rack 320 and pedestal 110 are integrally formed.
In a kind of embodiment, the decrement of rubber bar 240 in the horizontal direction is adjustable, and outside connector passes through side wall 130 Through-hole, outside connector is also threaded with the adjusting nut for being located at the two sides of through-hole.
By adjusting the decrement of rubber bar 240, decrement adjustment makes horizontal rubber bar 240 be in compressive state to produce Raw negative stiffness, the decrement of rubber bar 240 is related with the stiffness ratio of horizontal rubber bar 240 and vertical rubber slab 220, decrement Value be to be obtained by theoretical calculation, rubber bar 240 must be horizontal and compresses and could generate negative stiffness, ability reduction activity group The intrinsic frequency of part makes rubber slab 220 and rubber bar 240 that high static rigidity and low static rigidity, the number of rubber bar 240 may be implemented There is no limit for amount, can be multiple, makes rubber slab 220 and rubber bar 240 that can play a supporting role, and moves back and forth in movable part When can also reach lower dynamic stiffness, reduce the intrinsic frequency of movable component, increase the output of actuator low frequency;Guidance set is one Kind kinematic constraint mechanism, is accurately positioned to movable part using linear bearing 252 and is limited unnecessary transverse movement, from And guarantees movable part and move reciprocatingly in the axial direction of guiding axis 251.
Actuator is installed to control mechanically by the connecting hole 111 on pedestal 110, using nut.The magnetic circuit of actuator Principle are as follows: permanent magnet 212 → upper 213 → air gap of yoke → 211 → air gap of magnetic cylinder → 214 → permanent magnet of lower yoke 212, thus Constitute a closed magnetic circuit.The driving coil 310 of actuator draws positive and negative anodes by first interface 131, and passes through second The extraction of interface 132 is connected to external power amplifier (not regarding out in figure), and power amplifier exports electric current to driving coil 310, when driving coil 310 In when being connected with alternating current, electromagnetic action generates electromagnetic force to driving coil 310, because driving coil 310 is fixed on stainless steel Coil rack 320, therefore electromagnetic force is transmitted to pedestal 110, while 310 alternation of driving coil by stainless steel wire ring framework 320 Cutting magnetic line makes movable part generate reciprocating motion, and reciprocating motion can make rubber generation restoring force be transmitted to pedestal 110, The resultant force of two power is power output.
The above are the descriptions to the embodiment of the present invention to keep this field special by the foregoing description of the disclosed embodiments Industry technical staff can be realized or using the present invention.Various modifications to these embodiments carry out those skilled in the art Saying will be apparent, and the general principles defined herein can be the case where not departing from the spirit or scope of the present invention Under, it realizes in other embodiments.Therefore, the present invention will not be limited to the embodiments shown herein, but to accord with Close the widest scope consistent with the principles and novel features disclosed herein.

Claims (9)

1. a kind of quasi- zero stiffness inertia actuator, including shell, movable part and driving part, the shell include pedestal, Upper end cover and side wall, the movable part are respectively equipped with the first support member and guiding parts, first support member edge Vertical direction flexibly supports the movable part, and the guiding parts is oriented to the movable part, the activity along the vertical direction Component is by the first support member power transmission to the pedestal, in the driving part power transmission to the pedestal, the work Dynamic component constitutes a closed magnetic circuit system, with the synchronous active force for generating the driving driving part vibration and drives its own vibration Dynamic reaction force, which is characterized in that the movable part is additionally provided with the second support member, at least two second support portions Part movable part described in elastic connection and is uniformly arranged, first support portion in the horizontal direction along the circumferential direction of the movable part Part is that static compress state or dynamic compression stretch alternating state along the vertical direction, and second support member is in the horizontal direction Static compress state or dynamic compression state, the movable part include magnetic cylinder, the permanent magnet being arranged in the magnetic cylinder and set Set the fixed plate in the magnetic cylinder and the permanent magnet upper side position, the fixed plate respectively with the magnetic cylinder and the permanent magnet Relatively fixed, the driving part includes coil rack and driving coil, and the coil rack setting is in the magnetic cylinder and described In air gap between permanent magnet, first support member uses board-like complex spring, and the board-like complex spring includes connection Plate, connecting bushing and rubber slab, the connecting plate and the connecting bushing are metal material, and the connecting plate is logical equipped with middle part Hole, the connecting bushing are co-axially located in the middle through-hole, and the rubber slab sulfidization molding is in the inside of the connecting plate Between side and the outer wall of the connecting bushing, the connecting plate and the pedestal are relatively fixed, the connecting bushing and the work Dynamic component is relatively fixed and is vacantly arranged.
2. quasi- zero stiffness inertia actuator according to claim 1, which is characterized in that the base portion upwardly extends shape Boss is circularized, the annular convex platform and the connecting plate are relatively fixed.
3. quasi- zero stiffness inertia actuator according to claim 1, which is characterized in that second support member uses column Formula complex spring, the pillar complex spring include inside connector, outside connector and rubber bar, the inside connector It is metal material, the inside connector and outside connector coaxial arrangement, the rubber bar with the outside connector For sulfidization molding between the inside connector and the outside connector, the inside connector is opposite with the movable part Fixed, the outside connector and the side wall are relatively fixed.
4. quasi- zero stiffness inertia actuator according to claim 3, which is characterized in that the rubber bar is in the horizontal direction Decrement is adjustable, and the outside connector passes through the through-hole of the side wall, and the outside connector is also threaded with position respectively Adjusting nut in the two sides of the through-hole.
5. quasi- zero stiffness inertia actuator according to claim 4, which is characterized in that the coil rack is fixedly connected with institute Pedestal is stated, the driving coil is wrapped on the coil rack.
6. quasi- zero stiffness inertia actuator according to claim 5, which is characterized in that the base portion upwardly extends shape At cylindrical stent, the cylindrical stent is as the coil rack.
7. quasi- zero stiffness inertia actuator according to claim 5, which is characterized in that upper, the downside position of the permanent magnet Set and be also respectively provided with, lower yoke, it is described on, lower yoke respectively between the magnetic cylinder formed on, lower air gap is described On, the driving part is respectively set in lower air gap, two driving parts are cured as an entirety by epoxy resin set.
8. quasi- zero stiffness inertia actuator according to claim 1, which is characterized in that the guiding parts includes guiding Axis, the lower end of the guiding axis are connect with the pedestal, and the upper end of the guiding axis is connect with the upper end cover, the guiding axis On be arranged linear bearing be installed, the inner ring of the linear bearing and the guiding axis are relatively fixed, the linear bearing it is outer Enclose it is relatively fixed with the movable part, second support member be connected to the side wall and the linear bearing outer ring it Between.
9. quasi- zero stiffness inertia actuator according to claim 1, which is characterized in that the movable part and the upper end Space between lid is slightly larger than the vibratility adjustment of the movable part.
CN201611203638.0A 2016-12-23 2016-12-23 A kind of quasi- zero stiffness inertia actuator Active CN106594169B (en)

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Families Citing this family (4)

* Cited by examiner, † Cited by third party
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CN107654552B (en) * 2017-08-31 2019-07-16 哈尔滨工程大学 A kind of quasi-zero stiffness vibration isolators for carrying out adjusting neutrality using piezoelectric patches
CN109681572B (en) * 2018-11-30 2020-06-30 上海交通大学 Active and passive vibration isolator and power equipment
CN109667868B (en) * 2018-12-25 2020-04-28 西安交通大学 Resonant line spectrum inertial actuator, active control system and control method
CN112413044A (en) * 2020-11-18 2021-02-26 中国核动力研究设计院 Ultralow frequency inertial type actuator

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000049309A2 (en) * 1999-02-22 2000-08-24 Cooper Tire & Rubber Company Apparatus for vibrations attenuation using electronic and electromagnetic actuation
US6305675B1 (en) * 1999-08-27 2001-10-23 Tokai Rubber Industries, Ltd. Oscillating force generator and vibration damper using the generator
CN202451695U (en) * 2011-11-07 2012-09-26 哈尔滨工程大学 Seal structure coil external semi-active bump leveler
CN103791013A (en) * 2014-02-19 2014-05-14 哈尔滨工程大学 Integrated type inertia electromagnetic actuator
CN104033535A (en) * 2014-06-05 2014-09-10 哈尔滨工程大学 Three-dimensional vibration isolation device applicable to low-frequency vibration
CN104500647A (en) * 2015-01-04 2015-04-08 哈尔滨工程大学 Double-layer active-passive electromechanical integrated type vibration isolation device
CN104989776A (en) * 2015-07-08 2015-10-21 中国船舶重工集团公司第七一九研究所 Electromagnetic type active and passive composite vibration isolator
CN206468742U (en) * 2016-12-23 2017-09-05 苏州东菱智能减振降噪技术有限公司 A kind of quasi- zero stiffness inertia actuator

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016065584A (en) * 2014-09-24 2016-04-28 株式会社ケーヒン Active type vibration-proof device

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000049309A2 (en) * 1999-02-22 2000-08-24 Cooper Tire & Rubber Company Apparatus for vibrations attenuation using electronic and electromagnetic actuation
US6305675B1 (en) * 1999-08-27 2001-10-23 Tokai Rubber Industries, Ltd. Oscillating force generator and vibration damper using the generator
CN202451695U (en) * 2011-11-07 2012-09-26 哈尔滨工程大学 Seal structure coil external semi-active bump leveler
CN103791013A (en) * 2014-02-19 2014-05-14 哈尔滨工程大学 Integrated type inertia electromagnetic actuator
CN104033535A (en) * 2014-06-05 2014-09-10 哈尔滨工程大学 Three-dimensional vibration isolation device applicable to low-frequency vibration
CN104500647A (en) * 2015-01-04 2015-04-08 哈尔滨工程大学 Double-layer active-passive electromechanical integrated type vibration isolation device
CN104989776A (en) * 2015-07-08 2015-10-21 中国船舶重工集团公司第七一九研究所 Electromagnetic type active and passive composite vibration isolator
CN206468742U (en) * 2016-12-23 2017-09-05 苏州东菱智能减振降噪技术有限公司 A kind of quasi- zero stiffness inertia actuator

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