CN106678239B - A kind of composite construction vibration isolator that rubber is combined with wire mesh - Google Patents

A kind of composite construction vibration isolator that rubber is combined with wire mesh Download PDF

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Publication number
CN106678239B
CN106678239B CN201510762876.4A CN201510762876A CN106678239B CN 106678239 B CN106678239 B CN 106678239B CN 201510762876 A CN201510762876 A CN 201510762876A CN 106678239 B CN106678239 B CN 106678239B
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vibration isolator
rubber
spring
core
rubber block
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CN106678239A (en
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董万元
师永宁
张昕
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AVIC Aircraft Strength Research Institute
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AVIC Aircraft Strength Research Institute
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Abstract

The present invention relates to a kind of vibration isolator, in particular to the composite construction vibration isolator that is combined with wire mesh of a kind of electronic equipment rubber.Spring (8) is located on the bottom plate (9) of shell (1), the inside of spring (8) is filled with wire gauze pad (7), it is placed on spring (8) transition core (2), the outside of spring (8) is filled with wire gauze pad (7) below transition core (2);Cavity is had in transition core (2), rubber block (4) are installed in cavity, it is fixed with installation core (5) on rubber block (4), is filled with wire gauze pad (7) between shell (1) and transition core (2).The vibration isolator improves the efficiency of vibration damping, and structure is simple.

Description

A kind of composite construction vibration isolator that rubber is combined with wire mesh
Technical field
The present invention relates to a kind of vibration isolator, in particular to the composite junction that is combined with wire mesh of a kind of electronic equipment rubber Structure vibration isolator.
Background technique
In order to improve the measurement accuracy, control precision and safety and reliability of optoelectronic device, airplane equipment is for ring The limitation of border vibration requires to be increasingly stringenter;And with the raising of the speeds of service such as aircraft, vehicle so that structural environment vibrates Magnitude it is increasing, driving frequency to low-frequency range extend.By theory of vibration isolation it is found that if the rigidity of vibration isolator is lower, vibration isolation effect Rate is higher, and low frequency vibration isolation effect is also better.Therefore, to the vibration control precision of raising optoelectronic device, it is necessary to reduce airborne light The frequency of electric equipment vibration damping installation.
Existing wire mesh vibration isolator and rubber shock absorber all have the characteristic of three-dimensional vibration isolation, how free can be realized equipment Spend the requirement of vibration control.But they are generally used just for a certain equipment development, and intrinsic frequency is difficult to accomplish 10Hz or less.Therefore, for certain aircraft requirements lower than 10Hz low frequency vibration isolation below use current vibration isolator incapability for Power.It would therefore be highly desirable to design novel low frequency vibration isolation device for airborne opto-electronic device low frequency vibration isolation application field.
Summary of the invention
Present invention solves the technical problem that: it provides a kind of suitable for various electronic, the high vibration isolator of vibration isolation efficiency.
Technical solution of the present invention: the vibration isolator includes shell 1, transition core 2, rubber block 4, installation core 5, wire Gauze pad 7, spring 8 and bottom plate 9, spring 8 are located on the bottom plate 9 of shell 1, and the inside of spring 8 is filled with wire gauze pad 7, spring 8 On be placed with transition core 2, the outside of 2 lower section spring 8 of transition core is filled with wire gauze pad 7;
Cavity is had in transition core 2, rubber block 4 is installed in cavity, installation core 5 is fixed on rubber block 4, in shell 1 Wire gauze pad 7 is filled between transition core 2.
As a kind of improvement of the technical program, core 5 is installed and is fixed as one by vulcanization with rubber block 4.The program is solid Determine that effect is good, falling off for installation core can be prevented.
As a kind of improvement of the technical program, concave surface is provided on the outer surface of rubber block 4.This is designed as rubber block 4 Deformation provides space, improves the effect of vibration isolation.
Beneficial effects of the present invention: the vibration isolator structure is simple, convenient for assembly.By transition core by rubber block and wire It is isolated into upper layer and lower layer between net and spring, the second level Vibration Absorbing System Design for realizing vibration isolator can be facilitated.The vibration isolator has lower Rigidity, the vibration condition required suitable for low frequency vibration isolation.And vibration isolator still has the ability of three-dimensional vibration isolation, is applicable to three-dimensional The equipment that vibration isolation requires.Rubber bodies have it is compact-sized, the changeable advantage of shape can easily change the knot of rubber core Structure easily designs more multi-form vibration isolator.This composite construction vibration isolator has the frictional damping between wire mesh simultaneously, also The hysteretic damping for having rubber macromolecular chain to generate in deformation process increases the damping characteristic of vibration isolator.
Detailed description of the invention
Fig. 1 are as follows: structural schematic diagram of the invention;
Fig. 2 are as follows: cross-sectional view of the invention;
Fig. 3 are as follows: transition cored structure schematic diagram;
In figure, 1) shell, 2) transition core, 3) baffle, 4) rubber block, 5) install core, 6) threaded cap, 7) wire gauze pad, 8) spring, 9) bottom plate.
Specific embodiment
The technical program is described in further detail with reference to the accompanying drawing.
The vibration isolator includes shell 1, transition core 2, baffle 3, rubber block 4, installation core 5, threaded cap 6, wire mesh Pad 7, spring 8 and bottom plate 9, spring 8 are located on the bottom plate 9 of shell 1, and the inside of spring 8 is filled with wire gauze pad 7, on spring 8 It is placed with transition core 2, the outside of 2 lower section spring 8 of transition core is filled with wire gauze pad 7;
Cavity is had in transition core 2, rubber block 4 is installed, the upper end of cavity has internal screw thread, with threaded cap 6 in cavity External screw thread cooperate for fixing rubber block 4.It is fixed with installation core 5 on rubber block 4, is filled between shell 1 and transition core 2 Wire gauze pad 7 designs baffle 3, has the function of sealing metal mesh pad 7 between wire gauze pad 7 and shell 1.Rubber block 4 Outer surface on be provided with concave surface, which, which is equivalent to, provides the scope of freedom for rubber block 4, and the deformation for rubber block 4 provides sky Between, increase the effect of vibration isolation.
1 enclosed inside of shell 4 three kinds of wire gauze pad 7, spring 8 and rubber block elastomers, can effectively realize vibration Dynamic isolation.Rubber block 4 and wire gauze pad 7 and spring 8 are separated into upper layer and lower layer by transition core 2, constitute the knot of two grad vibration isolation Structure.According to spring tandem principle, this structure can reduce the rigidity of vibration isolator, to reduce the intrinsic frequency of vibration isolator.It adopts Rubber block 4 is vulcanized with rubber curing techniques and constitutes rubber core on installation core 5, what which can be convenient is installed to transition core In 2, second level vibration insulation structure is formed.The shape flexible design of rubber and have the advantages that small in size, can be designed to a variety of Shape.

Claims (3)

1. the composite construction vibration isolator that a kind of rubber is combined with wire mesh, it is characterized in that: the vibration isolator includes shell (1), transition core (2), rubber block (4), installation core (5), wire gauze pad, spring (8) and bottom plate (9), spring (8) are located at shell (1) on bottom plate (9), the inside of spring (8) is filled with wire gauze pad, is placed with transition core (2), transition core on spring (8) (2) outside of lower section spring (8) is filled with wire gauze pad;
Cavity is had in transition core (2), is equipped with rubber block (4) in cavity, installation core (5) is fixed on rubber block (4), outside Wire gauze pad is filled between shell (1) and transition core (2).
2. the composite construction vibration isolator that a kind of rubber according to claim 1 is combined with wire mesh, it is characterized in that: installation Core (5) is fixed as one by vulcanization with rubber block (4).
3. the composite construction vibration isolator that a kind of rubber according to claim 1 is combined with wire mesh, it is characterized in that: rubber Concave surface is provided on the outer surface of block (4).
CN201510762876.4A 2015-11-10 2015-11-10 A kind of composite construction vibration isolator that rubber is combined with wire mesh Active CN106678239B (en)

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CN201510762876.4A CN106678239B (en) 2015-11-10 2015-11-10 A kind of composite construction vibration isolator that rubber is combined with wire mesh

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CN106678239B true CN106678239B (en) 2019-02-15

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Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108105305B (en) * 2017-12-13 2019-11-29 中国飞机强度研究所 A kind of vibration isolator
CN109281971B (en) * 2018-10-24 2019-12-06 华中科技大学 high-performance shock absorber
CN109737165A (en) * 2019-01-03 2019-05-10 兰州空间技术物理研究所 Rigidity vibration isolators and the vibrating isolation systems such as a kind of three axis of all-metal
CN109882534B (en) * 2019-03-28 2020-10-09 中国飞机强度研究所 Vibration isolator

Citations (5)

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Publication number Priority date Publication date Assignee Title
CN201739411U (en) * 2009-12-23 2011-02-09 中国飞机强度研究所 Bidirectional independent rigidity wire mesh vibration isolator
CN102518727A (en) * 2011-12-20 2012-06-27 中国飞机强度研究所 Totally-closed rigidity adjustable type vibration isolator
CN202674137U (en) * 2012-06-27 2013-01-16 上海三一重机有限公司 Damper and excavator comprising damper
CN204127183U (en) * 2014-06-24 2015-01-28 中国飞机强度研究所 A kind of wire gaze three-way vibration isolating device of variable frequency
CN204213235U (en) * 2014-11-04 2015-03-18 无锡市华东减震器有限公司 The rubber of rubber absorbers and the linkage structure of metal

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7044455B2 (en) * 2001-04-27 2006-05-16 Tokai Rubber Industries, Ltd. Fluid-filled vibration damping device

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201739411U (en) * 2009-12-23 2011-02-09 中国飞机强度研究所 Bidirectional independent rigidity wire mesh vibration isolator
CN102518727A (en) * 2011-12-20 2012-06-27 中国飞机强度研究所 Totally-closed rigidity adjustable type vibration isolator
CN202674137U (en) * 2012-06-27 2013-01-16 上海三一重机有限公司 Damper and excavator comprising damper
CN204127183U (en) * 2014-06-24 2015-01-28 中国飞机强度研究所 A kind of wire gaze three-way vibration isolating device of variable frequency
CN204213235U (en) * 2014-11-04 2015-03-18 无锡市华东减震器有限公司 The rubber of rubber absorbers and the linkage structure of metal

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