CN105782253B - A kind of temperature change synchroballistic shafting - Google Patents

A kind of temperature change synchroballistic shafting Download PDF

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Publication number
CN105782253B
CN105782253B CN201410827094.XA CN201410827094A CN105782253B CN 105782253 B CN105782253 B CN 105782253B CN 201410827094 A CN201410827094 A CN 201410827094A CN 105782253 B CN105782253 B CN 105782253B
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China
Prior art keywords
axle sleeve
matrix
compensation
main shaft
compensation set
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Active
Application number
CN201410827094.XA
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Chinese (zh)
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CN105782253A (en
Inventor
陈耀忠
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Changzhou Wei Nengdajing Machine Co Ltd
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Changzhou Wei Nengdajing Machine Co Ltd
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Priority to CN201410827094.XA priority Critical patent/CN105782253B/en
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Publication of CN105782253B publication Critical patent/CN105782253B/en
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Abstract

Temperature change synchroballistic shafting disclosed by the invention: including main shaft, axle sleeve, compensation set, matrix, terminal pad and ring flange;Main shaft is equipped with axle sleeve, and sleeve outer surface is taper;Axle sleeve is equipped with compensation set, and compensation covers inner cavity for taper, and its taper corresponding matching consistent with sleeve outer surface taper;Compensation set outer circle and base mate, and the main shaft outer ring of axle sleeve, compensation set and matrix one end is provided with terminal pad, the other end outer ring of axle sleeve, compensation set and matrix is provided with ring flange;Main shaft, axle sleeve and ring flange are steel material, and compensation set, matrix and terminal pad are aluminum material.It is covered by the way that compensation is arranged in axle sleeve outer ring, the gradient of axle sleeve bus and axial line is determined according to after axial dimension, radial dimension actual measurement by different materials linear expansion coefficient.When temperature is widely varied, the running accuracy of shafting still keeps original high-precision.

Description

A kind of temperature change synchroballistic shafting
Technical field
The present invention relates to mechanical shafting fields, and in particular to a kind of temperature change synchroballistic shafting.
Background technique
The shafting of the prior art is that cylindrical or conical shaft and set form, and to slide or rolling matching mechanism, is usually made More be accurate machinery under room temperature or temperature constant state, it is desirable that temperature variation it is smaller, for example, at 20 DEG C ± 0.5 DEG C. Temperature is needed to be widely varied in range at -180 DEG C to 40 DEG C now, the geometric accuracy of mechanical structure varies less, such as axis The running accuracy of system.Since the material of mechanical structure component is different, the linear expansion coefficient of temperature change is different, mechanism member Relative position necessarily changes, it is now desired to the variation of position is overcome by temperature compensation mechanism, it is required several to ensure What position precision.
Summary of the invention
In order to solve the above technical problems, needing obtaining means we have proposed a kind of temperature change synchroballistic shafting When temperature is widely varied, the running accuracy of shafting still maintains original high-precision.
In order to achieve the above objectives, technical scheme is as follows:
A kind of temperature change synchroballistic shafting, including main shaft, axle sleeve, compensation set, matrix, terminal pad and ring flange;Institute Main shaft is stated equipped with axle sleeve, the sleeve outer surface is taper;The axle sleeve is equipped with compensation set, and compensation set inner cavity is cone Shape, and its taper is consistent with the sleeve outer surface taper in inner cavity corresponding matching;Described and compensation set cooperation is matrix, And it is provided with terminal pad outside the main shaft of the axle sleeve, compensation set and matrix one end, in the axle sleeve, compensation set and matrix Ring flange is provided with outside the other end;The main shaft, axle sleeve and ring flange are steel material, the compensation set, matrix and connection Disk is aluminum material.
Preferably, the compensation set is tightly fastened by the terminal pad in its end and the compensation set and matrix.
Preferably, the axle sleeve is tightly fastened with the ring flange, and the ring flange is tightly fastened with matrix.
Preferably, the main shaft is radial is equipped with rolling bearing with axial.
Through the above technical solutions, the present invention passes through in the more one layer of cone compensation sets of axle sleeve outer ring design, axle sleeve bus According to pressing after axial dimension, radial dimension actual measurement, different materials linear expansion coefficient is determining, and compensation covers and connects with the gradient of axial line It connects disk and matrix fastens, the taper outer circle and compensation set taper inner corresponding matching, axle sleeve and ring flange of axle sleeve fasten, ring flange It is fastened with matrix.Axis system is radial still can to take rolling bearing with axial, when temperature is widely varied, the rotation of shafting Turn precision and still maintains original high-precision.Be suitble to the common apparatus without isoperibol, high precision apparatus, vacuum environment equipment and Space technology equipment etc..
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this Some embodiments of invention for those of ordinary skill in the art without creative efforts, can be with It obtains other drawings based on these drawings.
Fig. 1 is a kind of cross-sectional view of temperature change synchroballistic shafting disclosed in the embodiment of the present invention.
Number and corresponding component title represented by letter in figure:
1. 2. terminal pad of axle sleeve, 3. matrix 4. compensation set
5. 6. main shaft of ring flange
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other Embodiment shall fall within the protection scope of the present invention.
The present invention provides a kind of temperature change synchroballistic shaftings, and which overcome the shadows of temperature change shaft precision It rings.
Below with reference to embodiment and specific embodiment, the present invention is described in further detail.
Embodiment
As shown in Figure 1, a kind of temperature change synchroballistic shafting, including main shaft 6, axle sleeve 1, compensation set 4, matrix 3, connection Disk 2 and ring flange 5;Axle sleeve 1 is arranged on the main shaft 6,1 outer surface of axle sleeve is taper;The axle sleeve 1 is equipped with compensation Set 4, it is taper that the compensation, which covers 4 inner cavities, and its taper and the 1 outer surface taper of axle sleeve are consistent in inner cavity corresponding matching; The compensation covers 4 outer circles and matrix 3 cooperates, and is provided in 6 outer ring of main shaft of the axle sleeve 1, compensation set 4 and 3 one end of matrix Terminal pad 2 is provided with ring flange 5 outside the other end of the axle sleeve 1, compensation set 4 and matrix 3;The main shaft 6,1 and of axle sleeve Ring flange 5 is steel material, and the compensation set 4, matrix 3 and terminal pad 2 are aluminum material.
Wherein, the compensation set 4 is tightly fastened by the terminal pad 2 in its end and described matrix 3;The axle sleeve 1 It is tightly fastened with the ring flange 5, the ring flange 5 is tightly fastened with matrix 3;The main shaft 6 is radial to be equipped with rolling with axial Dynamic bearing.
The cooperation of main shaft 6 and axle sleeve 1 is usually cylinder, now in the more one layer of cone compensation sets of 1 outer ring of axle sleeve design 4, the gradient of 1 outer circle bus of axle sleeve and axial line is according to pressing different materials linear expansion coefficient after axial dimension, radial dimension actual measurement It determines.Using the face A as benchmark face, the line of axial dimension expands variation delta L, and the line equal to small end head diameter dimension expands variable quantity The half of Δ D.
Need obtaining means when temperature is widely varied, geometric accuracy (i.e. geometric position) variation is small to keep high-precision Degree, such as the axis of rotation of shafting, axial line are equal to one of the variation delta D of small end head diametrically in axial variation delta L Half.
It can be seen that this temperature change synchroballistic shafting passes through in the more one layer of cone compensation sets of 1 outer ring of axle sleeve design 4, the gradient of 1 bus of axle sleeve and axial line is determined according to after axial dimension, radial dimension actual measurement by different materials linear expansion coefficient, Compensation set 4 is fastened with terminal pad 2 and matrix 3, taper (inclined-plane) outer circle and compensation 4 taper inner corresponding matchings of set of axle sleeve 1, axis Set 1 is fastened with ring flange 5, and ring flange 5 and matrix 3 fasten.Axis system is radial still can to take rolling bearing with axial, When temperature is widely varied, the running accuracy of shafting still maintains original high-precision.It is suitble to the common apparatus without isoperibol, High precision apparatus, vacuum environment equipment and space technology equipment etc..
Above-described is only a kind of temperature change synchroballistic shafting preferred embodiment of the invention, it is noted that For those of ordinary skill in the art, without departing from the concept of the premise of the invention, several changes can also be made Shape and improvement, these are all within the scope of protection of the present invention.

Claims (2)

1. a kind of temperature change synchroballistic shafting, which is characterized in that including main shaft, axle sleeve, compensation set, matrix, terminal pad and Ring flange;The main shaft is equipped with axle sleeve, and the sleeve outer surface is taper;The axle sleeve is equipped with compensation set, the compensation Set inner cavity is taper, and its taper is consistent with the sleeve outer surface taper in inner cavity corresponding matching;The compensation covers outer circle With base mate, and the axle sleeve, compensation set and the main shaft outer ring of matrix one end are provided with terminal pad, in the axle sleeve, benefit The other end outer ring for repaying set and matrix is provided with ring flange;The compensation set is by the terminal pad in its end and described matrix It is tightly fastened;The axle sleeve is tightly fastened with the ring flange, and the ring flange is tightly fastened with matrix;The compensation set and method It is not fixedly connected between blue side surface and has gap;The main shaft, axle sleeve and ring flange are steel material, the compensation Set, matrix and terminal pad are aluminum material;The gradient of the sleeve outer circle bus and axial line is according to axial dimension, radial dimension It is determined after actual measurement by different materials linear expansion coefficient.
2. a kind of temperature change synchroballistic shafting according to claim 1, which is characterized in that the main shaft radial direction and axis To being equipped with rolling bearing.
CN201410827094.XA 2014-12-26 2014-12-26 A kind of temperature change synchroballistic shafting Active CN105782253B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410827094.XA CN105782253B (en) 2014-12-26 2014-12-26 A kind of temperature change synchroballistic shafting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410827094.XA CN105782253B (en) 2014-12-26 2014-12-26 A kind of temperature change synchroballistic shafting

Publications (2)

Publication Number Publication Date
CN105782253A CN105782253A (en) 2016-07-20
CN105782253B true CN105782253B (en) 2019-08-02

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Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH582314A5 (en) * 1974-09-14 1976-11-30 Ringfeder Gmbh
FR2514443A1 (en) * 1981-10-09 1983-04-15 Dejoux Andre Wheel mounting for shaft - has muff with conical grip rings, and pressure screws to hold in place
JPS643330A (en) * 1987-02-24 1989-01-09 Tsubakimoto Chain Co Fastener for shaft and rotor
CN202251494U (en) * 2011-09-01 2012-05-30 上海格什特螺杆科技有限公司 Shaft hole matching self expansion connecting structure of permanent magnet synchronous motor rotor and screw compressor rotor
CN202612427U (en) * 2012-05-25 2012-12-19 四川德恩机械有限责任公司 Dual-ring taper fitting expansion sleeve connection structure
CN202811880U (en) * 2012-09-25 2013-03-20 李均 Shaft cohesion device for unmanned helicopter
CN203395042U (en) * 2013-07-10 2014-01-15 河北科技大学 Expansion connection device
CN203926469U (en) * 2014-05-05 2014-11-05 广州广船国际股份有限公司 A kind of Tensioning structure

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PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: A synchronous compensation shafting for temperature change

Effective date of registration: 20210825

Granted publication date: 20190802

Pledgee: China Construction Bank Corporation Changzhou Economic Development Zone sub branch

Pledgor: CHANGZHOU WEINENGDA PRECISION MACHINERY Co.,Ltd.

Registration number: Y2021980008270

PE01 Entry into force of the registration of the contract for pledge of patent right