CN104279994B - One kind shield solar or lunar halo framework cubing - Google Patents
One kind shield solar or lunar halo framework cubing Download PDFInfo
- Publication number
- CN104279994B CN104279994B CN201410522130.1A CN201410522130A CN104279994B CN 104279994 B CN104279994 B CN 104279994B CN 201410522130 A CN201410522130 A CN 201410522130A CN 104279994 B CN104279994 B CN 104279994B
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- Prior art keywords
- position limiting
- limiting slide
- slide block
- block
- cubing
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B5/00—Measuring arrangements characterised by the use of mechanical techniques
- G01B5/0025—Measuring of vehicle parts
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- A Measuring Device Byusing Mechanical Method (AREA)
Abstract
Solar or lunar halo framework cubing is protected the invention discloses one kind, including cubing framework, two the first limit assemblies and two the second limit assemblies are respectively arranged with two relative support bodys of the cubing framework, first limit assembly includes first and fixes sliding block, first position limiting slide block and the second position limiting slide block, first position limiting slide block is vertical with the second position limiting slide block, first position limiting slide block and the second position limiting slide block both pass through described first and fix sliding block, second position limiting slide block passes through first position limiting slide block, second limit assembly includes fixed spacing pin block, 3rd position limiting slide block and the 4th position limiting slide block, 3rd position limiting slide block is vertical with the 4th position limiting slide block, 3rd position limiting slide block and the 4th position limiting slide block both pass through the spacing pin block of the fixation, 3rd position limiting slide block passes through the 4th position limiting slide block, the spacing bearing pin of protrusion is vertically installed with the middle part of fixed spacing pin block.The shield solar or lunar halo framework cubing of the present invention can rapidly and accurately detect that simple in construction, detection efficiency is high to the critical size for protecting solar or lunar halo product.
Description
Technical field
The present invention relates to a kind of detection instrument for the shield solar or lunar halo product critical size for being used to detect on automobile.
Background technology
With the development of automobile industry, the making of automobile interiors part shield solar or lunar halo is also more and more, and detection requires also to get over
Come higher.More often, it is desirable to be able to which whether the critical size for being quickly detected shield solar or lunar halo product is qualified.At present, it is based on
Solar or lunar halo product is protected than larger, the more complicated situation of structure, the measurement of shield solar or lunar halo critical size, which is depended on, uses three coordinate methods, examines
The survey time is long, is difficult for volume production Product checking, detection efficiency is low.
The content of the invention
The present invention solves the technical problem of a kind of shield solar or lunar halo framework cubing is provided, the cubing can be rapidly and accurately
The critical size for protecting solar or lunar halo product is detected, simple in construction, detection efficiency is high.
In order to solve the above technical problems, one aspect of the present invention is：A kind of shield solar or lunar halo framework cubing is provided,
Two the first limit assemblies and two are respectively arranged with cubing framework including rectangle, two relative support bodys of the cubing framework
Individual second limit assembly, first limit assembly includes first and fixes sliding block, the first position limiting slide block and the second position limiting slide block, institute
State the first fixation sliding block to be fixed on the support body, first position limiting slide block is vertical with the second position limiting slide block, first limit
Position sliding block and the second position limiting slide block both pass through described first and fix sliding block, and second position limiting slide block passes through the described first spacing cunning
Block, second limit assembly includes fixed spacing pin block, the 3rd position limiting slide block and the 4th position limiting slide block, the fixed spacer pin
Block is fixed on the support body, and the 3rd position limiting slide block is vertical with the 4th position limiting slide block, the 3rd position limiting slide block and the 4th
Position limiting slide block both passes through the spacing pin block of the fixation, and the 3rd position limiting slide block passes through the 4th position limiting slide block, and the fixation is spacing
The spacing bearing pin of protrusion is vertically installed with the middle part of pin block.
In a preferred embodiment of the present invention, it is provided with limited impression on the inside of the first fixation sliding block top.
In a preferred embodiment of the present invention, the limited impression is cone tank.
In a preferred embodiment of the present invention, described first sliding block, the first position limiting slide block and the second position limiting slide block are fixed
It is slidably connected each other.
In a preferred embodiment of the present invention, the spacing pin block of the fixation, the 3rd position limiting slide block and the 4th position limiting slide block
It is slidably connected each other.
The beneficial effects of the invention are as follows：The cubing of the present invention rapidly and accurately can be entered to the critical size for protecting solar or lunar halo product
Row detection, simple in construction, detection efficiency is high, it is not necessary to is detected, is adapted for large batch of by three complicated coordinate methods
Detection.
Brief description of the drawings
Technical scheme in order to illustrate the embodiments of the present invention more clearly, makes required in being described below to embodiment
Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the present invention, for
For those of ordinary skill in the art, on the premise of not paying creative work, it can also obtain other according to these accompanying drawings
Accompanying drawing, wherein：
Fig. 1 is the dimensional structure diagram of the shield solar or lunar halo framework cubing of the present invention；
Fig. 2 is the structural front view with the shield solar or lunar halo framework cubing of the present invention；
Fig. 3 is the shield solar or lunar halo framework cubing and the structure top view of test of the present invention；
Fig. 4 is the schematic diagram of the shield solar or lunar halo framework cubing and shield solar or lunar halo assembling product state to be checked of the present invention.
The mark of each part is as follows in accompanying drawing：100th, cubing framework, the 200, first limit assembly, 300, second spacing group
Part, 400, shield solar or lunar halo, 1, limited impression, 2, spacing bearing pin, 3, first fixes sliding block, the 4, first position limiting slide block, and 5, second is spacing
Sliding block, the 6, the 3rd position limiting slide block, the 7, the 4th position limiting slide block, 8, fixed spacing pin block, 9, spacing block set, 10, positive stop lug boss, 11,
Support body.
Embodiment
The technical scheme in the embodiment of the present invention will be clearly and completely described below, it is clear that described implementation
Example is only a part of embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, this area is common
All other embodiment that technical staff is obtained under the premise of creative work is not made, belongs to the model that the present invention is protected
Enclose.
Fig. 1 to Fig. 4 is referred to, the embodiment of the present invention includes：
One kind shield solar or lunar halo framework cubing, includes the cubing framework 100 of rectangle, two relative framves of the cubing framework 100
Two the first limit assemblies 200 and two the second limit assemblies 300, first limit assembly 200 are respectively arranged with body 11
Sliding block 3, the first position limiting slide block 4 and the second position limiting slide block 5 are fixed including first, the first fixation sliding block 3 is fixed on the frame
On body 11, first position limiting slide block 4 is vertical with the second position limiting slide block 5, the position limiting slide block 5 of the first position limiting slide block 4 and second
Both pass through described first and fix sliding block 3, second position limiting slide block 5 passes through first position limiting slide block 4.
Second limit assembly 300 includes fixed spacing pin block 8, the 3rd position limiting slide block 6 and the 4th position limiting slide block 7, institute
State fixed spacing pin block 8 to be fixed on the support body 11, the 3rd position limiting slide block 6 is vertical with the 4th position limiting slide block 7, described the
Three position limiting slide blocks 6 and the 4th position limiting slide block 7 both pass through the spacing pin block 8 of the fixation, and the 3rd position limiting slide block 6 is limited through the 4th
Position sliding block 7, the middle part of the spacing pin block 8 of fixation is vertically installed with the spacing bearing pin 2 of protrusion.
Limited impression 1 is provided with the inside of first fixation sliding block 3 top.The limited impression 1 is preferably cone tank,
The limited impression 1 matches with the spacing block set 9 set on shield solar or lunar halo 400 to be detected.
The first fixation sliding block 3, the first position limiting slide block 4 and the second position limiting slide block 5 are slidably connected each other.
The spacing pin block 8 of fixation, the 3rd position limiting slide block 6 and the 4th position limiting slide block 7 are slidably connected each other.
Shield solar or lunar halo 400 is provided with positive stop lug boss 10, the center of positive stop lug boss 10 with the fixed spacing position corresponding section of pin block 8
Hole is provided with, the hole matches with spacing bearing pin 2.The spacing block set 9 of two tapers is respectively put into cubing by shield solar or lunar halo 400 when detecting
In upper corresponding limited impression 1, on the borehole jack of the center of positive stop lug boss 10 to spacing bearing pin 2, shield solar or lunar halo 400 is realized substantially and is existed
Fixation in cubing.
Sliding block 3, the first position limiting slide block 4 and the second position limiting slide block 5 a certain amount of cunning each other are fixed by measurement first
Dynamic and fixed spacing pin block 8, the 3rd position limiting slide block 6 and a certain amount of slip, Ke Yizhi each other of the 4th position limiting slide block 7
Road protect solar or lunar halo 400 in X/Y directions be vertical or horizontal change in size whether in the margin of tolerance of setting, so as to judge to protect wind
Whether the size of circle 400 is qualified.
Embodiments of the invention are the foregoing is only, are not intended to limit the scope of the invention, it is every to utilize this hair
Equivalent structure or equivalent flow conversion that bright description is made, or directly or indirectly it is used in other related technology necks
Domain, is included within the scope of the present invention.
Claims (1)
1. one kind shield solar or lunar halo framework cubing, it is characterised in that the cubing framework including rectangle, the two of the cubing framework are relative
Two the first limit assemblies and two the second limit assemblies are respectively arranged with support body, first limit assembly includes first and consolidated
Fixed slider, the first position limiting slide block and the second position limiting slide block, the first fixation sliding block are fixed on the support body, first limit
Position sliding block is vertical with the second position limiting slide block, and first position limiting slide block and the second position limiting slide block both pass through described first and fix cunning
Block, second position limiting slide block passes through first position limiting slide block, and second limit assembly includes fixed spacing pin block, the 3rd
Position limiting slide block and the 4th position limiting slide block, the spacing pin block of fixation are fixed on the support body, the 3rd position limiting slide block and
Four position limiting slide blocks are vertical, and the 3rd position limiting slide block and the 4th position limiting slide block both pass through the spacing pin block of the fixation, the described 3rd
Position limiting slide block passes through the spacing bearing pin that protrusion is vertically installed with the middle part of the 4th position limiting slide block, the spacing pin block of fixation, described
It is provided with limited impression on the inside of first fixation sliding block top, the limited impression is cone tank, described first fixes sliding block, the
It is slidably connected between one position limiting slide block and the second position limiting slide block, the spacing pin block of fixation, the 3rd position limiting slide block and the 4th
It is slidably connected between position limiting slide block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410522130.1A CN104279994B (en) | 2014-10-08 | 2014-10-08 | One kind shield solar or lunar halo framework cubing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410522130.1A CN104279994B (en) | 2014-10-08 | 2014-10-08 | One kind shield solar or lunar halo framework cubing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104279994A CN104279994A (en) | 2015-01-14 |
| CN104279994B true CN104279994B (en) | 2017-09-01 |
Family
ID=52255122
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410522130.1A Active CN104279994B (en) | 2014-10-08 | 2014-10-08 | One kind shield solar or lunar halo framework cubing |
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| Country | Link |
|---|---|
| CN (1) | CN104279994B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107527562B (en) * | 2017-10-24 | 2023-09-19 | 山西高科华杰光电科技有限公司 | LED display screen function jig structure |
| CN108151615B (en) * | 2017-12-29 | 2023-06-23 | 江西鑫田车业有限公司 | Distance inspection tool and distance inspection method for wind ring and bracket of radiator |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4027321A1 (en) * | 1990-08-29 | 1992-03-05 | Wenzel Praezision Gmbh | Cartesian coordinate measuring instrument with adjustable bearing - sufficiently stable to counteract torques exerted by stator according to transverse arm protrusion |
| CN201622059U (en) * | 2010-03-26 | 2010-11-03 | 江西杭萧钢构有限公司 | Size detector of cross column end |
| CN102441856A (en) * | 2010-10-09 | 2012-05-09 | 昆山洺九机电有限公司 | Conical slide block positioning device |
| CN102506791A (en) * | 2011-10-20 | 2012-06-20 | 北京航空航天大学 | In-situ test positioning controllable mechanical loading and fixing device |
| CN202547955U (en) * | 2011-12-28 | 2012-11-21 | 上海市计量测试技术研究院 | Automobile frame assembled type calibrating device of four-wheel position finder |
| CN204214421U (en) * | 2014-10-08 | 2015-03-18 | 沙洲职业工学院 | One protects solar or lunar halo framework cubing |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59160023A (en) * | 1983-03-01 | 1984-09-10 | Nippon Denso Co Ltd | Blower |
-
2014
- 2014-10-08 CN CN201410522130.1A patent/CN104279994B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4027321A1 (en) * | 1990-08-29 | 1992-03-05 | Wenzel Praezision Gmbh | Cartesian coordinate measuring instrument with adjustable bearing - sufficiently stable to counteract torques exerted by stator according to transverse arm protrusion |
| CN201622059U (en) * | 2010-03-26 | 2010-11-03 | 江西杭萧钢构有限公司 | Size detector of cross column end |
| CN102441856A (en) * | 2010-10-09 | 2012-05-09 | 昆山洺九机电有限公司 | Conical slide block positioning device |
| CN102506791A (en) * | 2011-10-20 | 2012-06-20 | 北京航空航天大学 | In-situ test positioning controllable mechanical loading and fixing device |
| CN202547955U (en) * | 2011-12-28 | 2012-11-21 | 上海市计量测试技术研究院 | Automobile frame assembled type calibrating device of four-wheel position finder |
| CN204214421U (en) * | 2014-10-08 | 2015-03-18 | 沙洲职业工学院 | One protects solar or lunar halo framework cubing |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104279994A (en) | 2015-01-14 |
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| CB03 | Change of inventor or designer information |
Inventor after: Xu Xianghong Inventor before: Xu Xianghong Inventor before: Chen Li Inventor before: Jin Jie Inventor before: Tian Bo Inventor before: Qian Yuanping Inventor before: Zhang Junfeng Inventor before: Wang Yanhui |
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| GR01 | Patent grant |