CN206966361U - Aviation part deformation straightening device - Google Patents
Aviation part deformation straightening device Download PDFInfo
- Publication number
- CN206966361U CN206966361U CN201720752369.7U CN201720752369U CN206966361U CN 206966361 U CN206966361 U CN 206966361U CN 201720752369 U CN201720752369 U CN 201720752369U CN 206966361 U CN206966361 U CN 206966361U
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- CN
- China
- Prior art keywords
- aviation part
- bottom plate
- straightening device
- part deformation
- hydraulic jack
- Prior art date
- Legal status (The legal status 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 status listed.)
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Abstract
The utility model discloses a kind of aviation part deformation straightening device, it is related to aviation part manufacture field, the aviation part deformation straightening device includes bottom plate, hanging beam and two support columns, two support column one end are symmetrically connected to hanging beam both ends, the other end is connected with bottom plate, two isometry blocks are also symmetrically arranged with bottom plate, two isometry blocks are between two support columns, limited block is additionally provided with bottom plate, limited block is between two isometry blocks, spacing tile height is less than two isometry blocks, briquetting is provided with above two isometry blocks, it is symmetrical arranged between briquetting and hanging beam and is connected with two extension springs, hydraulic jack is provided between two extension springs.Compared with the existing, the utility model solves the big aligning of aviation part deflection.
Description
Technical field
Aviation part manufacture field is the utility model is related to, more particularly to a kind of aviation part deformation straightening device.
Background technology
In the process for manufacturing aviation part, workpiece bending deformed situation often occurs, has plenty of elongated
Part, in process, part and material frame deform together, two bending.Have plenty of because this body structure of part is (such as list
Surface frame) in process, deformed after cutting, two is bent upwards.Have plenty of after being heat-treated because of part, inside parts
Organize the caused deformation that changes.Three of the above deforms, in digital control processing, it is necessary to is effectively controlled and solves,
It can continue to process.
If deflection is minimum, in rough machined margin range, numeric control can be become by having a shave repeatedly to eliminate
Shape, when deflection exceedes allowance, then deformation can not be eliminated by having a shave repeatedly, but there is no effectively eliminate change so far
Shape utensil, seriously constrain continuing for production.
Utility model content
The purpose of this utility model, which is that, provides a kind of aviation part deformation straightening device, the aviation part deformation straightening device
Solves the problems, such as the big aligning of aviation part deflection.
The technical solution of the utility model is：A kind of aviation part deformation straightening device, the aviation part deformation straightening device
Including bottom plate, hanging beam and two support columns, two support column one end are symmetrically connected to hanging beam both ends, the other end and bottom plate
It is connected, two isometry blocks is also symmetrically arranged with bottom plate, two isometry blocks is additionally provided with spacing between two support columns on bottom plate
Block, for limited block between two isometry blocks, spacing tile height is less than two isometry blocks, and briquetting, briquetting are provided with above two isometry blocks
It is symmetrical arranged between hanging beam and is connected with two extension springs, hydraulic jack is provided between two extension springs.
Preferably, the hydraulic jack is Manual hydraulic jack.
Preferably, the hydraulic jack is just to put Manual hydraulic jack.
Preferably, the Manual hydraulic jack is irreversible Manual hydraulic jack.
Preferably, regulation correcting value unit is provided with the limited block.
Preferably, the regulation correcting value unit is adjusting nut.
Inventive principle and beneficial effect：
Inventor is had found by studying, because the external force that correction applies have to be larger than inner stress of work and external carbuncle sum
The complete effect of correction can be played, therefore the utility model applies external force using Manual hydraulic jack, is controlled by external force
Correct amount processed.It has furthermore been found that because the Manual hydraulic jack of the inverted installation of energy must have external oil way and fuel tank, therefore
Using can not be reverse mounted hydraulic jack can not be reverse mounted, according to " material apply active force have it is much, what it bore
Reaction force just has much ", inventor is just putting Manual hydraulic jack, while by two tension springs, the briquetting of two pieces one,
To carry out external force transmission.
Brief description of the drawings
Fig. 1 is the overall structure diagram of the utility model embodiment 1；
Fig. 2 is the structural representation of the utility model embodiment 2.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in further detail.
Embodiment 1
As shown in figure 1, a kind of aviation part deformation straightening device, including bottom plate 6, hanging beam 3 and two support columns 9, this two
The one end of root support column 9 is symmetrically connected to the both ends of hanging beam 3, and the other end is connected to bottom plate 6, two etc. are also symmetrically arranged with bottom plate 6
High block 7, two isometry blocks 7 are additionally provided with limited block 8, limited block 8 is located at two isometry blocks between two support columns 9 on bottom plate 6
Between 7, the height of limited block 8 is less than two isometry blocks 7, and the top of two isometry block 7 is provided with briquetting 4, right between briquetting 4 and hanging beam 3
Claim setting to be connected with two extension springs 1, Manual hydraulic jack 2 is provided between two extension springs 1.
Manual hydraulic jack 2 is irreversible Manual hydraulic jack.
During correction, part 5 is placed on two isometry blocks 7 and can be carried out corrective operations.
Embodiment 2
As shown in Fig. 2 a kind of aviation part deformation straightening device, including bottom plate 6, hanging beam 3 and two support columns 9, this two
The one end of root support column 9 is symmetrically connected to the both ends of hanging beam 3, and the other end is connected to bottom plate 6, two etc. are also symmetrically arranged with bottom plate 6
High block 7, two isometry blocks 7 are additionally provided with limited block 8, limited block 8 is located at two isometry blocks between two support columns 9 on bottom plate 6
Between 7, the height of limited block 8 is less than two isometry blocks 7, and regulation correcting value unit 10 is provided with limited block 8, adjusts correcting value unit
10 can be arranged on the bottom of limited block 8, can also be arranged on other positions, as long as the height of limited block 8 can be adjusted.Adjust
Section correcting value unit 10 can use adjusting nut.
The top of two isometry block 7 is provided with briquetting 4, is symmetrical arranged between briquetting 4 and hanging beam 3 and is connected with two extension springs 1, and two draw
Manual hydraulic jack 2 is provided between spring 1.
During correction, part 5 is placed on two isometry blocks 7, regulation correcting value unit 10, it is possible to carry out corrective operations
If part deformation amount is little, limited block 8 can be adjusted than two isometry blocks, 7 low 1mm, part 5 is taken out after aligning and is examined
Survey, if being not reaching to effect, then turn down limited block 8, then align, need precision until reaching.
Claims (6)
- A kind of 1. aviation part deformation straightening device, it is characterised in that：The aviation part deformation straightening device includes bottom plate, hanging beam With two support columns, two support column one end are symmetrically connected to hanging beam both ends, and the other end is connected with bottom plate, also right on bottom plate Title is provided with two isometry blocks, and two isometry blocks are additionally provided with limited block between two support columns on bottom plate, limited block is located at two Between isometry block, spacing tile height is less than two isometry blocks, and briquetting is provided with above two isometry blocks, symmetrical between briquetting and hanging beam Setting is connected with two extension springs, and hydraulic jack is provided between two extension springs.
- 2. aviation part deformation straightening device according to claim 1, it is characterised in that：The hydraulic jack is manual liquid Press jack.
- 3. aviation part deformation straightening device according to claim 2, it is characterised in that：The hydraulic jack is just to put hand Hydrodynamic pressure jack.
- 4. aviation part deformation straightening device according to claim 3, it is characterised in that：The Manual hydraulic jack is not Can inverted Manual hydraulic jack.
- 5. according to any described aviation part deformation straightening devices of claim 1-4, it is characterised in that：Set on the limited block There is regulation correcting value unit.
- 6. aviation part deformation straightening device according to claim 5, it is characterised in that：The regulation correcting value unit is tune Save nut.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720752369.7U CN206966361U (en) | 2017-06-26 | 2017-06-26 | Aviation part deformation straightening device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720752369.7U CN206966361U (en) | 2017-06-26 | 2017-06-26 | Aviation part deformation straightening device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206966361U true CN206966361U (en) | 2018-02-06 |
Family
ID=61405772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720752369.7U Active CN206966361U (en) | 2017-06-26 | 2017-06-26 | Aviation part deformation straightening device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206966361U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110064682A (en) * | 2019-05-14 | 2019-07-30 | 珠海格力智能装备有限公司 | Crooked correction equipment |
| CN111604386A (en) * | 2020-04-17 | 2020-09-01 | 红云红河烟草(集团)有限责任公司 | Device for correcting deformation of box cover of leaf storage box |
-
2017
- 2017-06-26 CN CN201720752369.7U patent/CN206966361U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110064682A (en) * | 2019-05-14 | 2019-07-30 | 珠海格力智能装备有限公司 | Crooked correction equipment |
| CN111604386A (en) * | 2020-04-17 | 2020-09-01 | 红云红河烟草(集团)有限责任公司 | Device for correcting deformation of box cover of leaf storage box |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 610000 No. 18, Ganxi Road, Industrial Development Zone, Jinyuan Town, Dayi County, Chengdu, Sichuan Patentee after: Chengdu chaohepur Aviation Technology Co.,Ltd. Address before: 610000 No. 18, Ganxi Road, Industrial Development Zone, Jinyuan Town, Dayi County, Chengdu, Sichuan Patentee before: CHENGDU JIAODA PUER INDUSTRIAL Co.,Ltd. |
|
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 610000 No. 18, Ganxi Road, Industrial Development Zone, Jinyuan Town, Dayi County, Chengdu, Sichuan Patentee after: Chengdu Chaohepu Aviation Technology Co.,Ltd. Address before: 610000 No. 18, Ganxi Road, Industrial Development Zone, Jinyuan Town, Dayi County, Chengdu, Sichuan Patentee before: Chengdu chaohepur Aviation Technology Co.,Ltd. |