CN206200065U - A kind of airplane parts riveting set - Google Patents
A kind of airplane parts riveting set Download PDFInfo
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- CN206200065U CN206200065U CN201621297523.8U CN201621297523U CN206200065U CN 206200065 U CN206200065 U CN 206200065U CN 201621297523 U CN201621297523 U CN 201621297523U CN 206200065 U CN206200065 U CN 206200065U
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- riveting
- expansion link
- crossbeam
- component
- airplane parts
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Abstract
A kind of airplane parts riveting set, it is related to a kind of riveting set, and in particular to a kind of airplane parts riveting set.The utility model can only carry out the amount of movement regulation of single direction to solve existing airplane parts riveting set, when causing operative, it is often necessary to which moving parts coordinate riveting set, influence the problem of production efficiency.The utility model includes riveting machine, riveting platform, crossbeam, moving beam component, screw rod, bearing block, telescopic boom component and bracket component, crossbeam is arranged on the bracket component, riveting machine is connected by the moving beam component with crossbeam, riveting platform is arranged on the lower section of riveting machine, the telescopic boom component is connected with one end of crossbeam, and one end of screw rod is connected through the telescopic boom component with the bearing block on riveting machine.The utility model belongs to aircraft manufacturing field.
Description
Technical field
The utility model is related to a kind of riveting set, and in particular to a kind of airplane parts riveting set, belongs to aircraft manufacturing
Field.
Background technology
Having substantial amounts of part during aircraft manufacturing needs riveting.Due to using the production continuous assembling work of wire type,
Therefore existing airplane parts riveting set can only carry out the amount of movement regulation of single direction, when causing operative, it is often necessary to
Moving parts coordinate riveting set, influence production efficiency.
The content of the invention
The utility model is to solve existing airplane parts riveting set to carry out the amount of movement regulation of single direction, is caused
During operative, it is often necessary to which moving parts coordinate riveting set, the problem of production efficiency is influenceed, and then propose a kind of aircraft zero
Part riveting set.
The utility model is adopted the technical scheme that to solve the above problems：The utility model includes that riveting machine, riveting are flat
Platform, crossbeam, moving beam component, screw rod, bearing block, telescopic boom component and bracket component, crossbeam are arranged on the support group
On part, riveting machine is connected by the moving beam component with crossbeam, and riveting platform is arranged on the lower section of riveting machine, described flexible
Support arm assembly is connected with one end of crossbeam, and one end of screw rod connects through the telescopic boom component with the bearing block on riveting machine
Connect.
Further, the moving beam component includes slip cap, first sleeve and the first expansion link, and slip cap is sleeved on
On crossbeam, and slip cap can be moved linearly along crossbeam, and one end of first sleeve is connected with slip cap, and one end of the first expansion link is inserted
In the other end of first sleeve, the other end of the first expansion link is connected with riveting machine.
Further, the telescopic boom component includes the second sleeve pipe, the second expansion link, the first bolt, second set
One end of pipe is connected with one end of crossbeam, and one end of the second expansion link is inserted into the other end of the second sleeve pipe, for fixing
First bolt of two expansion links is inserted on the lateral wall of the second sleeve pipe.
Further, the bracket component is made up of two support units, each described support unit include the 3rd sleeve pipe,
3rd expansion link and the second bolt, the lower end of the 3rd sleeve pipe are connected with riveting platform, and the lower end of the 3rd expansion link is inserted into
In the upper end of the 3rd sleeve pipe, the upper end of the 3rd expansion link is connected with the end of crossbeam, and second for fixing the 3rd expansion link is determined
Position bolt is inserted on the lateral wall of the 3rd sleeve pipe.
Further, the other end of screw rod is provided with rotation handle.
Further, rivet platform is respectively arranged at two ends with feed conveyor belt and infeed conveyor.
Further, the lower surface of riveting platform is laid with multiple levelling shoes.
The beneficial effects of the utility model are：1st, the utility model can carry out three amount of movement regulations in direction, without
Workman's moving parts coordinate riveting set, substantially increase production efficiency, improve riveting precision, it is to avoid error occur；2nd, originally
Utility model uses conveyer belt self-feeding and discharging, effectively raises operating efficiency；3rd, the utility model is using tune manually
Section, makes degree of regulation more accurate；4th, the utility model simple structure, it is easy to operate.
Brief description of the drawings
Fig. 1 is overall structure diagram of the present utility model, and Fig. 2 is top view of the present utility model.
Specific embodiment
Specific embodiment one：With reference to Fig. 1 and Fig. 2 explanation present embodiments, a kind of airplane parts described in present embodiment
Riveting set include riveting machine 1, riveting platform 2, crossbeam 3, moving beam component, screw rod 4, bearing block 5, telescopic boom component and
Bracket component, crossbeam 3 is arranged on the bracket component, and riveting machine 1 is connected by the moving beam component with crossbeam 3, riveting
The lower section that platform 2 is arranged on riveting machine 1 is connect, the telescopic boom component is connected with one end of crossbeam 3, and one end of screw rod 4 passes through
The telescopic boom component is connected with the bearing block 5 on riveting machine 1.
Specific embodiment two：With reference to Fig. 1 and Fig. 2 explanation present embodiments, a kind of airplane parts described in present embodiment
The moving beam component of riveting set includes slip cap 6, the expansion link 8 of first sleeve 7 and first, and slip cap 6 is sleeved on crossbeam 3
On, and slip cap 6 can move linearly along crossbeam 3, one end of first sleeve 7 is connected with slip cap 6, one end of the first expansion link 8
It is inserted into the other end of first sleeve 7, the other end of the first expansion link 8 is connected with riveting machine 1.Other compositions and annexation
It is identical with specific embodiment one.
Specific embodiment three：With reference to Fig. 1 and Fig. 2 explanation present embodiments, a kind of airplane parts described in present embodiment
The telescopic boom component of riveting set includes the second sleeve pipe 9, the second expansion link 10, the first bolt 11, the one of the second sleeve pipe 9
End is connected with one end of crossbeam 3, and one end of the second expansion link 10 is inserted into the other end of the second sleeve pipe 9, for fixing second
First bolt 11 of expansion link 10 is inserted on the lateral wall of the second sleeve pipe 9.Other compositions and annexation and specific reality
Apply mode one identical.
Specific embodiment four：With reference to Fig. 1 and Fig. 2 explanation present embodiments, a kind of airplane parts described in present embodiment
The bracket component of riveting set is made up of two support units, and each described support unit includes that the 3rd sleeve pipe the 12, the 3rd stretches
The bolt 14 of bar 13 and second, the lower end of the 3rd sleeve pipe 12 is connected with riveting platform 2, and the lower end of the 3rd expansion link 13 is inserted into
In the upper end of the 3rd sleeve pipe 12, the upper end of the 3rd expansion link 13 is connected with the end of crossbeam 3, for fixing the 3rd expansion link 13
Second bolt 14 is inserted on the lateral wall of the 3rd sleeve pipe 12.Other compositions and annexation and the phase of specific embodiment one
Together.
Specific embodiment five：With reference to Fig. 1 and Fig. 2 explanation present embodiments, a kind of airplane parts described in present embodiment
The other end of the screw rod 4 of riveting set is provided with rotation handle 15.Other compositions and annexation are identical with specific embodiment one.
Specific embodiment six：With reference to Fig. 1 and Fig. 2 explanation present embodiments, a kind of airplane parts described in present embodiment
The riveting platform 2 of riveting set is respectively arranged at two ends with feed conveyor belt 16 and infeed conveyor 17.Other compositions and connection are closed
System is identical with specific embodiment one.
Specific embodiment seven：With reference to Fig. 1 and Fig. 2 explanation present embodiments, a kind of airplane parts described in present embodiment
The lower surface of the riveting platform 2 of riveting set is laid with multiple levelling shoes 18.Other compositions and annexation and specific reality
Apply mode one identical.
The above, is only preferred embodiment of the present utility model, not makees any formal to the utility model
Limitation, although the utility model is disclosed above with preferred embodiment, but is not limited to the utility model, any ripe
Professional and technical personnel is known, is not being departed from the range of technical solutions of the utility model, when in the technology using the disclosure above
Appearance makes a little change or is modified to the Equivalent embodiments of equivalent variations, as long as being without departing from technical solutions of the utility model
Hold, according to technical spirit of the present utility model, within spirit of the present utility model and principle, what above example was made appoints
What simple modification, equivalent and improvement etc., still falls within the protection domain of technical solutions of the utility model.
Claims (7)
1. a kind of airplane parts riveting set, it is characterised in that：A kind of airplane parts riveting set includes riveting machine（1）、
Riveting platform（2）, crossbeam（3）, moving beam component, screw rod（4）, bearing block（5）, telescopic boom component and bracket component, it is horizontal
Beam（3）On the bracket component, riveting machine（1）By the moving beam component and crossbeam（3）Connection, rivets platform
（2）It is arranged on riveting machine（1）Lower section, the telescopic boom component and crossbeam（3）One end connection, screw rod（4）One end wear
Cross the telescopic boom component and riveting machine（1）On bearing block（5）Connection.
2. a kind of airplane parts riveting set according to claim 1, it is characterised in that：The moving beam component includes sliding
Dynamic set（6）, first sleeve（7）With the first expansion link（8）, slip cap（6）It is sleeved on crossbeam（3）On, and slip cap（6）Can be along horizontal stroke
Beam（3）Rectilinear movement, first sleeve（7）One end and slip cap（6）Connection, the first expansion link（8）One end be inserted into first
Sleeve pipe（7）The other end in, the first expansion link（8）The other end and riveting machine（1）Connection.
3. a kind of airplane parts riveting set according to claim 1, it is characterised in that：The telescopic boom component includes the
Two sleeve pipes（9）, the second expansion link（10）, the first bolt（11）, the second sleeve pipe（9）One end and crossbeam（3）One end connect
Connect, the second expansion link（10）One end be inserted into the second sleeve pipe（9）The other end in, for fixing the second expansion link（10）
One bolt（11）It is inserted into the second sleeve pipe（9）Lateral wall on.
4. a kind of airplane parts riveting set according to claim 1, it is characterised in that：The bracket component is by two supports
Unit is constituted, and each described support unit includes the 3rd sleeve pipe（12）, the 3rd expansion link（13）With the second bolt（14）, the
Three sleeve pipes（12）Lower end with riveting platform（2）Connection, the 3rd expansion link（13）Lower end be inserted into the 3rd sleeve pipe（12）It is upper
In end, the 3rd expansion link（13）Upper end and crossbeam（3）End connection, for fixing the 3rd expansion link（13）Second positioning
Bolt（14）It is inserted into the 3rd sleeve pipe（12）Lateral wall on.
5. a kind of airplane parts riveting set according to claim 1, it is characterised in that：Screw rod（4）The other end be provided with turn
Fixed handle（15）.
6. a kind of airplane parts riveting set according to claim 1, it is characterised in that：Riveting platform（2）Two ends difference
It is provided with feed conveyor belt（16）And infeed conveyor（17）.
7. a kind of airplane parts riveting set according to claim 1, it is characterised in that：Riveting platform（2）Lower surface it is equal
It is laid with multiple levelling shoes（18）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621297523.8U CN206200065U (en) | 2016-11-30 | 2016-11-30 | A kind of airplane parts riveting set |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621297523.8U CN206200065U (en) | 2016-11-30 | 2016-11-30 | A kind of airplane parts riveting set |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206200065U true CN206200065U (en) | 2017-05-31 |
Family
ID=58751628
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621297523.8U Active CN206200065U (en) | 2016-11-30 | 2016-11-30 | A kind of airplane parts riveting set |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206200065U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107377856A (en) * | 2017-08-15 | 2017-11-24 | 扬州五岳电器有限公司 | A kind of bimetal leaf connects iron nail forming machine |
| CN108043974A (en) * | 2017-12-08 | 2018-05-18 | 桃江飞尔照明有限公司 | A kind of riveting device and production method for coldplate |
-
2016
- 2016-11-30 CN CN201621297523.8U patent/CN206200065U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107377856A (en) * | 2017-08-15 | 2017-11-24 | 扬州五岳电器有限公司 | A kind of bimetal leaf connects iron nail forming machine |
| CN107377856B (en) * | 2017-08-15 | 2024-02-23 | 扬州五岳电器有限公司 | Forming machine for bimetal strip connecting iron nails |
| CN108043974A (en) * | 2017-12-08 | 2018-05-18 | 桃江飞尔照明有限公司 | A kind of riveting device and production method for coldplate |
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| 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: 519000 Room 612, 6th Floor, Office Building of Zhuhai Airport Group, Haicheng Township, Sanzao Town, Zhuhai City, Guangdong Province Patentee after: Guanglian Airlines (Zhuhai) Co., Ltd. Address before: 519000 Room 612, 6th Floor, Office Building of Zhuhai Airport Group, Haicheng Township, Sanzao Town, Zhuhai City, Guangdong Province Patentee before: Zhuhai Guanglian general aviation equipment Co. Ltd. |