CN206435983U - A kind of aircraft clip class part forming mould - Google Patents
A kind of aircraft clip class part forming mould Download PDFInfo
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- CN206435983U CN206435983U CN201621372580.8U CN201621372580U CN206435983U CN 206435983 U CN206435983 U CN 206435983U CN 201621372580 U CN201621372580 U CN 201621372580U CN 206435983 U CN206435983 U CN 206435983U
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- clamping plate
- fuse
- plate
- left clamping
- right clamping
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Abstract
A kind of aircraft clip class part forming mould, contain bottom plate, fuse, right clamping plate, left clamping plate, fuse is fixed on the middle part of bottom plate by connector, provided with horizontal through hole at the caudal peduncle of fuse, the inner side of right clamping plate and left clamping plate is matched with the lateral face of clip part, the front end of right clamping plate and left clamping plate is hinged on the front end of bottom plate by connector, right clamping plate and left clamping plate are combined into the forming face of part with fuse, the rear end of right clamping plate and left clamping plate is respectively equipped with drill bushing hole corresponding with fuse caudal peduncle through hole, the plate of strip is clamped between fuse and right clamping plate and left clamping plate, make the matched moulds of right clamping plate and left clamping plate and fuse by handle, the connecting hole at clip part two ends is made by the through hole in coaxial drill bushing hole and fuse afterbody again.
Description
Technical field
The application is related to aircraft manufacturing technology, specifically a kind of shaping dies of aircraft clip class part.
Background technology
Aircraft clip class part is a kind of curved class part of plate for being used to connect pipe, because aircraft pipeline is more, pipe diameter
Different, so aircraft clip class part specifications are a lot, but batch is small.Two sets of bending dies and a set of drill jig are typically needed during shaping.Two
Set bending die is used for the profile that clip class part is shaped on punch press, and drill jig is used to drill the hole on part.Using this side
Legal system makes part, needs three molds, and die manufacturing cycle is long, and cost is high, low production efficiency, it is impossible to meet the need of Aircraft Production
Will.For such case, it is badly in need of finding a kind of new easy manufacturing process, to meet the need of aircraft clip class part production
Ask.It is required that mould structure is simple, it is easy to manufacture, the manufacturing cycle is short, and cost is low.Require that mould is easy to use simultaneously, it is easy to operate, with
Improve production efficiency.
The content of the invention
The purpose of the application is to provide a kind of new easy aircraft clip class part forming shaping dies.
A kind of aircraft clip class part forming mould, it is characterised in that：The mould contains bottom plate, fuse, right clamping plate, Zuo Jia
Plate, the main body of described fuse is a circular block structure, and the afterbody of fuse has the caudal peduncle of strip and block, its profile and clip
Part medial type face is matched, and fuse is fixed on by connector provided with horizontal through hole at the middle part of bottom plate, the caudal peduncle of fuse, right
The inner side of clamping plate and left clamping plate is matched with the lateral face of clip part, and the front end of right clamping plate and left clamping plate is hinged by connector
In the front end of bottom plate, right clamping plate and left clamping plate and fuse are combined into the rear end point in the forming face of part, right clamping plate and left clamping plate
Not She You drill bushing hole corresponding with fuse caudal peduncle through hole, be additionally provided with handle in the rear end tails of right clamping plate and left clamping plate.
In use, the plate of strip is clamped between fuse and right clamping plate and left clamping plate, by handle make right clamping plate and
The matched moulds of left clamping plate and fuse, shapes clip part shape, then make by the through hole in coaxial drill bushing hole and fuse afterbody
The connecting hole at clip part two ends.
The beneficial effect of the application is that forming die structure is rationally simple, easy to use, using one set of die, can
The profile of formation of parts, can drill the hole on part again, fully meet the demand of aircraft clip class part production.
Accompanying drawing is described in further detail to the application with reference to embodiments.
Brief description of the drawings
Fig. 1 is the aircraft clip class part forming mould of the application.
Fig. 2 is Fig. 1 lateral structure signal.
Fig. 3 is Fig. 1 horizontality structural representation.
Fig. 4 is the aircraft clip class part shaping techniques of the application.
Explanation is numbered in figure：1 fuse, 2 right clamping plates, 3 rank type screws, 4 left clamping plates, 5 bottom plates, 6 connectors, 7 handles, 8 are bored
Cover hole, 9 through holes, 10 clip parts.
Embodiment
Referring to accompanying drawing, the aircraft clip class part forming mould of the application contains bottom plate 5, fuse 1, right clamping plate 2, Zuo Jia
Plate 4, the main body of described fuse 1 is a circular block structure, and the afterbody of fuse has outside the caudal peduncle of strip and block, fuse 1
Shape is matched with the medial type face of clip part 10, and fuse 1 is fixed on the middle part of bottom plate 5 by connector 6, and the caudal peduncle portion of fuse 1 is set
There is horizontal through hole 9, the inner side of right clamping plate 2 and left clamping plate 4 is matched with the lateral face of clip part 10, right clamping plate 2 and left folder
Plate 4 is combined into the both sides forming face of part with fuse 1, and the front end of right clamping plate 2 and left clamping plate 4 passes through connector rank type screw 3
The front end of bottom plate 5 is hinged on, the rear end of right clamping plate 2 and left clamping plate 4 is respectively equipped with and the corresponding drill bushing hole of fuse caudal peduncle portion through hole 9
8, it is additionally provided with handle 7 in the rear end tails of right clamping plate 2 and left clamping plate 4.
Application method is as follows：It is the plate of a strip before the shaping of aircraft clip class part 10, the plate of strip is clamped in
Between fuse 1 and right clamping plate 2 and left clamping plate 4, operation handle 7 makes right clamping plate 2, left clamping plate 4 be rotated around rank type screw 3, closure
Right clamping plate 2 and left clamping plate 4 and the matched moulds of fuse 1, are adjacent to the plate of strip and paste contour forming on fuse 1, the right side is passed through using instrument
Make the connecting hole at the two ends of clip part 10 in the coaxial drill bushing hole 8 of clamping plate 2, left clamping plate 4.
Claims (1)
1. a kind of aircraft clip class part forming mould, it is characterised in that：The mould contains bottom plate, fuse, right clamping plate, Zuo Jia
Plate, the main body of described fuse is a circular block structure, and the afterbody of fuse has the caudal peduncle of strip and block, its profile and clip
Part medial type face is matched, and fuse is fixed on by connector provided with horizontal through hole at the middle part of bottom plate, the caudal peduncle of fuse, right
The inner side of clamping plate and left clamping plate is matched with the lateral face of clip part, and the front end of right clamping plate and left clamping plate is hinged by connector
In the front end of bottom plate, right clamping plate and left clamping plate and fuse are combined into the rear end point in the forming face of part, right clamping plate and left clamping plate
Not She You drill bushing hole corresponding with fuse caudal peduncle through hole, be additionally provided with handle in the rear end tails of right clamping plate and left clamping plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621372580.8U CN206435983U (en) | 2016-12-14 | 2016-12-14 | A kind of aircraft clip class part forming mould |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621372580.8U CN206435983U (en) | 2016-12-14 | 2016-12-14 | A kind of aircraft clip class part forming mould |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206435983U true CN206435983U (en) | 2017-08-25 |
Family
ID=59647825
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621372580.8U Active CN206435983U (en) | 2016-12-14 | 2016-12-14 | A kind of aircraft clip class part forming mould |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206435983U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106670813A (en) * | 2016-12-14 | 2017-05-17 | 中航飞机股份有限公司西安飞机分公司 | Forming method and mold for airplane clamping hoop part |
-
2016
- 2016-12-14 CN CN201621372580.8U patent/CN206435983U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106670813A (en) * | 2016-12-14 | 2017-05-17 | 中航飞机股份有限公司西安飞机分公司 | Forming method and mold for airplane clamping hoop part |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: No. 710089 in Shaanxi province Xi'an city Yanliang District West Avenue Patentee after: AVIC Xi'an Aircraft Industry Group Co.,Ltd. Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee before: AVIC AIRCRAFT Corp. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210617 Address after: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee after: AVIC AIRCRAFT Corp. Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee before: XI'AN AIRCRAFT BRANCH OF XI'AN AIRCRAFT INTERNATIONAL Corp. |