CN212761309U - Aviation panel production is with drilling mould - Google Patents
Aviation panel production is with drilling mould Download PDFInfo
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- CN212761309U CN212761309U CN202021607080.4U CN202021607080U CN212761309U CN 212761309 U CN212761309 U CN 212761309U CN 202021607080 U CN202021607080 U CN 202021607080U CN 212761309 U CN212761309 U CN 212761309U
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- drilling
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- connecting rod
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Abstract
The utility model relates to a drilling field specifically is a drilling mould is used in aviation panel production, including drilling board, fixed plate and clamping device, be equipped with the drilling on the drilling board, be equipped with fixing bolt on the drilling board, the last connecting rod that is equipped with of fixing bolt, the connecting rod below is equipped with fixed boss, fixed boss below is equipped with the nut, is equipped with the through-hole slot on the fixed plate, and the fixed plate bottom surface is equipped with the bottom plate, is equipped with clamping device on the bottom plate, is equipped with the telescopic shaft on the clamping device, is equipped with the spring on the telescopic shaft; the beneficial effects are that: the utility model provides an aviation is drilling jig for panel production carries out configuration optimization to traditional drilling jig for the material resources of using manpower sparingly more conveniently simultaneously.
Description
Technical Field
The utility model relates to a drilling field specifically is a drilling mould is used in aviation panel production.
Background
The traditional processing steps of aviation plate drilling are as follows: the aviation plate is well positioned on a workbench by a professional fitter, then the aviation plate is manually marked by a height gauge according to the drawing requirements, the coordinates of a workpiece are marked, the professional fitter aligns to the marked line and beats a center hole, finally the aviation plate is placed on punching equipment, and the professional fitter aligns to each center hole to drill holes on the equipment.
In the prior art, the traditional processing method has high processing difficulty, high requirement on drilling technology, poor consistency of processed products, and needs professional workers, so that the labor cost is increased, and thus, a drilling die is needed to realize the processing of aviation plates; therefore, the utility model provides an aviation panel production is with drilling mould is with solution problem.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aviation is drilling die for panel production to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an aviation panel production is with drilling mould, includes drilling board, fixed plate and clamping device, be equipped with drilling on the drilling board, be equipped with fixing bolt on the drilling board, the last connecting rod that is equipped with of fixing bolt, the connecting rod below is equipped with fixed boss, and fixed boss below is equipped with the nut, is equipped with the through-hole slot on the fixed plate, and the fixed plate bottom surface is equipped with the bottom plate, is equipped with clamping device on the bottom plate, is equipped with the telescopic shaft on the clamping device, is equipped with the spring on the.
Preferably, the drilling plate is of a cuboid structure, a fixing bolt is fixedly connected with the connecting rod, the connecting rod penetrates through the fixing boss, and the connecting rod and the fixing boss are fixedly connected through a nut.
Preferably, the through-hole slot is the cuboid structure, and the bottom plate is the U word structure, and the telescopic shaft is the cylinder structure, telescopic shaft and bottom plate side fixed connection, spring and telescopic shaft top and middle section fixed connection, and the grip block is the cuboid structure, grip block and telescopic shaft fixed connection.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model provides an aviation panel production is with drilling mould carries out configuration optimization to traditional drilling mould, through setting up clamping device application telescopic shaft and spring for aviation panel can all be fixed at the clamping within range.
2. The utility model provides an aviation panel production is with drilling mould carries out configuration optimization to traditional drilling mould, through setting up fixed plate and through-hole slot, can reciprocate the drilling plate, and accessible nut is fixed with the connecting rod simultaneously, can drill to the aviation panel of co-altitude not.
Drawings
Fig. 1 is the utility model discloses aviation panel production is with drilling mould structure chart.
In the figure: drilling board 1, fixed plate 2, bottom plate 3, through-hole slot 4, drilling 5, fixed boss 6, fixing bolt 7, connecting rod 8, nut 9, clamping device 10, telescopic shaft 11, spring 12, grip block 13.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below. The embodiments of the present invention, all other embodiments obtained by a person skilled in the art without creative work, all belong to the protection scope of the present invention.
Referring to fig. 1, the present invention provides a technical solution: the utility model provides an aviation is drilling mould for panel production, including drilling board 1, fixed plate 2 and clamping device 10, be equipped with drilling 5 on the drilling board 1, be equipped with fixing bolt 7 on the drilling board 1, the last connecting rod 8 that is equipped with of fixing bolt 7, connecting rod 8 below is equipped with fixed boss 6, 6 below fixed boss are equipped with nut 9, be equipped with through-hole slot 4 on the fixed plate 2, 2 bottom surfaces of fixed plate are equipped with bottom plate 3, be equipped with clamping device 10 on the bottom plate 3, be equipped with telescopic shaft 11 on the clamping device 10, be equipped with spring 12 on the telescopic shaft 11, be equipped with grip block 13.
Through-hole slot 4 is the cuboid structure, and bottom plate 3 is the U word structure, and telescopic shaft 11 is the cylinder structure, telescopic shaft 11 and 3 side fixed connection of bottom plate, spring 12 and 11 tops of telescopic shaft and middle section fixed connection, grip block 13 is the cuboid structure, grip block 13 and 11 fixed connection of telescopic shaft.
The working principle is as follows: during operation, press grip block 13, grip block 13 and 11 fixed connection of telescopic shaft, spring 12 and 11 tops of telescopic shaft and middle section fixed connection, make 11 contractions of telescopic shaft, spring 12 is compressed simultaneously, place aviation panel on bottom plate 3, spring 12 kick-backs simultaneously, telescopic shaft 11 is driven tensile, grip block 13 presss from both sides aviation panel tightly, then select the drilling height according to panel thickness, insert drilling plate 1 through-hole slot 4, use fixing bolt 7, connecting rod 8 and nut 9 are fixed, use drilling equipment to change the hole through drilling 5, this device fixed panel need not the bolt and fixes, dismantle simple to operate, fix drilling plate 1 simultaneously, make and can not take place the aversion at drilling process.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (3)
1. The utility model provides an aviation panel production is with drilling mould, includes drilling board (1), fixed plate (2) and clamping device (10), its characterized in that: be equipped with drilling (5) on drilling board (1), be equipped with fixing bolt (7) on drilling board (1), be equipped with connecting rod (8) on fixing bolt (7), connecting rod (8) below is equipped with fixed boss (6), fixed boss (6) below is equipped with nut (9), be equipped with through-hole slot (4) on fixed plate (2), fixed plate (2) bottom surface is equipped with bottom plate (3), be equipped with clamping device (10) on bottom plate (3), be equipped with telescopic shaft (11) on clamping device (10), be equipped with spring (12) on telescopic shaft (11), be equipped with grip block (13) on telescopic shaft (11).
2. The aviation board production drilling die as claimed in claim 1, wherein: drilling board (1) is the cuboid structure, fixing bolt (7) and connecting rod (8) fixed connection, and connecting rod (8) pass fixed boss (6), and nut (9) are with connecting rod (8) and fixed boss (6) bolt fixed connection.
3. The aviation board production drilling die as claimed in claim 1, wherein: through-hole slot (4) are the cuboid structure, and bottom plate (3) are the U word structure, and telescopic shaft (11) are the cylinder structure, telescopic shaft (11) and bottom plate (3) side fixed connection, spring (12) and telescopic shaft (11) top and middle section fixed connection, grip block (13) are the cuboid structure, grip block (13) and telescopic shaft (11) fixed connection.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202021607080.4U CN212761309U (en) | 2020-08-05 | 2020-08-05 | Aviation panel production is with drilling mould |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202021607080.4U CN212761309U (en) | 2020-08-05 | 2020-08-05 | Aviation panel production is with drilling mould |
Publications (1)
Publication Number | Publication Date |
---|---|
CN212761309U true CN212761309U (en) | 2021-03-23 |
Family
ID=75050291
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202021607080.4U Active CN212761309U (en) | 2020-08-05 | 2020-08-05 | Aviation panel production is with drilling mould |
Country Status (1)
Country | Link |
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CN (1) | CN212761309U (en) |
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2020
- 2020-08-05 CN CN202021607080.4U patent/CN212761309U/en active Active
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