CN209937061U - Perforating machine for aerospace materials - Google Patents
Perforating machine for aerospace materials Download PDFInfo
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- CN209937061U CN209937061U CN201920737025.8U CN201920737025U CN209937061U CN 209937061 U CN209937061 U CN 209937061U CN 201920737025 U CN201920737025 U CN 201920737025U CN 209937061 U CN209937061 U CN 209937061U
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- plate
- positioning
- backplate
- sliding
- screw rod
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Abstract
The utility model provides an aerospace puncher for material, includes puncher body, backplate, bottom plate, slide bar, regulating plate, fixed plate, splint, slide, locating plate, screw rod, the puncher body has the backplate, backplate sub-unit connection bottom plate, backplate upper portion joint support board, the screw rod passes backplate, backup pad in proper order, and the nut No. one of threaded connection is passed through at the screw rod both ends, regulating plate sub-unit connection bottom plate, regulating plate upper portion have the connecting plate, the slide bar passes backup pad, connecting plate in proper order, and the slide bar both ends are through No. two nuts of threaded connection, and the slide bar has a plurality of locating holes No. one, and the connecting plate has No. two locating holes, and No. one the locating hole is corresponding with No. two locating holes, and fixing bolt passes No. two locating holes in proper.
Description
Technical Field
The utility model relates to an aerospace field especially relates to a puncher for aerospace material.
Background
The puncher is comparatively single to material clamping structure when aerospace material punches, can not adjust the centre gripping according to the not unidimensional of material, influences the stability to the material location, and the operation in-process takes place drunkenness, skew easily, causes the deviation of punching, and the material is extravagant, has the drawback.
SUMMERY OF THE UTILITY MODEL
The utility model discloses it is not enough to the above-mentioned that prior art exists, provide a puncher for aerospace material rational in infrastructure.
The utility model aims at realizing through the following technical scheme:
the utility model provides an aerospace puncher for material, includes puncher body, backplate, bottom plate, slide bar, regulating plate, fixed plate, splint, slide, locating plate, screw rod, the puncher body has the backplate, backplate sub-unit connection bottom plate, backplate upper portion joint support board, the screw rod passes backplate, backup pad in proper order, and the nut No. one of threaded connection is passed through at the screw rod both ends, regulating plate sub-unit connection bottom plate, regulating plate upper portion have the connecting plate, the slide bar passes backup pad, connecting plate in proper order, and the slide bar both ends are through No. two nuts of threaded connection, and the slide bar has a plurality of locating holes No. one, and the connecting plate has No. two locating holes, and No. one the locating hole is corresponding with No. two locating holes, and fixing bolt passes No. two locating holes in proper.
The adjustable plate is provided with a fixing plate, the inner side of the adjustable plate is connected with a clamping plate, the clamping plate is provided with a sliding block, the adjustable plate is provided with a sliding way, the sliding block is connected with the sliding way, the sliding block slides in the sliding way, the outer side of the adjustable plate is connected with a positioning plate, two sides of the positioning plate are provided with inserted rods, the adjustable plate is provided with a plurality of No. three positioning holes, the inserted rods are matched with No. three positioning holes, the inserted rods sequentially penetrate through No. three positioning holes and the sliding block to be connected with.
Has the advantages that:
the slide bar has supporting and positioning functions on the adjusting plate, the adjusting plate slides on the slide bar through the connecting plate to adjust the distance between the adjusting plates on two sides, so that the clamping requirements of the aerospace materials with different lengths during punching are met, the adjusting plate is matched with the four nuts through the fixing bolt to play a role in positioning and connecting, the adjusting plate after positioning is prevented from transversely shifting, the structure is stable and reasonable, the support plate supports the slide bar while playing a role in positioning and supporting the slide bar, space is reserved for the connecting plate to slide on the slide bar, friction between the connecting plate and the upper part of the back plate during sliding is avoided, the structure is reasonable, the clamping plate slides in the slide way through the slide block to adjust the distance between the clamping plate and the fixing plate, so that the clamping requirements of the aerospace materials with different thicknesses are met, the practicability is high, the inserted bar is matched with the three nuts, the positioning and connecting, strengthen its and adjusting plate between firm in connection nature, avoid it to take place to break away from, rational in infrastructure, fixed plate, splint and both sides adjusting plate cooperate, transversely and vertically carry out the centre gripping location to the space material, and the reinforcing is to the location nature of material, prevents to punch the in-process, and skew, drunkenness appear in the material, lead to phenomenons such as deviation, material waste, rational in infrastructure.
Drawings
Fig. 1 is the utility model discloses an aerospace puncher structure sketch map for material.
Fig. 2 is a side view of the structure of the hole-punching machine for aerospace material according to the present invention.
Fig. 3 is a partial enlarged view of the structure of the hole punching machine for aerospace materials.
Detailed Description
The invention is explained in more detail below with reference to the figures and examples:
a perforating machine for aerospace materials comprises a perforating machine body 01, a back plate 02, a bottom plate 03, a slide rod 04, an adjusting plate 05, a fixing plate 09, a clamping plate 10, a slide way 11, a positioning plate 13 and a screw rod 19, wherein the perforating machine body 01 is provided with the back plate 02, the lower part of the back plate 02 is connected with the bottom plate 03, the upper part of the back plate 02 is connected with a supporting plate 08, the screw rod 19 sequentially penetrates through the back plate 02 and the supporting plate 08, two ends of the screw rod 19 are connected with a first nut 20 through threads, the lower part of the adjusting plate 05 is connected with the bottom plate 03, the upper part of the adjusting plate 05 is provided with a connecting plate 17, the slide rod 04 sequentially penetrates through the supporting plate 08 and the connecting plate 17, two ends of the slide rod 04 are connected with a second nut 16 through threads, the slide rod 04 is provided with a plurality of first positioning holes 07, the connecting plate, the fixing bolt 06 is connected with the fourth nut 22 through threads.
The adjusting plate 05 is provided with a fixing plate 09, the inner side of the adjusting plate 05 is connected with a clamping plate 10, the clamping plate 10 is provided with a sliding block 14, the adjusting plate 05 is provided with a sliding way 11, the sliding block 14 is matched with the sliding way 11, the sliding block 14 is connected with the sliding way 11 and slides in the sliding way 11, the outer side of the adjusting plate 05 is connected with a positioning plate 13, two sides of the positioning plate 13 are provided with inserting rods 18, the adjusting plate 05 is provided with a plurality of No. three positioning holes 12, the inserting rods 18 are matched with No. three positioning holes 12, the inserting rods 18 sequentially penetrate through the No. three positioning holes 12, the sliding block 14.
The sliding rod 04 has a supporting and positioning effect on the adjusting plate 05, the adjusting plate 05 slides on the sliding rod 04 through the connecting plate 17, the distance between the adjusting plates 05 on two sides is adjusted, the clamping requirements during punching of aerospace materials with different lengths are met, the adjusting plate 05 is matched through the fixing bolt 06 and the fourth nut 22 to play a positioning and connecting effect, the adjusting plate 05 after positioning is prevented from moving transversely, the structure is stable and reasonable, the supporting plate 08 plays a positioning and supporting effect on the sliding rod 04 and supports the sliding rod 04 to reserve a space for the connecting plate 17 to slide on the sliding rod 04, friction between the connecting plate 17 and the upper part of the backboard 02 during sliding is avoided, the structure is reasonable, the clamping plate 10 slides in the slide way 11 through the sliding block 14 to adjust the distance between the clamping plate and the fixing plate 09, the clamping requirements for aerospace materials with different thicknesses are met, the practicability is high, the inserting rod 18 is matched with the third nut 15 to play, prevent that splint 10 from taking place the displacement drunkenness in, strengthen its and regulating plate 05 within a definite time fastness of being connected, avoid it to take place to break away from, rational in infrastructure, fixed plate 09, splint 10 and both sides regulating plate 05 cooperate, transversely reach vertically to the space material and carry out the centre gripping location, the reinforcing is to the location nature of material, prevents to punch the in-process, and skew, drunkenness appear in the material, lead to phenomenons such as the deviation of punching, material waste, rational in infrastructure.
Claims (2)
1. The perforating machine for aerospace materials is characterized by comprising a perforating machine body, a back plate, a bottom plate, a sliding rod, an adjusting plate, a fixing plate, a clamping plate, a slide way, a positioning plate and a screw rod, wherein the perforating machine body is provided with the back plate, the lower part of the back plate is connected with the bottom plate, the upper part of the back plate is connected with a supporting plate, the screw rod sequentially penetrates through the back plate and the supporting plate, the two ends of the back plate are connected with the supporting plate, the screw rod sequentially penetrates through the back plate and the supporting plate, the two ends of the sliding rod are connected with a second nut through threads, the sliding rod is provided with a plurality of first positioning holes, the connecting plate is provided with a second positioning hole, the first positioning hole corresponds.
2. The hole puncher as claimed in claim 1, wherein the adjusting plate is provided with a fixing plate, the inner side of the adjusting plate is connected with a clamping plate, the clamping plate is provided with a sliding block, the adjusting plate is provided with a sliding way, the sliding block is matched with the sliding way and is connected with the sliding way, the sliding block slides in the sliding way, the outer side of the adjusting plate is connected with a positioning plate, two sides of the positioning plate are provided with inserting rods, the adjusting plate is provided with a plurality of third positioning holes, the inserting rods are matched with the third positioning holes, the inserting rods sequentially penetrate through the third positioning holes, the sliding block is connected with third nuts, and.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920737025.8U CN209937061U (en) | 2019-05-22 | 2019-05-22 | Perforating machine for aerospace materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920737025.8U CN209937061U (en) | 2019-05-22 | 2019-05-22 | Perforating machine for aerospace materials |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209937061U true CN209937061U (en) | 2020-01-14 |
Family
ID=69133495
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920737025.8U Active CN209937061U (en) | 2019-05-22 | 2019-05-22 | Perforating machine for aerospace materials |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209937061U (en) |
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2019
- 2019-05-22 CN CN201920737025.8U patent/CN209937061U/en active Active
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