CN220481632U - Aerospace material processing fixing device - Google Patents
Aerospace material processing fixing device Download PDFInfo
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- CN220481632U CN220481632U CN202322241953.4U CN202322241953U CN220481632U CN 220481632 U CN220481632 U CN 220481632U CN 202322241953 U CN202322241953 U CN 202322241953U CN 220481632 U CN220481632 U CN 220481632U
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- 239000011825 aerospace material Substances 0.000 title claims abstract description 46
- 238000009434 installation Methods 0.000 claims description 15
- 244000309464 bull Species 0.000 claims description 6
- 238000003754 machining Methods 0.000 claims description 5
- 230000000694 effects Effects 0.000 abstract description 3
- 239000000463 material Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000003044 adaptive effect Effects 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses an aerospace material processing and fixing device which comprises a processing and fixing device main body, wherein a workbench is fixedly arranged on the upper end face of the processing and fixing device main body, two fixing slide bars are arranged in the workbench, and two connecting sliding seats are connected to two sides of the outer surface of each of the two fixing slide bars in a sliding manner. The device structure drives rubber splint and arc splint through the rotation of fixed plate and changes the position in proper order, lets rubber splint and arc splint can adapt to the aerospace material of different shapes respectively, can adjust fixed mode according to the aerospace material of different shapes like this, improves the application scope when processing fixing device is fixed, drives bottom plate department through electric putter's extension and is connected with reset spring's rubber seat and moves down, lets the rubber seat can freely adjust the height and fix a position the top of aerospace material like this to further improve the fixed effect of processing fixing device.
Description
Technical Field
The utility model relates to the technical field of aerospace material processing, in particular to an aerospace material processing fixing device.
Background
The aerospace material is one of the decisive factors for the development of aerospace engineering technology, has excellent high and low temperature resistance, ageing resistance and corrosion resistance, can adapt to space environment, and is required to be processed in order to meet different engineering requirements;
in the use process of the existing aerospace material processing and fixing device, solid clamping blocks are used for fixing materials, the materials are easily damaged due to overlarge force in the fixing process, and the quality of the materials is affected;
the prior patent (publication number: CN 213411730U) is an aerospace material processing and fixing device, and the aerospace material processing and fixing device can adjust the distance between the first fixing piece and the second fixing piece by sliding the second fixing piece so as to clamp aerospace materials to be processed, so that the operation is convenient; and the arrangement of the spring can effectively reduce the abrasion to aerospace materials in the fixing process, and the fixing column used for limiting can effectively avoid the spring losing elasticity due to the fact that the spring is compressed infinitely for a long time.
The aerospace material processing and fixing device can only prevent the materials from being damaged due to overlarge strength, and in the actual use process, most of the processing and fixing device can only be used for fixing aerospace materials in a square state, if the aerospace materials in a cylindrical state are required to be fixed, the processing and fixing device cannot well clamp and fix the aerospace materials, so that the aerospace materials can easily slide and are separated from the processing and fixing device, and the use of the processing and fixing device is not facilitated.
For this purpose, an aerospace material processing and fixing device is proposed.
Disclosure of Invention
The utility model aims to solve the technical problem of providing an aerospace material processing and fixing device which can solve the problem that only square aerospace materials can be matched for fixing.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an aerospace material processing fixing device, including processing fixing device main part, processing fixing device main part's up end fixed mounting has the workstation, the internally mounted of workstation has two fixed slide bars, the surface both sides of two fixed slide bars all sliding connection has a connection slide, the up end of two connection slide all rotates and is connected with a rotation axis, the up end of two rotation axes all fixed mounting has a fixed plate, the left and right sides of two fixed plates all sliding connection has four telescopic columns, the right-hand member face fixedly connected with first mounting box of four telescopic columns, the up end slip joint of first mounting box has first embedded block, rubber splint are installed to the right-hand member face of first embedded block;
the left end face fixed connection second mounting box of four flexible posts, the up end slip joint of second mounting box has the second embedded block, and arc splint are installed to the left end face of second embedded block, are connected with two first connecting springs between two connection slides and the processing fixing device main part.
Preferably, four support plates are fixedly installed around the upper end face of the machining and fixing device main body, the inner side face of each support plate is connected with a U-shaped top plate, the inner side face of each U-shaped top plate is rotationally connected with a bolt rotating rod, the outer surface of each bolt rotating rod is in spiral transmission with a mounting block, the inner side face of each U-shaped top plate is connected with two round rods, and the lower end face of each mounting block is provided with an electric push rod.
Preferably, the servo motor is fixedly arranged on the left end face of the bolt rotating rod, the lower end face of the electric push rod is connected with the bottom plate, the lower end face of the bottom plate is connected with the reset spring, and the rubber seat is arranged on the lower end face of the reset spring.
Preferably, one side of the bolt rotating rod penetrates through the U-shaped top plate and extends to the left end face of the U-shaped top plate, and the two round rods are mutually parallel.
Preferably, one side of the first connecting spring is connected to the outer side of the fixing plate, the other side of the first connecting spring is connected to the inner side of the machining fixing device main body, a side plate is mounted on the front side and the rear side of the two fixing plates, the upper end faces of the four side plates are slidably clamped with a positioning bolt, and one side of the positioning bolt penetrates through the side plate and extends to the upper end face of the connecting sliding seat.
Preferably, four second connecting springs are connected between the fixing plate and the first mounting box, one side of each second connecting spring is connected to the right end face of the fixing plate, and the other side of each second connecting spring is connected to the left end face of the first mounting box.
Preferably, four third connecting springs are connected between the fixing plate and the second mounting box, one side of each third connecting spring is connected to the left end face of the fixing plate, and the other side of each third connecting spring is connected to the right end face of the second mounting box.
Preferably, the left and right sides of the installation block are provided with transversely-through sliding grooves, the transversely-through sliding grooves are matched with the round rods, and the outer surfaces of the round rods are in sliding connection with the left and right sides of the installation block through the transversely-through sliding grooves.
Compared with the prior art, the utility model has the beneficial effects that:
1. the rubber clamping plate and the arc clamping plate are driven to sequentially change positions through rotation of the fixing plate, so that the rubber clamping plate and the arc clamping plate can be respectively matched with aerospace materials in different shapes, the fixing mode can be adjusted according to the aerospace materials in different shapes, and the application range of fixing the processing fixing device is improved;
2. the rubber seat connected with the reset spring at the bottom plate is driven to move downwards through the extension of the electric push rod, so that the rubber seat can be freely adjusted in height to position the upper part of the aerospace material, and the fixing effect of the processing fixing device is further improved.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions in the prior art, the drawings that are needed in the description of the embodiments or the prior art will be briefly described, and it is obvious that the drawings in the description below are some embodiments of the present utility model, and other drawings can be obtained according to the drawings without inventive effort for a person skilled in the art.
FIG. 1 is an overall structural view of the present utility model;
FIG. 2 is a schematic view of the structure of the fixed slide bar, the connecting slide and the first connecting spring according to the present utility model;
FIG. 3 is a schematic view of the rubber clamping plate and the arc clamping plate of the present utility model;
fig. 4 is a schematic installation view of the return spring and the rubber seat of the present utility model.
Reference numerals illustrate:
1. machining a fixing device main body; 2. a work table; 3. fixing the slide bar; 4. the connecting slide seat; 5. a rotation shaft; 6. a fixing plate; 7. a telescopic column; 8. a first mounting box; 9. a first embedded block; 10. a rubber clamping plate; 11. a second mounting box; 12. a second embedded block; 13. an arc clamping plate; 14. a second connecting spring; 15. a third connecting spring; 16. a side plate; 17. positioning a bolt; 18. a support plate; 19. a U-shaped top plate; 20. a bolt rotating rod; 21. a servo motor; 22. a round bar; 23. a mounting block; 24. an electric push rod; 25. a bottom plate; 26. a return spring; 27. a rubber seat; 28. a chute; 29. and a first connecting spring.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1 to 4, the present utility model provides a technical solution:
the utility model provides an aerospace material processing fixing device, including processing fixing device main part 1, processing fixing device main part 1's up end fixed mounting has workstation 2, the internally mounted of workstation 2 has two fixed slide bars 3, the surface both sides of the fixed slide bar 3 of two fixed slide bars 3 all sliding connection has a connection slide 4, the up end of two connection slide 4 all rotates and is connected with a rotation axis 5, the up end of two rotation axes 5 all fixed mounting has a fixed plate 6, through the rotation of rotation axis 5 and fixed plate 6, utilize pivoted rotation axis 5 to drive fixed plate 6 rotation regulation, so can change different fixed modes, the right and left sides of two fixed plates 6 all sliding connection has four telescopic column 7, the right-hand member face fixedly connected with first mounting box 8 of four telescopic column 7, the up end sliding joint of first mounting box 8 has first embedded block 9, the right-hand member face of first embedded block 9 installs rubber splint 10;
the left end face fixed connection second mounting box 11 of four flexible posts 7, the up end slip joint of second mounting box 11 has second embedded block 12, and arc splint 13 is installed to the left end face of second embedded block 12, is connected with two first connecting springs 29 between two connection slide 4 and the processing fixing device main part 1.
Four backup pads 18 are fixedly installed around the up end of processing fixing device main part 1, the medial surface of backup pad 18 is connected with U type roof 19, the medial surface of U type roof 19 rotates and is connected with bolt bull stick 20, the surface screw drive of bolt bull stick 20 has installation piece 23, through the installation use of bolt bull stick 20 and installation piece 23, along with the rotation of bolt bull stick 20 drive installation piece 23 remove, the convenience is fixed in a flexible way to the different positions of aerospace material top like this, the medial surface of U type roof 19 is connected with two round bars 22, electric putter 24 is installed to the lower terminal surface of installation piece 23.
The servo motor 21 is fixedly arranged on the left end face of the bolt rotating rod 20, the bottom face of the electric push rod 24 is connected with the bottom plate 25, the lower end face of the bottom plate 25 is connected with the reset spring 26, the rubber seat 27 is arranged on the lower end face of the reset spring 26, the rubber seat 27 is installed and used through the reset spring 26 and the rubber seat 27, the aerospace material can be clamped and fixed in an adaptive mode through the elasticity of the reset spring 26, and the stability of the aerospace material is further improved.
One side of the bolt rotating rod 20 penetrates through the U-shaped top plate 19 and extends to the left end face of the U-shaped top plate 19, and two round rods 22 are mutually parallel.
One side of the first connecting spring 29 is connected to the outer side of the fixed plate 6, the other side of the first connecting spring 29 is connected to the inside of the machining fixing device main body 1, a side plate 16 is mounted on the front side and the rear side of the two fixed plates 6, the upper end faces of the four side plates 16 are slidably clamped with a positioning bolt 17, and one side of the positioning bolt 17 penetrates through the side plate 16 and extends to the upper end face of the connecting sliding seat 4.
Four second connecting springs 14 are connected between the fixed plate 6 and the first mounting box 8, one side of each second connecting spring 14 is connected to the right end face of the fixed plate 6, and the other side of each second connecting spring 14 is connected to the left end face of the first mounting box 8.
Four third connecting springs 15 are connected between the fixed plate 6 and the second mounting box 11, the telescopic columns 7 at the two mounting boxes can be telescopically adjusted by using the elastic force of the second connecting springs 14 and the third connecting springs 15 through the installation and use of the telescopic columns 7, the second connecting springs 14 and the third connecting springs 15, the clamping force is weakened by using the elastic deformation of the two connecting springs so as to better protect aerospace materials, one side of the third connecting springs 15 is connected to the left end face of the fixed plate 6, and the other side of the third connecting springs 15 is connected to the right end face of the second mounting box 11.
The left and right sides of the installation block 23 are provided with transversely-through sliding grooves 28, the transversely-through sliding grooves 28 are matched with the round rod 22, and the outer surface of the round rod 22 is in sliding connection with the left and right sides of the installation block 23 through the transversely-through sliding grooves 28.
Working principle: when the aerospace material processing fixing device is used, two first embedded blocks 9 are respectively inserted into two first mounting boxes 8, the two first embedded blocks 9 drive rubber clamping plates 10 to be clamped and fixed, then aerospace materials in a square state are placed into the two rubber clamping plates 10, at the moment, the aerospace materials can simultaneously extrude two connecting sliding seats 4 and fixing plates 6 connected with first connecting springs 29, the two connecting sliding seats 4 can slide on two fixing sliding rods 3, the two rubber clamping plates 10 can be clamped and fixed by utilizing the elasticity of the first connecting springs 29 in an adaptive manner to square aerospace materials in different specifications, then the two fixing plates 6 are driven to rotate by utilizing a rotating shaft 5, the other surfaces of the two fixing plates 6 are rotated to the inner sides, the two fixing plates 6 are fixed by utilizing positioning bolts 17, and then a second embedded block 12 at an arc clamping plate 13 is inserted into the second mounting boxes 11, so that the aerospace materials in a cylindrical state can be placed into the two arc clamping plates 13, the cylindrical aerospace materials can also extrude the connecting plates 4 and the fixing plates 6 in the cylindrical state, and the two fixing plates 29 can be clamped and fixed by utilizing the elasticity of the first connecting springs 29 in the same specification, and the arc clamping plates can be fixed by utilizing the elasticity of the same specifications, and the two fixing devices can be fixed by adopting different clamping manners;
by starting the servo motor 21, the output shaft of the servo motor 21 drives the bolt rotating rod 20 to rotate, the mounting block 23 on the bolt rotating rod 20 can be moved and adjusted left and right, then the electric push rod 24 is started, the electric push rod 24 stretches downwards to drive the rubber seat 27 connected with the reset spring 26 at the bottom plate 25 to move downwards, and thus the rubber seat 27 can be freely adjusted in height to position the upper part of the aerospace material, so that the fixing effect of the processing fixing device is further improved.
Finally, it should be noted that: the above embodiments are only for illustrating the technical solution of the present utility model, and not for limiting the same; although the utility model has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some or all of the technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit of the utility model.
Claims (8)
1. Aerospace material processing fixing device, including processing fixing device main part (1), its characterized in that: the processing fixing device comprises a processing fixing device body (1), wherein a workbench (2) is fixedly arranged on the upper end face of the processing fixing device body (1), two fixing slide bars (3) are arranged in the workbench (2), two connecting sliding seats (4) are slidably connected to two sides of the outer surface of each fixing slide bar (3), a rotating shaft (5) is rotatably connected to the upper end faces of the two connecting sliding seats (4), a fixing plate (6) is fixedly arranged on the upper end faces of the two rotating shafts (5), four telescopic columns (7) are slidably connected to the left side and the right side of the fixing plate (6), a first mounting box (8) is fixedly connected to the right end faces of the four telescopic columns (7), a first embedded block (9) is slidably clamped to the upper end faces of the first mounting boxes (8), and a rubber clamping plate (10) is arranged on the right end faces of the first embedded blocks (9).
The four left end face fixed connection second mounting box (11) of flexible post (7), the up end slip joint of second mounting box (11) has second embedded block (12), arc splint (13) are installed to the left end face of second embedded block (12), two be connected with two first connecting spring (29) between connection slide (4) and processing fixing device main part (1).
2. An aerospace material processing fixture according to claim 1, wherein: four backup pads (18) are fixed mounting all around to the up end of processing fixing device main part (1), the medial surface of backup pad (18) is connected with U type roof (19), the medial surface of U type roof (19) rotates and is connected with bolt bull stick (20), the surface screw drive of bolt bull stick (20) has installation piece (23), the medial surface of U type roof (19) is connected with two round bars (22), electric putter (24) are installed to the lower terminal surface of installation piece (23).
3. An aerospace material processing fixture according to claim 2, wherein: the left end face of the bolt rotating rod (20) is fixedly provided with a servo motor (21), the lower end face of the electric push rod (24) is connected with a bottom plate (25), the lower end face of the bottom plate (25) is connected with a return spring (26), and the lower end face of the return spring (26) is provided with a rubber seat (27).
4. An aerospace material processing fixture according to claim 2, wherein: one side of the bolt rotating rod (20) penetrates through the U-shaped top plate (19) and extends to the left end face of the U-shaped top plate (19), and two round rods (22) are mutually parallel.
5. An aerospace material processing fixture according to claim 1, wherein: one side of the first connecting spring (29) is connected to the outer side of the fixed plate (6), the other side of the first connecting spring (29) is connected to the inside of the machining fixing device main body (1), two side plates (16) are mounted on the front side and the rear side of the fixed plate (6), four upper end faces of the side plates (16) are slidably clamped with a positioning bolt (17), and one side of the positioning bolt (17) penetrates through the side plates (16) and extends to the upper end face of the connecting sliding seat (4).
6. An aerospace material processing fixture according to claim 1, wherein: four second connecting springs (14) are connected between the fixed plate (6) and the first mounting box (8), one side of each second connecting spring (14) is connected to the right end face of the fixed plate (6), and the other side of each second connecting spring (14) is connected to the left end face of the first mounting box (8).
7. An aerospace material processing fixture according to claim 1, wherein: four third connecting springs (15) are connected between the fixed plate (6) and the second mounting box (11), one side of each third connecting spring (15) is connected to the left end face of the fixed plate (6), and the other side of each third connecting spring (15) is connected to the right end face of the second mounting box (11).
8. An aerospace material processing fixture according to claim 2, wherein: the left side and the right side of the installation block (23) are provided with transversely-through sliding grooves (28), the transversely-through sliding grooves (28) are matched with the round rods (22), and the outer surfaces of the round rods (22) are in sliding connection with the left side and the right side of the installation block (23) through the transversely-through sliding grooves (28).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322241953.4U CN220481632U (en) | 2023-08-21 | 2023-08-21 | Aerospace material processing fixing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322241953.4U CN220481632U (en) | 2023-08-21 | 2023-08-21 | Aerospace material processing fixing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220481632U true CN220481632U (en) | 2024-02-13 |
Family
ID=89826164
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322241953.4U Active CN220481632U (en) | 2023-08-21 | 2023-08-21 | Aerospace material processing fixing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220481632U (en) |
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2023
- 2023-08-21 CN CN202322241953.4U patent/CN220481632U/en active Active
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