CN211518201U - Aerospace composite material fixing device for mould - Google Patents
Aerospace composite material fixing device for mould Download PDFInfo
- Publication number
- CN211518201U CN211518201U CN201922023152.4U CN201922023152U CN211518201U CN 211518201 U CN211518201 U CN 211518201U CN 201922023152 U CN201922023152 U CN 201922023152U CN 211518201 U CN211518201 U CN 211518201U
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- China
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- fixedly connected
- fixing device
- composite material
- base
- vertical plate
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Abstract
The utility model discloses a fixing device for aerospace combined material mould, including the base of fixed mounting on the workstation, left riser and right riser that two symmetries of upper end fixedly connected with of base set up, the lateral wall of left side riser and right riser all runs through and is equipped with the guiding hole, two run through the cover in the guiding hole and be equipped with the guide bar, the left mounting bracket of upper end fixedly connected with of guide bar, the right mounting bracket that the lateral wall fixedly connected with of right riser corresponds with left mounting bracket, right mounting bracket all is equipped with T shape slide, two with the corresponding face of left mounting bracket the corresponding splint that the equal fixedly connected with of corresponding lateral wall of T shape slider is corresponding, two be equipped with between the splint and step up the mechanism, two the T shape slider all locks through buckle mechanism. The utility model discloses, it can convenient and fast fixed to the mould to can make things convenient for the splint of quick change different models, effectively promote work efficiency.
Description
Technical Field
The utility model relates to an aerospace mould technical field that fixes especially relates to an aerospace is fixing device for combined material mould.
Background
Aviation refers to the navigation activity of an aircraft in the earth's atmosphere, and aerospace refers to the navigation activity of an aircraft in the space outside the atmosphere. Aerospace has greatly changed the structure of transportation.
The spare part of aerospace craft is of many kinds, so can use the mould of a large number of types when producing the spare part of aerospace craft to need fix the mould when reprocessing, but current mould fixing device when facing the mould of different models, the splint of change and mould matched with that can not be convenient influence the process progress of the spare part of aerospace craft.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the aerospace fixing device for combined material mould that proposes, it can convenient and fast fixed to the mould to can make things convenient for the splint of quick change different models, effectively promoted work efficiency.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an aerospace is fixing device for combined material mould, includes the base of fixed mounting on the workstation, left riser and the right riser that two symmetries of upper end fixedly connected with of base set up, the lateral wall of left side riser and right riser all runs through and is equipped with the guiding hole, two run through the cover in the guiding hole and be equipped with the guide bar, the left mounting bracket of upper end fixedly connected with of guide bar, the right mounting bracket that the lateral wall fixedly connected with of right side riser corresponds with left mounting bracket, the corresponding face of right side mounting bracket and left mounting bracket all is equipped with T shape slide, two all be equipped with T shape slider, two in the T shape slide the corresponding splint of the equal fixedly connected with of corresponding lateral wall of T shape slider, two be equipped with between the splint and step up the mechanism, two the T shape slider all locks through buckle mechanism.
Preferably, the tightening mechanism comprises a supporting plate fixedly connected to the right end of the guide rod, the supporting plate is elastically connected with the side wall of the left vertical plate through a return spring, the lower end of the guide rod is fixedly connected with a rack, the upper end of the base is provided with a cylindrical groove, a rotating shaft is rotatably connected between the axial side walls of the cylindrical groove, the outer wall of the rotating shaft is fixedly connected with a gear meshed with the rack, and one end of the rotating shaft extends to the front end face of the base and is fixedly connected with a handle.
Preferably, buckle mechanism is including setting up the through-hole in left side mounting bracket and right mounting bracket upper end, two the through-hole communicates with two T shape slides respectively, two all be equipped with the slide bar in the through-hole, two the equal fixedly connected with pull ring in upper end of slide bar, two through supporting tight spring elastic connection, two between pull ring and left mounting bracket and the right mounting bracket respectively the upper end of T shape slider be equipped with respectively with two slide bar complex locating holes.
Preferably, the guide bar has a rectangular cross section.
Preferably, the left side wall and the right side wall of the base are fixedly connected with housings sleeved at two ends of the guide rod.
Preferably, the end of the handle is inclined toward the return spring.
The utility model discloses in, its beneficial effect does:
1. the handle is pressed downwards to the mechanism that steps up that sets up, and the handle drives gear revolve through the pivot, and the gear passes through the rack and drives the elastic force that reset spring was overcome to the guide bar and move left, and the guide bar drives left mounting bracket and keeps away from right mounting bracket, then puts the mould in the centre of two splint, then the loose hand handle can be fixed the mould, easy operation, and fixed mould is convenient.
2. The buckle mechanism that sets up upwards stimulates the pull ring, and the pull ring drives the slide bar and overcomes the elastic force rebound that supports tight spring, when the end of slide bar breaks away from the locating hole, can take out the splint of changing different models with T shape slider, then loosens the pull ring, and the pull ring resets under the effect that supports tight spring and blocks owner once more with T shape slider, can accomplish the change of splint, changes convenient and fast, has promoted work efficiency.
Drawings
Fig. 1 is a schematic structural view of a fixing device for an aerospace composite material mold according to the present invention;
fig. 2 is a schematic cross-sectional structural view of a fixing device for an aerospace composite material mold according to the present invention;
fig. 3 is the utility model provides an enlarged structure schematic diagram of a department of aerospace composite material fixing device for mould.
In the figure: the device comprises a base 1, a left vertical plate 2, a right vertical plate 3, a guide hole 4, a guide rod 5, a left mounting frame 6, a right mounting frame 7, a slide way 8T-shaped, a slide block 9T-shaped, a clamping plate 10, a cylindrical groove 11, a rotating shaft 12, a gear 13, a rack 14, a handle 15, a pressing plate 16, a return spring 17, a through hole 18, a slide rod 19, a pull ring 20, a pressing spring 21, a positioning hole 22 and a housing 23.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1-3, a fixing device for an aerospace composite material mold comprises a base 1 fixedly installed on a workbench, the upper end of the base 1 is fixedly connected with two left vertical plates 2 and right vertical plates 3 which are symmetrically arranged, the side walls of the left vertical plates 2 and the right vertical plates 3 are both provided with guide holes 4 in a penetrating manner, guide rods 5 are sleeved in the two guide holes 4 in a penetrating manner, the cross sections of the guide rods 5 are rectangular, the left side wall and the right side wall of the base 1 are both fixedly connected with a housing 23 which is sleeved at the two ends of the guide rods 5, the housing 23 plays a role of protection, the upper end of the guide rod 5 is fixedly connected with a left mounting frame 6, the side wall of the right vertical plate 3 is fixedly connected with a right mounting frame 7 corresponding to the left mounting frame 6, the corresponding surfaces of the right mounting frame 7 and the left mounting frame 6 are both provided with T-shaped slide ways 8, the two T-shaped slide ways 8 are, a clamping mechanism is arranged between the two clamping plates 10, the clamping mechanism comprises a supporting plate 16 fixedly connected at the right end of the guide rod 5, the supporting plate 16 is elastically connected with the side wall of the left vertical plate 2 through a reset spring 17, the lower end of the guide rod 5 is fixedly connected with a rack 14, the upper end of the base 1 is provided with a cylindrical groove 11, a rotating shaft 12 is rotatably connected between the axial side walls of the cylindrical groove 11, the outer wall of the rotating shaft 12 is fixedly connected with a gear 13 meshed with the rack 14, one end of the rotating shaft 12 extends to the front end face of the base 1 and is fixedly connected with a handle 15, the tail end of the handle 15 is obliquely arranged towards the direction of the reset spring 17, the handle 15 is pressed downwards, the handle 15 drives the gear 13 to rotate through the rotating shaft 12, the gear 13 drives the guide rod 5 to move leftwards by overcoming the elastic force of the reset spring 17 through the rack 14, the guide rod 5 drives the, then the handle 15 is loosened to fix the mould, the operation is simple, and the mould is convenient to fix.
The two T-shaped sliding blocks 9 are locked through a buckling mechanism, the buckling mechanism comprises through holes 18 arranged at the upper ends of a left mounting frame 6 and a right mounting frame 7, the two through holes 18 are respectively communicated with the two T-shaped slideways 8, sliding rods 19 are respectively arranged in the two through holes 18, pull rings 20 are respectively fixedly connected at the upper ends of the two sliding rods 19, the two pull rings 20 are respectively and elastically connected with the left mounting frame 6 and the right mounting frame 7 through abutting springs 21, positioning holes 22 matched with the two sliding rods 19 are respectively arranged at the upper ends of the two T-shaped sliding blocks 9, the pull rings 20 are pulled upwards, the pull rings 20 drive the sliding rods 19 to overcome the elastic force of the abutting springs 21 to move upwards, when the tail ends of the sliding rods 19 are separated from the positioning holes 22, the T-shaped sliding blocks 9 can be taken out to replace clamping plates 10 with different types, then the pull rings 20 are loosened, the pull rings 20 reset under, the replacement of the clamping plate 10 can be completed, the replacement is convenient and fast, and the working efficiency is improved.
In the utility model, when the mold needs to be fixed, the handle 15 is pressed downwards, the handle 15 drives the rotating shaft 12 to rotate, the rotating shaft 12 drives the gear 13 to rotate, the gear 13 rotates to make the rack 14 move leftwards, the rack 14 drives the guide rod 5 to overcome the elastic force of the reset spring 17 to move leftwards, the guide rod 5 drives the left mounting frame 6 to be away from the right mounting frame 7, then the mold is placed between the two clamp plates 10, then the handle 15 is loosened, the guide rod 5 resets under the action of the reset spring 17, the guide rod 5 drives the left mounting frame 6 to reset towards the right mounting frame 7, thereby fixing the mold between the two clamp plates 10, the operation is simple, the mold is convenient to fix, when the clamp plates 10 need to be replaced, the pull ring 20 is pulled upwards, the pull ring 20 drives the slide rod 19 to overcome the elastic force of the press spring 21 to move upwards, when the tail end of the slide rod, can take T shape slider 9 out from 8 ends of T shape slide, then change splint 10 of different models and loose hand with pull ring 20, pull ring 20 resets under the effect of supporting tight spring 21 and blocks owner once more with T shape slider 9, can accomplish the change of splint 10, changes convenient and fast, has promoted work efficiency.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. A fixing device for an aerospace composite material die comprises a base (1) fixedly installed on a workbench, and is characterized in that the upper end of the base (1) is fixedly connected with a left vertical plate (2) and a right vertical plate (3) which are symmetrically arranged, the side walls of the left vertical plate (2) and the right vertical plate (3) are respectively provided with a guide hole (4) in a penetrating manner, a guide rod (5) is sleeved in the two guide holes (4) in a penetrating manner, the upper end of the guide rod (5) is fixedly connected with a left installing frame (6), the side wall of the right vertical plate (3) is fixedly connected with a right installing frame (7) corresponding to the left installing frame (6), T-shaped slide ways (8) are respectively arranged on the corresponding surfaces of the right installing frame (7) and the left installing frame (6), T-shaped slide blocks (9) are respectively arranged in the two T-shaped slide ways (8), and corresponding side walls of the two T-shaped slide blocks (9) are respectively fixedly, and a clamping mechanism is arranged between the two clamping plates (10), and the two T-shaped sliding blocks (9) are locked through a buckle mechanism.
2. The aerospace composite material fixing device for the mold according to claim 1, wherein the clamping mechanism comprises a supporting plate (16) fixedly connected to the right end of the guide rod (5), the supporting plate (16) is elastically connected with the side wall of the left vertical plate (2) through a return spring (17), a rack (14) is fixedly connected to the lower end of the guide rod (5), a cylindrical groove (11) is formed in the upper end of the base (1), a rotating shaft (12) is rotatably connected between the axial side walls of the cylindrical groove (11), a gear (13) meshed with the rack (14) is fixedly connected to the outer wall of the rotating shaft (12), and a handle (15) is fixedly connected to one end of the rotating shaft (12) and extends to the front end face of the base (1).
3. The aerospace composite material fixing device for the mold according to claim 1, wherein the buckling mechanism comprises through holes (18) formed in upper ends of a left mounting frame (6) and a right mounting frame (7), the through holes (18) are respectively communicated with two T-shaped slide ways (8), a slide rod (19) and a pull ring (20) are fixedly connected to the upper ends of the slide rod (19), the pull rings (20) are respectively and elastically connected with the left mounting frame (6) and the right mounting frame (7) through abutting springs (21), and positioning holes (22) matched with the two slide rods (19) are respectively formed in the upper ends of the T-shaped sliding blocks (9).
4. An aerospace composite mould fixture device according to claim 1, wherein the guide bar (5) is rectangular in cross-section.
5. The fixing device for the aerospace composite material mold according to claim 1, wherein the left and right side walls of the base (1) are fixedly connected with covers (23) which are sleeved at two ends of the guide rod (5).
6. An aerospace composite material mould fixture device according to claim 2, wherein the end of the handle (15) is inclined towards the return spring (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922023152.4U CN211518201U (en) | 2019-11-21 | 2019-11-21 | Aerospace composite material fixing device for mould |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922023152.4U CN211518201U (en) | 2019-11-21 | 2019-11-21 | Aerospace composite material fixing device for mould |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211518201U true CN211518201U (en) | 2020-09-18 |
Family
ID=72463563
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922023152.4U Expired - Fee Related CN211518201U (en) | 2019-11-21 | 2019-11-21 | Aerospace composite material fixing device for mould |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211518201U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116572473A (en) * | 2023-06-01 | 2023-08-11 | 浙江锦富隆包装有限公司 | One-step injection molding equipment for special-shaped food packaging cup |
-
2019
- 2019-11-21 CN CN201922023152.4U patent/CN211518201U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116572473A (en) * | 2023-06-01 | 2023-08-11 | 浙江锦富隆包装有限公司 | One-step injection molding equipment for special-shaped food packaging cup |
| CN116572473B (en) * | 2023-06-01 | 2023-12-12 | 浙江锦富隆包装有限公司 | One-step injection molding equipment for special-shaped food packaging cup |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200918 Termination date: 20201121 |
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| CF01 | Termination of patent right due to non-payment of annual fee |