CN219777305U - Compressive strength detection device for aircraft plastic part - Google Patents
Compressive strength detection device for aircraft plastic part Download PDFInfo
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- CN219777305U CN219777305U CN202321192406.5U CN202321192406U CN219777305U CN 219777305 U CN219777305 U CN 219777305U CN 202321192406 U CN202321192406 U CN 202321192406U CN 219777305 U CN219777305 U CN 219777305U
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- mounting
- compressive strength
- electric sliding
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- plate
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- 229920003023 plastic Polymers 0.000 title claims abstract description 37
- 239000004033 plastic Substances 0.000 title claims abstract description 37
- 238000001514 detection method Methods 0.000 title claims abstract description 31
- 230000005540 biological transmission Effects 0.000 claims abstract description 14
- 238000009434 installation Methods 0.000 claims abstract description 11
- 238000003825 pressing Methods 0.000 claims abstract description 10
- 230000010354 integration Effects 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 6
- 230000006835 compression Effects 0.000 description 8
- 238000007906 compression Methods 0.000 description 8
- 239000012634 fragment Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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Abstract
The utility model discloses an airplane plastic part compressive strength detection device, which comprises: the mounting base is fixedly provided with a supporting plate at the outer side of the upper end of the mounting base through bolts, the inner side of the top of the supporting plate is provided with a mounting block, the outer side of the rear end of the mounting block is provided with a driving motor, and the output end of the driving motor is connected with a transmission rod positioned in the mounting block; the mounting plate is arranged on the inner side of the upper end of the supporting plate, an electric sliding rail is arranged on the outer side of the lower end of the mounting plate through a bolt, and an electric sliding block which is matched with the electric sliding rail is connected on the inner side of the electric sliding rail; the hydraulic cylinder is arranged on the outer side of the lower end of the electric sliding block, the outer side of the lower end of the hydraulic cylinder is connected with a pressurizing assembly, and the pressurizing assembly comprises a pressing block, an installation cylinder and a fixing bolt. This aircraft working of plastics compressive strength detection device conveniently carries out omnidirectional compressive strength to the aircraft working of plastics and detects work, has improved the effect of detection, has comparatively convenient dismouting function to the briquetting simultaneously, facilitates the use.
Description
Technical Field
The utility model relates to the technical field of compressive strength detection, in particular to a compressive strength detection device for an aircraft plastic part.
Background
The compressive strength detection is a detection process for qualitatively or quantitatively evaluating the compressive property of the aircraft plastic part, and the compressive property of the aircraft plastic part affects the running safety of the finished aircraft product, so that the compressive strength detection device is required to determine the pressure limit which can be born by the aircraft plastic part in the production process of the aircraft plastic part;
the utility model provides a chinese patent is authorized compression resistance detection device for auto plastic spare of publication number CN210401029U, includes the base, the standing groove has been seted up at the top of base, the top fixed mounting of base has the organism that is located the standing groove outside, the standing groove that is located the base inside has all been seted up to the inner chamber left and right sides wall of standing groove, two the mounting groove is all seted up to one side that the standing groove is on the back mutually is located the inside mounting groove of base, two the mounting groove is on the back mutually one side all fixed mounting has the mounting panel, two the equal fixed mounting of one side that the mounting panel is opposite has hydraulic push rod, two the one side fixed mounting that hydraulic push rod is opposite has one end to extend to the inside thrust piece of standing groove, the bottom fixed mounting of thrust piece has the sealing plug. This resistance to compression detection device for auto plastic spare, fragment are then promoted by the thrust piece after contacting with the thrust piece, and the final fragment drops in the collecting box from the clearance groove to the mesh that the fragment was convenient for clear up has been reached.
Most prior art solutions suffer from the following drawbacks: the detection position is fixed, the detection range is limited, the detection effect on the aircraft plastic part is easy to influence, and meanwhile, the pressing block is inconvenient to disassemble and assemble, so that the utility model provides the device for detecting the compressive strength of the aircraft plastic part, and the problems are solved.
Disclosure of Invention
The utility model aims to provide an airplane plastic part compressive strength detection device, which solves the problems that the detection position proposed in the background technology is fixed, the detection range is limited, the detection effect on the airplane plastic part is easily affected, and meanwhile, the pressing block is inconvenient to disassemble and assemble.
In order to achieve the above purpose, the present utility model provides the following technical solutions: an aircraft plastic compression strength detection device, comprising:
the mounting base is fixedly provided with a supporting plate at the outer side of the upper end of the mounting base through bolts, the inner side of the top of the supporting plate is provided with a mounting block, the outer side of the rear end of the mounting block is provided with a driving motor, and the output end of the driving motor is connected with a transmission rod positioned in the mounting block;
the mounting plate is arranged on the inner side of the upper end of the supporting plate, an electric sliding rail is arranged on the outer side of the lower end of the mounting plate through a bolt, and an electric sliding block which is matched with the electric sliding rail is connected on the inner side of the electric sliding rail;
the hydraulic cylinder is arranged at the outer side of the lower end of the electric sliding block, the outer side of the lower end of the hydraulic cylinder is connected with the pressurizing assembly, and the pressurizing assembly comprises a pressing block, a mounting cylinder and a fixing bolt;
the bottom plate, it sets up in the inboard lower extreme of backup pad, and the inboard fixed mounting of bottom plate has first spring, the limiting plate is installed in the one end outside that first spring is close to the bottom plate axis, the upper surface mid-mounting of installation base has pressure detector.
Preferably, the transmission rod is connected with the mounting block in a rotating mode, and the transmission rod is connected with the mounting plate in a threaded mode.
Preferably, the mounting blocks are arranged in one-to-one correspondence with the supporting plates and play a role in supporting and limiting the mounting plates.
Preferably, the upper end outside of briquetting integration fixed mounting has a mounting cylinder, and the both ends all run through and are provided with the fixing bolt that is used for fixed about the mounting cylinder.
Preferably, the mounting cylinder is connected with the hydraulic cylinder in an inserting manner, and a threaded hole structure matched with the fixing bolt is formed at the lower end of the hydraulic cylinder.
Preferably, the limiting plate and the bottom plate form a telescopic structure through the first spring, and the longitudinal section of the bottom plate is of a U-shaped structure.
Preferably, a second spring positioned on the mounting base is connected below the bottom plate.
Compared with the prior art, the utility model has the beneficial effects that: the compressive strength detection device for the airplane plastic part is convenient for carrying out omnibearing compressive strength detection work on the airplane plastic part, improves the detection effect, has a relatively convenient disassembly and assembly function on the pressing block, and is convenient to use;
1. the transmission rod is connected with the mounting block in a rotating mode, the transmission rod is connected with the mounting plate in a threaded mode, the transmission rod is convenient for driving the mounting plate to move forwards and backwards, and meanwhile, the electric sliding rail and the electric sliding block can drive the hydraulic cylinder to move left and right, so that the positions of the hydraulic cylinder and the pressurizing assembly are conveniently adjusted, the omnibearing compressive strength detection work of the aircraft plastic part is conveniently carried out, and the detection effect is improved;
2. the installation cylinder is connected with the hydraulic cylinder in an inserting manner, the lower end of the hydraulic cylinder is provided with a threaded hole structure matched with the fixing bolt, and the pressing block is conveniently and fixedly installed on the outer side of the lower end of the hydraulic cylinder through the fixing bolt, so that the pressing block has a convenient dismounting function and is convenient to use;
3. the limiting plate and the bottom plate form a telescopic structure under the action of the first spring, the longitudinal section of the bottom plate is of a U-shaped structure, and the limiting plate is contacted with the left side and the right side of the aircraft plastic part under the action of the first spring and plays a role in limiting and clamping the aircraft plastic part.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic diagram of the whole structure of the connection of the electric sliding rail and the electric sliding block;
FIG. 3 is a schematic view of the overall structure of the hydraulic cylinder and pressurization assembly connection of the present utility model;
FIG. 4 is an enlarged schematic view of the structure of FIG. 1A according to the present utility model;
FIG. 5 is a schematic view of the overall structure of the mounting base and the second spring connection of the present utility model.
In the figure: 1. a mounting base; 2. a support plate; 3. a mounting block; 4. a driving motor; 5. a transmission rod; 6. a mounting plate; 7. an electric slide rail; 8. an electric slide block; 9. a hydraulic cylinder; 10. a pressurizing assembly; 1001. briquetting; 1002. a mounting cylinder; 1003. a fixing bolt; 11. a bottom plate; 12. a first spring; 13. a limiting plate; 14. a second spring; 15. a pressure detector.
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. 1-5, the present utility model provides a technical solution: the utility model provides an aircraft working of plastics compressive strength detection device, including the upper end outside of installation base 1 has backup pad 2 through bolt fixed mounting, and the top inboard of backup pad 2 is provided with installation piece 3, driving motor 4 is installed in the rear end outside of installation piece 3, and driving motor 4's output is connected with the transfer line 5 that is located installation piece 3, mounting panel 6 sets up in the upper end inboard of backup pad 2, and the lower extreme outside of mounting panel 6 has electric slide rail 7 through the bolt mounting, electric slide rail 7's inboard is connected with the electric slider 8 of looks adaptation, pneumatic cylinder 9 installs in electric slide block 8's lower extreme outside, and pneumatic cylinder 9's lower extreme outside is connected with compression subassembly 10, and compression subassembly 10 includes briquetting 1001, installation cylinder 1002 and fixing bolt 1003, the upper end outside of briquetting 1001 is integrative fixed mounting has installation cylinder 1002, and the left and right sides of installation cylinder 1002 all runs through and is provided with the fixing bolt 1003 that is used for fixing, bottom plate 11 sets up in backup pad 2's inboard lower extreme simultaneously, and the inboard fixed mounting plate 11 has first spring 12, first spring 12 is close to the one end outside of bottom plate 11 installs limiting plate 13, the bottom plate 11 below the axis 11 is connected with compression strength detector 1 at the bottom plate 1, the second surface mounting device of aircraft base is installed to compression strength detector 1, the assembly is located the compression strength detector is installed to the aircraft base 15.
When the device for detecting the compressive strength of the plastic parts of the airplane is used, as shown in fig. 1 and 5, firstly, the mounting base 1 is stably placed on a designated plane, then the plastic parts of the airplane, which are required to be subjected to compressive strength detection, are placed in the middle of the upper end face of the bottom plate 11, and as shown in fig. 4, the limiting plate 13 and the bottom plate 11 form a telescopic structure through the first spring 12, and the longitudinal section of the bottom plate 11 is of a U-shaped structure, at the moment, the limiting plate 13 is contacted with the left side and the right side of the plastic parts of the airplane under the action of the first spring 12, and plays a role of limiting and clamping the plastic parts of the airplane, the hydraulic cylinder 9 is started again, so that the hydraulic cylinder 9 is extended, the pressurizing assembly 10 is driven to downwards move, the plastic parts of the airplane are pressurized, at the moment, the bottom plate 11 is pressurized and the second spring 14 and the damper are compressed downwards, so that the bottom plate 11 is contacted with the pressure detector 15, and the pressure detector 15 can transmit the received pressure data to the control panel and display;
specifically, as shown in fig. 1 and 2, since the transmission rod 5 is connected with the mounting block 3 in a rotating manner, and the transmission rod 5 is connected with the mounting plate 6 in a threaded manner, during detection, the driving motor 4 can be started to drive the transmission rod 5 to rotate, and at the moment, the transmission rod 5 is in threaded connection with the mounting plate 6, so that the mounting plate 6 is conveniently driven to move forwards and backwards, and meanwhile, the electric sliding rail 7 and the electric sliding block 8 can drive the hydraulic cylinder 9 to move left and right, so that the positions of the hydraulic cylinder 9 and the pressurizing assembly 10 are conveniently adjusted, the comprehensive compressive strength detection work of the aircraft plastic part is conveniently carried out, and the detection effect is improved;
as shown in fig. 3, the mounting cylinder 1002 is connected with the hydraulic cylinder 9 in a plugging manner, and the lower end of the hydraulic cylinder 9 is provided with a threaded hole structure matched with the fixing bolt 1003, when the pressing block 1001 is mounted, the mounting cylinder 1002 can be plugged and mounted on the outer side of the lower end of the hydraulic cylinder 9, and then the fixing bolt 1003 is sequentially rotated, so that the fixing bolt 1003 is in threaded connection with the mounting cylinder 1002 and the hydraulic cylinder 9 respectively through the threaded holes, and the pressing block 1001 is conveniently and fixedly mounted on the outer side of the lower end of the hydraulic cylinder 9, which is the use method of the device for detecting the compressive strength of the plastic part of the airplane.
Standard parts used in the utility model can be purchased from the market, special-shaped parts can be customized according to the description of the specification and the drawings, the specific connection modes of all parts adopt conventional means such as mature bolts, rivets and welding in the prior art, the machinery, the parts and the equipment adopt conventional modes in the prior art, and the circuit connection adopts conventional connection modes in the prior art, so that details are not described in detail in the specification, and the utility model belongs to the prior art known to the person skilled in the art.
Although the present utility model has been described with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements and changes may be made without departing from the spirit and principles of the present utility model.
Claims (7)
1. An aircraft plastic part compressive strength detection device, characterized by comprising:
the mounting base is fixedly provided with a supporting plate at the outer side of the upper end of the mounting base through bolts, the inner side of the top of the supporting plate is provided with a mounting block, the outer side of the rear end of the mounting block is provided with a driving motor, and the output end of the driving motor is connected with a transmission rod positioned in the mounting block;
the mounting plate is arranged on the inner side of the upper end of the supporting plate, an electric sliding rail is arranged on the outer side of the lower end of the mounting plate through a bolt, and an electric sliding block which is matched with the electric sliding rail is connected on the inner side of the electric sliding rail;
the hydraulic cylinder is arranged at the outer side of the lower end of the electric sliding block, the outer side of the lower end of the hydraulic cylinder is connected with the pressurizing assembly, and the pressurizing assembly comprises a pressing block, a mounting cylinder and a fixing bolt;
the bottom plate, it sets up in the inboard lower extreme of backup pad, and the inboard fixed mounting of bottom plate has first spring, the limiting plate is installed in the one end outside that first spring is close to the bottom plate axis, the upper surface mid-mounting of installation base has pressure detector.
2. The device for detecting the compressive strength of an aircraft plastic part according to claim 1, wherein: the transmission rod is connected with the mounting block in a rotating mode, and is connected with the mounting plate in a threaded mode.
3. The device for detecting the compressive strength of an aircraft plastic part according to claim 1, wherein: the mounting blocks are arranged in one-to-one correspondence with the supporting plates and play a role in supporting and limiting the mounting plates.
4. The device for detecting the compressive strength of an aircraft plastic part according to claim 1, wherein: the upper end outside integration fixed mounting of briquetting has a mounting cylinder, and the both ends all run through in the left and right sides of mounting cylinder and are provided with the fixing bolt that is used for fixed.
5. The device for detecting the compressive strength of an aircraft plastic according to claim 4, wherein: the mounting cylinder is connected with the hydraulic cylinder in an inserting mode, and a threaded hole structure matched with the fixing bolt is formed in the lower end of the hydraulic cylinder.
6. The device for detecting the compressive strength of an aircraft plastic part according to claim 1, wherein: the limiting plate and the bottom plate form a telescopic structure through the first spring, and the longitudinal section of the bottom plate is of a U-shaped structure.
7. The device for detecting the compressive strength of an aircraft plastic component according to claim 6, wherein: and a second spring positioned on the mounting base is connected below the bottom plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321192406.5U CN219777305U (en) | 2023-05-17 | 2023-05-17 | Compressive strength detection device for aircraft plastic part |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321192406.5U CN219777305U (en) | 2023-05-17 | 2023-05-17 | Compressive strength detection device for aircraft plastic part |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219777305U true CN219777305U (en) | 2023-09-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321192406.5U Active CN219777305U (en) | 2023-05-17 | 2023-05-17 | Compressive strength detection device for aircraft plastic part |
Country Status (1)
| Country | Link |
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| CN (1) | CN219777305U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117491133A (en) * | 2023-11-06 | 2024-02-02 | 金华市***化妆用品有限公司 | Pressure detection device for nail patch |
-
2023
- 2023-05-17 CN CN202321192406.5U patent/CN219777305U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117491133A (en) * | 2023-11-06 | 2024-02-02 | 金华市***化妆用品有限公司 | Pressure detection device for nail patch |
| CN117491133B (en) * | 2023-11-06 | 2024-04-05 | 金华市***化妆用品有限公司 | Pressure detection device for nail patch |
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