CN220912837U - Sparrow feather line fatigue test device - Google Patents
Sparrow feather line fatigue test device Download PDFInfo
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- CN220912837U CN220912837U CN202322685079.3U CN202322685079U CN220912837U CN 220912837 U CN220912837 U CN 220912837U CN 202322685079 U CN202322685079 U CN 202322685079U CN 220912837 U CN220912837 U CN 220912837U
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- sparrow
- disc
- test device
- fatigue test
- feather line
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- 241000287127 Passeridae Species 0.000 title claims abstract description 74
- 210000003746 feather Anatomy 0.000 title claims abstract description 70
- 238000009661 fatigue test Methods 0.000 title claims abstract description 21
- 238000002474 experimental method Methods 0.000 claims abstract description 34
- 238000001514 detection method Methods 0.000 abstract description 17
- 238000012545 processing Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 5
- 238000012360 testing method Methods 0.000 description 3
- 241000218202 Coptis Species 0.000 description 2
- 235000002991 Coptis groenlandica Nutrition 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 239000003086 colorant Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 241000692870 Inachis io Species 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
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- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The utility model discloses a fatigue test device for a sparrow feather line, and relates to the field of sparrow feather line processing. The sparrow feather line fatigue test device comprises an experiment platform, wherein a disc is arranged at the top of the experiment platform, a fixed rod is arranged at the top of the disc, a round rod is fixedly connected to the top of the disc, the fixed rod and the round rod are used for rotating and stretching the sparrow feather line, and a movable rod is arranged at the top of the experiment platform. This sparrow feather line fatigue test device, earlier with the tip centre gripping of sparrow feather line fixed respectively in the inside of movable rod and dead lever, when detecting shorter sparrow feather line, supplementary fixed plectane through the spliced pole, the drive of rethread electric telescopic handle, round trip movement movable rod can carry out fatigue detection to the sparrow feather line, when detecting longer sparrow feather line, through the drive of first motor, can make the disc rotate, the sparrow feather line can twine the lateral wall at the pole this moment, carries out tensile fatigue test, the accuracy of experiment has been promoted.
Description
Technical Field
The utility model relates to the technical field of sparrow feather line processing, in particular to a sparrow feather line fatigue test device.
Background
The sparrow feather thread is a kind of textile thread, and is a thread formed by processing yarns blended by sparrow feather and real silk and gold threads, and is used in embroidery technology because of various colors and gorgeous colors, peacock feather is twisted into feather threads in ancient times, and then the feather threads are kneaded into gold threads to weave embroidery which is resplendent.
When the current detection device detects the fatigue of the sparrow feather line, the length of the sparrow feather line cannot be adjusted, the middle part of the sparrow feather line is loosened due to overlong sparrow feather line, and the toughness detection effect of the sparrow feather line is inaccurate, so that secondary detection is needed, the practicability of equipment is reduced, the detection efficiency is affected, and aiming at the defects of the prior art, the fatigue test device for the sparrow feather line is provided for solving the problems.
Disclosure of utility model
(One) solving the technical problems
Aiming at the defects of the prior art, the utility model provides the fatigue test device for the sparrow feather line, which solves the problems that when the current detection device detects the fatigue of the sparrow feather line, the length of the sparrow feather line cannot be adjusted, the middle part of the sparrow feather line is loosened due to overlong sparrow feather line, and the toughness detection effect of the sparrow feather line is inaccurate, so that secondary detection is needed, and the practicability of equipment is reduced.
(II) technical scheme
In order to achieve the above purpose, the utility model is realized by the following technical scheme: sparrow feather line fatigue test device, including the experiment platform, the top of experiment platform is provided with the disc, the dead lever is installed at the top of disc, the top fixedly connected with round bar of disc, the dead lever is used for rotating tensile sparrow feather line with the round bar, the top of experiment platform is provided with the movable rod.
Preferably, the top of experiment platform runs through there is the montant, disc fixed connection is at the top of montant, the bottom of montant is provided with first motor, first motor installs the bottom at experiment platform.
Preferably, the bottom fixedly connected with bracing piece of disc, bracing piece sliding connection is at the top of experiment platform, the bracing piece is used for keeping the stability of disc.
Preferably, the spout has been seted up at the top of experiment platform, the bottom fixedly connected with slide bar of carriage release lever, slide bar sliding connection is in the inside of spout.
Preferably, the electric telescopic rod is installed in the experimental platform, the square block is installed on the side wall of the electric telescopic rod, the moving rod is installed at the top of the square block, and the electric telescopic rod is used for moving the moving rod.
Preferably, the top of movable rod is provided with the clamp mouth, the lateral wall fixedly connected with nut cap of movable rod, the lateral wall threaded connection of movable rod has the bolt, nut cap threaded connection is at the end side of bolt.
Preferably, the top of disc runs through there is the spliced pole, the top of experiment platform is provided with the circular slot, the spliced pole is pegged graft in the inside of circular slot, the periphery wall fixedly connected with plectrum of spliced pole, the top fixedly connected with spring of plectrum, the inside at the disc is installed to the spring.
Preferably, the top of plectane fixedly connected with circle piece, the top sliding connection of circle piece has the horizontal pole, the lateral wall of connecting rod is penetrated to the tip of horizontal pole.
The utility model discloses a sparrow feather line fatigue test device, which has the following beneficial effects: the end of the sparrow feather line is clamped and fixed in the moving rod and the fixing rod respectively, when the short sparrow feather line is detected, the circular plate is fixed in an auxiliary mode through the inserting rod, the moving rod is driven by the electric telescopic rod to move back and forth, fatigue detection can be conducted on the sparrow feather line, when the long sparrow feather line is detected, the circular plate can be rotated through driving of the first motor, at the moment, the sparrow feather line can be wound on the side wall of the round rod to conduct tensile fatigue experiments, the problems that an existing test device cannot be adjusted according to the length of the sparrow feather line, the middle portion is loosened due to overlong of the sparrow feather line, and the toughness detection effect on the sparrow feather line is inaccurate are solved.
Drawings
In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic structural diagram of an experimental platform of the present utility model;
FIG. 2 is a schematic view of a movable rod according to the present utility model;
FIG. 3 is a schematic cross-sectional view of the experimental platform of the present utility model;
fig. 4 is a schematic structural view of a plug rod according to the present utility model.
In the figure: 1. an experiment platform; 101. a chute; 102. a circular groove; 103. round blocks; 104. a cross bar; 2. a disc; 201. a fixed rod; 202. a round bar; 203. a vertical rod; 204. a first motor; 205. a support rod; 3. a moving rod; 301. a clamping opening; 302. a nut cap; 303. a bolt; 304. a slide bar; 5. an electric telescopic rod; 501. a square block; 6. inserting a connecting rod; 601. a circular plate; 602. and (3) a spring.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more clear, the technical solutions in the embodiments of the present utility model are clearly and completely described, and it is obvious that the described embodiments are 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.
According to the embodiment of the application, by providing the fatigue test device for the sparrow feather line, the problems that when the fatigue of the sparrow feather line is detected by the existing detection device, the fatigue cannot be adjusted according to the length of the sparrow feather line, so that the middle part of the sparrow feather line is loosened due to overlong, and the toughness detection effect on the sparrow feather line is inaccurate, so that secondary detection is needed, and the practicability of equipment is reduced are solved.
In order to better understand the above technical solutions, the following detailed description will refer to the accompanying drawings and specific embodiments.
The embodiment of the utility model discloses a sparrow feather line fatigue test device.
According to the shown in the attached drawings 1-4, the device for testing the fatigue of the sparrow feather line comprises an experiment platform 1, a disc 2 is arranged at the top of the experiment platform 1, a fixing rod 201 is arranged at the top of the disc 2, a round rod 202 is fixedly connected to the top of the disc 2, the fixing rod 201 and the round rod 202 are used for rotating and stretching the sparrow feather line, a movable rod 3 is arranged at the top of the experiment platform 1, and the disc 2 can be rotated again through clamping the sparrow feather line inside the fixing rod 201, so that the sparrow feather line can be stretched and detected.
The top of experiment platform 1 runs through there is montant 203, disc 2 fixed connection at the top of montant 203, and the bottom of montant 203 is provided with first motor 204, and first motor 204 installs the bottom at experiment platform 1, through the drive of first motor 204, can make disc 2 rotate, makes the sparrow feather line carry out tensile detection.
The bottom fixedly connected with bracing piece 205 of disc 2, bracing piece 205 sliding connection is at the top of experiment platform 1, and bracing piece 205 is used for keeping the stability of disc 2.
The spout 101 has been seted up at the top of experiment platform 1, and the bottom fixedly connected with slide bar 304 of movable rod 3, slide bar 304 sliding connection are in the inside of spout 101.
The internally mounted of experiment platform 1 has electric telescopic handle 5, and square 501 is installed to electric telescopic handle 5's lateral wall, and movable rod 3 installs at the top of square 501, and electric telescopic handle 5 is used for removing movable rod 3, through electric telescopic handle 5's drive, can round trip movement movable rod 3.
The top of movable rod 3 is provided with clamp 301, and the lateral wall fixedly connected with nut cap 302 of movable rod 3, and the lateral wall threaded connection of movable rod 3 has bolt 303, and nut cap 302 threaded connection is at the end side of bolt 303, with sparrow feather line centre gripping in the inside of clamp 301, again with bolt 303 threaded connection in the inside of nut cap 302, until fix the sparrow feather line.
The top of disc 2 runs through has peg graft pole 6, and experiment platform 1's top is provided with circular slot 102, and peg graft pole 6 peg graft in the inside of circular slot 102, and peg graft pole 6's periphery wall fixedly connected with plectrum 601, the top fixedly connected with spring 602 of plectrum 601, spring 602 installs in the inside of disc 2.
The top fixedly connected with circle piece 103 of plectane 601, the top sliding connection of circle piece 103 has horizontal pole 104, and the lateral wall of connecting rod 6 is penetrated to the tip of horizontal pole 104, through pressing down inserting rod 6, is pegged graft at the top of disc 2, and again with horizontal pole 104 penetrating the lateral wall of inserting rod 6, can assist fixed disc 2 this moment.
When the utility model is used, the end parts of the sparrow feather wires are respectively clamped and fixed in the moving rod 3 and the fixed rod 201, when the short sparrow feather wires are detected, the circular plate 601 is assisted and fixed through the inserting rod 6, then the moving rod 3 is driven by the electric telescopic rod 5 to move back and forth, fatigue detection can be carried out on the sparrow feather wires, when the long sparrow feather wires are detected, the circular plate 2 can be rotated through the driving of the first motor 204, and the sparrow feather wires can be wound on the side wall of the circular rod 202 at the moment, and a tensile fatigue experiment is carried out.
In summary, compared with the prior art, the method has the following beneficial effects: the end of the sparrow feather line is clamped and fixed in the moving rod 3 and the fixed rod 201 respectively, when the short sparrow feather line is detected, the circular plate 601 is fixed in an auxiliary mode through the inserting connection rod 6, the moving rod 3 is moved back and forth through the driving of the electric telescopic rod 5, fatigue detection can be conducted on the sparrow feather line, when the long sparrow feather line is detected, the disc 2 can be rotated through the driving of the first motor 204, the sparrow feather line can be wound on the side wall of the circular rod 202 at the moment to conduct a tensile fatigue experiment, the problem that an existing test device cannot be adjusted according to the length of the sparrow feather line, the middle portion is loosened due to overlong of the sparrow feather line, and the toughness detection effect on the sparrow feather line is inaccurate is solved.
The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (8)
1. Sparrow feather line fatigue test device, including experiment platform (1), its characterized in that, the top of experiment platform (1) is provided with disc (2), dead lever (201) are installed at the top of disc (2), the top fixedly connected with round bar (202) of disc (2), dead lever (201) are used for rotating tensile sparrow feather line with round bar (202), the top of experiment platform (1) is provided with movable rod (3).
2. The sparrow line fatigue test device according to claim 1, wherein: the top of experiment platform (1) runs through has montant (203), disc (2) fixed connection is at the top of montant (203), the bottom of montant (203) is provided with first motor (204), the bottom at experiment platform (1) is installed to first motor (204).
3. The sparrow line fatigue test device according to claim 1, wherein: the bottom fixedly connected with bracing piece (205) of disc (2), bracing piece (205) sliding connection is at the top of experiment platform (1), bracing piece (205) are used for keeping the stability of disc (2).
4. The sparrow line fatigue test device according to claim 1, wherein: the top of experiment platform (1) has seted up spout (101), the bottom fixedly connected with slide bar (304) of movable rod (3), slide bar (304) sliding connection is in the inside of spout (101).
5. The sparrow line fatigue test device according to claim 1, wherein: the inside of experiment platform (1) is installed electric telescopic handle (5), square (501) are installed to the lateral wall of electric telescopic handle (5), movable rod (3) are installed at the top of square (501), electric telescopic handle (5) are used for removing movable rod (3).
6. The sparrow line fatigue test device according to claim 5, wherein: the top of movable rod (3) is provided with double-layered mouth (301), the lateral wall fixedly connected with nut cap (302) of movable rod (3), the lateral wall threaded connection of movable rod (3) has bolt (303), nut cap (302) threaded connection is at the end side of bolt (303).
7. The sparrow line fatigue test device according to claim 1, wherein: the top of disc (2) is run through and is had spliced pole (6), the top of experiment platform (1) is provided with circular slot (102), spliced pole (6) are pegged graft in the inside of circular slot (102), the periphery wall fixedly connected with plectrum (601) of spliced pole (6), the top fixedly connected with spring (602) of plectrum (601), spring (602) are installed in the inside of disc (2).
8. The sparrow line fatigue test device according to claim 7, wherein: the top of plectane (601) fixedly connected with circle piece (103), the top sliding connection of circle piece (103) has horizontal pole (104), the lateral wall of connecting rod (6) is penetrated to the tip of horizontal pole (104).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322685079.3U CN220912837U (en) | 2023-10-08 | 2023-10-08 | Sparrow feather line fatigue test device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322685079.3U CN220912837U (en) | 2023-10-08 | 2023-10-08 | Sparrow feather line fatigue test device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220912837U true CN220912837U (en) | 2024-05-07 |
Family
ID=90908981
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322685079.3U Active CN220912837U (en) | 2023-10-08 | 2023-10-08 | Sparrow feather line fatigue test device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220912837U (en) |
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2023
- 2023-10-08 CN CN202322685079.3U patent/CN220912837U/en active Active
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