CN214426879U - Novel slider formula tension tester for aviation cable wire - Google Patents
Novel slider formula tension tester for aviation cable wire Download PDFInfo
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- CN214426879U CN214426879U CN202120421621.2U CN202120421621U CN214426879U CN 214426879 U CN214426879 U CN 214426879U CN 202120421621 U CN202120421621 U CN 202120421621U CN 214426879 U CN214426879 U CN 214426879U
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- sensor
- handle
- tension tester
- slide rail
- novel slider
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Abstract
The utility model discloses a novel slider formula tension tester for aviation cable wire belongs to tension tester technical field, including the bracing piece, the one end of bracing piece is connected with the slide rail, and sliding connection has the sensor on the slide rail, and the top of slide rail is connected with the kicking block corresponding with the sensor, and the other end of bracing piece is connected with the handle, is connected with the stay cord on the handle, and the other end and the sensor of stay cord are connected, still are connected through reset spring between sensor and the slide rail. The utility model discloses with the sensor setting on the slide rail, drive the sensor action through the stay cord to test the tension of cable wire with the kicking block cooperation, have small in size, measurement accuracy height and be applicable to the characteristics that multiple occasion was used.
Description
Technical Field
The utility model belongs to the technical field of tension tester, concretely relates to novel slider formula tension tester for aviation cable wire.
Background
The current aviation steel cable tension tester has the following problems: 1. the volume is too large, the precision is not enough after the volume is small, and the measurement requirement cannot be met. After the volume is large, the utility model can not be used in narrow space. 2. The measuring chuck is rigidly connected with the operating mechanism, and cannot meet the measuring requirements of a deep closed space, such as a steel cable crossing in a small hole.
SUMMERY OF THE UTILITY MODEL
To solve the problems set forth in the background art described above. The utility model provides a novel slider formula tension tester for air wire rope has small in size, measurement accuracy height and is applicable to the characteristics that multiple occasion was used.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a novel slider formula tension tester for aviation cable wire, includes the bracing piece, and the one end of bracing piece is connected with the slide rail, and sliding connection has the sensor on the slide rail, and the top of slide rail is connected with the kicking block corresponding with the sensor, and the other end of bracing piece is connected with the handle, is connected with the stay cord on the handle, and the other end and the sensor of stay cord are connected, still are connected through reset spring between sensor and the slide rail.
Preferably, the exterior of the sensor is covered with a housing.
Preferably, the end of the pull rope connected with the sensor is connected with a limiting block.
Preferably, a cover plate is connected between the supporting rod and the top block.
Preferably, one end of the support rod close to the handle is connected with a display screen, and the display screen is electrically connected with the sensor.
Preferably, the handle comprises a fixed handle and a movable handle, wherein the fixed handle is connected to the end of the support rod, the movable handle is rotatably connected with the fixed handle through a rotating shaft, and the end of the pull rope is connected with the movable handle.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses with the sensor setting on the slide rail, drive the sensor action through the stay cord to test the tension of cable wire with the kicking block cooperation, have small in size, measurement accuracy height and be applicable to the characteristics that multiple occasion was used.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is an enlarged schematic view of the structure of FIG. 1;
FIG. 3 is a schematic side view of the embodiment of FIG. 1;
fig. 4 is a schematic top view of the present invention;
fig. 5 is an enlarged schematic view of the structure at B in fig. 4 according to the present invention.
In the figure: 1. fixing a handle; 2. a display screen; 3. a support bar; 4. pulling a rope; 5. a movable handle; 6. a slide rail; 7. a return spring; 8. a limiting block; 9. a housing; 10. a sensor; 11. a top block; 12. a cover plate; 13. the steel cable to be tested.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides the following technical solutions: the utility model provides a novel slider formula tension tester for aviation cable wire, includes bracing piece 3, and the one end of bracing piece 3 is connected with slide rail 6, and sliding connection has sensor 10 on slide rail 6, and the top of slide rail 6 is connected with the kicking block 11 corresponding with sensor 10, and the other end of bracing piece 3 is connected with the handle, is connected with stay cord 4 on the handle, and the other end and the sensor 10 of stay cord 4 are connected, still are connected through reset spring 7 between sensor 10 and the slide rail 6.
Specifically, the exterior of the sensor 10 is covered with a housing 9.
By adopting the technical scheme, the sensor 10 is protected by the shell 9.
Specifically, one end of the pull rope 4 connected with the sensor 10 is connected with a limiting block 8.
Through adopting above-mentioned technical scheme, carry on spacingly through stopper 8 to make stay cord 4 can drive sensor 10 and remove on slide rail 6.
Specifically, a cover plate 12 is connected between the support rod 3 and the top block 11.
Through adopting above-mentioned technical scheme, seal the gap between top piece 11 and the bracing piece 3.
Specifically, one end of the support rod 3 close to the handle is connected with a display screen 2, and the display screen 2 is electrically connected with the sensor 10.
By adopting the technical scheme, the data measured by the sensor 10 are read through the display screen 2.
Specifically, the handle includes fixed handle 1 and movable handle 5, and wherein, fixed handle 1 is connected at the tip of bracing piece 3, and movable handle 5 rotates through the pivot with fixed handle 1 to be connected, and the tip and the movable handle 5 of stay cord 4 are connected.
By adopting the technical scheme, the pull rope 4 is controlled by pinching the movable handle 5, so that the sensor 10 is driven to move.
The utility model discloses a theory of operation and use flow: in the initial state, the movable handle 5 is in a relaxed state, and the sensor 10 forms an opening with the top block 11 under the action of the return spring 7. At this time, the wire rope 13 to be measured is caught in the opening. Then the movable handle 5 is firmly held by hand, and at the same time, the pull rope 4 pulls the sensor 10 to move on the slide rail 6, so that the opening between the sensor 10 and the top block 11 is smaller and smaller, the measured steel cable 13 is deformed by stress, and the tension is transferred to the sensor 10, so that the measurement is realized.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a novel slider formula tension tester for aviation cable wire, includes bracing piece (3), its characterized in that: one end of the supporting rod (3) is connected with a sliding rail (6), the sliding rail (6) is connected with a sensor (10) in a sliding mode, a top block (11) corresponding to the sensor (10) is connected above the sliding rail (6), the other end of the supporting rod (3) is connected with a handle, a pull rope (4) is connected onto the handle, the other end of the pull rope (4) is connected with the sensor (10), and the sensor (10) is connected with the sliding rail (6) through a reset spring (7).
2. The novel slider type tension tester for the aviation steel cable as claimed in claim 1, wherein: the exterior of the sensor (10) is covered with a housing (9).
3. The novel slider type tension tester for the aviation steel cable as claimed in claim 1, wherein: one end of the pull rope (4) connected with the sensor (10) is connected with a limiting block (8).
4. The novel slider type tension tester for the aviation steel cable as claimed in claim 1, wherein: a cover plate (12) is connected between the support rod (3) and the top block (11).
5. The novel slider type tension tester for the aviation steel cable as claimed in claim 1, wherein: one end of the support rod (3) close to the handle is connected with a display screen (2), and the display screen (2) is electrically connected with the sensor (10).
6. The novel slider type tension tester for the aviation steel cable as claimed in claim 1, wherein: the handle comprises a fixed handle (1) and a movable handle (5), wherein the fixed handle (1) is connected to the end of the support rod (3), the movable handle (5) is rotatably connected with the fixed handle (1) through a rotating shaft, and the end of the pull rope (4) is connected with the movable handle (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120421621.2U CN214426879U (en) | 2021-02-24 | 2021-02-24 | Novel slider formula tension tester for aviation cable wire |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120421621.2U CN214426879U (en) | 2021-02-24 | 2021-02-24 | Novel slider formula tension tester for aviation cable wire |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214426879U true CN214426879U (en) | 2021-10-19 |
Family
ID=78072060
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120421621.2U Active CN214426879U (en) | 2021-02-24 | 2021-02-24 | Novel slider formula tension tester for aviation cable wire |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214426879U (en) |
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2021
- 2021-02-24 CN CN202120421621.2U patent/CN214426879U/en active Active
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