CN211626885U - Many specifications of integral type thrust testing arrangement - Google Patents
Many specifications of integral type thrust testing arrangement Download PDFInfo
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- CN211626885U CN211626885U CN201922461962.8U CN201922461962U CN211626885U CN 211626885 U CN211626885 U CN 211626885U CN 201922461962 U CN201922461962 U CN 201922461962U CN 211626885 U CN211626885 U CN 211626885U
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Abstract
The utility model discloses a many specifications of integral type thrust testing arrangement, it includes the device body, the up end of device body runs through and is provided with a plurality of test fixed slots that are used for fixed different specification products, in the inside of device body corresponds the test fixed slot is provided with the waste material and holds the chamber, just a side end intercommunication of device body the waste material holds the chamber and is provided with the exhaust outlet. The utility model is of an integrated structure, can directly discharge test waste without disassembly, can avoid the waste from splashing at will while ensuring the accuracy of the test, and effectively prevents the waste from splashing outside the device body in the thrust test process by arranging a slope, thereby being convenient for centralized processing of the waste; in addition, the device can be compatible with the laminating assemblies with different dimensions and specifications to perform thrust test, and does not need to additionally manufacture a plurality of thrust test devices with different specifications, so that the design times of the device are reduced, and the production cost is saved.
Description
Technical Field
The utility model relates to a light filter laminating processing field, concretely relates to many specifications of integral type thrust testing arrangement.
Background
At present, in the process of laminating and processing the optical filter, the thrust test needs to be carried out on an optical filter laminating assembly, the existing thrust test device is mainly formed by assembling a separated cover plate and a base, the cover plate and the base need to be disassembled when waste materials are discharged every time, and after repeated disassembly and assembly, the thrust test device is easy to be assembled badly due to looseness, so that the accuracy of the thrust test is influenced; and this thrust testing arrangement only can support the laminating subassembly of few several specifications to carry out thrust test, generally be provided with 2 to 4 test fixed slots on this apron promptly, in order to compatible the many specifications laminating subassembly of different length, width, often need make the thrust testing arrangement of different specifications come the adaptation, cause the inconvenience of test, manufacturing cost is high.
SUMMERY OF THE UTILITY MODEL
In order to overcome the technical problem, the utility model discloses a many specifications of integral type thrust testing arrangement.
The utility model discloses a realize that the technical scheme that above-mentioned purpose adopted is:
the utility model provides a many specifications of integral type thrust testing arrangement, its includes the device body, the up end of device body runs through and is provided with a plurality of test fixed slots that are used for fixed different specification products, in the inside of device body corresponds the test fixed slot is provided with the waste material and holds the chamber, just a side end intercommunication of device body the waste material holds the chamber and is provided with the waste material discharge port.
The integrated multi-specification thrust test device is characterized in that the height of the waste discharge port is smaller than that of the waste accommodating cavity.
The integrated multi-specification thrust test device is characterized in that a slope is formed between the waste discharge port and the waste containing cavity.
The integrated multi-specification thrust testing device is characterized in that the slope is provided with a fillet.
The integrated multi-specification thrust test device is characterized in that the angle of the slope is 14.4 degrees.
The integrated multi-specification thrust testing device is characterized in that four rows of groove positions with different dimensions are arranged on the upper end face of the device body according to the interval distance, and four test fixing grooves with different dimensions are arranged in each groove position according to the interval distance.
The integrated multi-specification thrust testing device is characterized in that the specification of the test fixing groove is 5.0mm multiplied by 5.0 mm-9.0 mm multiplied by 9.0 mm.
In the integrated multi-specification thrust testing device, the four test fixing grooves connected with the slot position in each row are provided with the water flowing grooves.
In the above integrated multi-specification thrust testing device, the length of the gutter channel is greater than the length of the slot position, and the width of the gutter channel is smaller than the width of the test fixing slot.
In the integrated multi-specification thrust testing device, the end points of the testing fixing grooves are respectively provided with the avoiding holes.
The utility model has the advantages that: the utility model is of an integrated structure, can directly discharge test waste without disassembly, can avoid the waste from splashing at will while ensuring the accuracy of the test, and effectively prevents the waste from splashing outside the device body in the thrust test process by arranging a slope, thereby being convenient for centralized processing of the waste; in addition, the device can be compatible with the laminating assemblies with different dimensions and specifications to perform thrust test, and does not need to additionally manufacture a plurality of thrust test devices with different specifications, so that the design times of the device are reduced, and the production cost is saved.
Drawings
The present invention will be further explained with reference to the drawings and examples.
Fig. 1 is a perspective view of the present invention;
fig. 2 is a schematic top view of the present invention;
fig. 3 is a schematic cross-sectional view taken along the direction a-a in fig. 2 according to the present invention.
Detailed Description
The present invention is further described below with reference to specific embodiments, so that the technical solution of the present invention is easier to understand and master, rather than to limit the present invention.
Example (b): referring to fig. 1 to 3, the integrated multi-specification thrust testing device provided in this embodiment includes a device body 1, a plurality of test fixing grooves 2 for fixing products of different specifications are formed in an upper end surface of the device body 1 in a penetrating manner, a waste accommodating cavity 3 is formed in the device body 1 corresponding to the test fixing grooves 2, and a waste discharge port 4 is formed in one side end of the device body 1 and communicated with the waste accommodating cavity 3; the laminating subassembly of being convenient for compatible different dimensions carries out thrust test, and adopts the integral type device body 1 need not to open and can directly discharge the test waste material, avoids when thrust test, the waste material warp the clearance department of device body 1 splashes at will.
Preferably, the height of the waste material discharge opening 4 is smaller than that of the waste material accommodating cavity 3, a slope 5 is formed between the waste material discharge opening 4 and the waste material accommodating cavity 3, wherein the angle of the slope 5 is 14.4 °, the width is 8.0mm, and the height is 4.0mm, and the slope 5 prevents waste materials generated in the thrust test from splashing outside the device body 1, so that the waste materials can be conveniently treated in a centralized manner.
Specifically, slope 5 is equipped with the radius, the radius of radius is 2.5mm, is convenient for centralized processing and derives the waste material.
Preferably, four rows of slot positions with different dimensions are arranged on the upper end surface of the device body 1 at intervals, and four test fixing grooves 2 with different dimensions are arranged in each row of slot positions at intervals; test fixed slot 2 not only can be compatible the flat class laminating subassembly of different specifications, can also be compatible the screw thread class laminating subassembly of different specifications, and compatible practicality is strong, according to the size and specification of laminating subassembly, will laminate the subassembly and arrange corresponding specification carry out thrust test in the test fixed slot 2.
Furthermore, the specification of the test fixing groove 2 is 5.0mm multiplied by 5.0mm to 9.0mm multiplied by 9.0 mm; specifically, the specification of the test fixing groove 2 is 5.0mm × 5.0mm, 5.5mm × 5.5mm, 6.0mm × 6.0mm, 6.5mm × 6.5mm, 7.0mm × 7.0mm, 7.5mm × 7.5mm, 8.0mm × 8.0mm, 8.5mm × 8.5mm, 9.0mm × 9.0 mm.
Furthermore, four test fixing grooves 2 are connected to each row of the slot positions, a water flowing groove 6 is arranged on each row of the slot positions, the length of each water flowing groove 6 is larger than that of each slot position, the width of each water flowing groove 6 is smaller than that of each test fixing groove 2, and the water flowing grooves 6 are convenient to clamp and attach the assembly by using tweezers.
Further, the end points of the test fixing grooves 2 are respectively provided with avoiding holes 7, and the avoiding holes 7 are used for avoiding that four end corners of the laminating assembly interfere with the test fixing grooves 2 to influence the thrust test result.
When the utility model works, firstly, the size specification of the laminating component is determined, the laminating component is placed in the test fixing groove 2 with corresponding specification, the thrust test is carried out under the use of a thrust gauge, and the waste material generated in the test falls into the waste material accommodating cavity 3; after the thrust test is completed, the device body 1 is directly taken out, and the test waste is discharged from the waste discharge port 4.
The utility model is of an integrated structure, can directly discharge test waste without disassembly, can avoid the waste from splashing at will while ensuring the accuracy of the test, and effectively prevents the waste from splashing outside the device body in the thrust test process by arranging a slope, thereby being convenient for centralized processing of the waste; in addition, the device can be compatible with the laminating assemblies with different dimensions and specifications to perform thrust test, and does not need to additionally manufacture a plurality of thrust test devices with different specifications, so that the design times of the device are reduced, and the production cost is saved.
The above description is only for the preferred embodiment of the present invention, and is not intended to limit the present invention in any way. The technical solution of the present invention can be used by anyone skilled in the art to make many possible variations and modifications, or to modify equivalent embodiments, using the technical means and contents disclosed above, without departing from the scope of the technical solution of the present invention. Therefore, the protection scope of the present invention should be covered by the equivalent changes made according to the shape, structure and principle of the present invention, all without departing from the technical solution of the present invention.
Claims (10)
1. The utility model provides a many specifications of integral type thrust testing arrangement which characterized in that, it includes the device body, the up end of device body runs through and is provided with a plurality of test fixed slots that are used for fixed different specification products, in the inside of device body corresponds the test fixed slot is provided with the waste material and holds the chamber, just a side end intercommunication of device body the waste material holds the chamber and is provided with the waste discharge mouth.
2. The integrated, multi-specification thrust testing device of claim 1, wherein a height of the waste ejection port is less than a height of the waste containment cavity.
3. The integrated, multi-specification thrust test apparatus of claim 2, wherein a ramp is formed between the scrap discharge opening and the scrap receptacle cavity.
4. The integrated, multi-gauge thrust test device of claim 3, wherein the ramp is rounded.
5. The integrated, multi-gauge thrust test device of claim 4, wherein the angle of the ramp is 14.4 °.
6. The integrated multi-specification thrust testing device according to claim 1, wherein four rows of slots with different dimensions are arranged on the upper end face of the device body at intervals, and four test fixing grooves with different dimensions are arranged in each row of slots at intervals.
7. The integrated multi-specification thrust test device according to claim 5, wherein the specification of the test fixing groove is 5.0mm x 5.0mm to 9.0mm x 9.0 mm.
8. The integrated multi-specification thrust testing device according to claim 6, wherein a water flowing groove is formed in each row of the groove positions to connect four test fixing grooves.
9. The integrated multi-specification thrust test device according to claim 8, wherein the length of the water flowing groove is greater than the length of the slot position, and the width of the water flowing groove is smaller than the width of the test fixing groove.
10. The integrated multi-specification thrust testing device according to claim 9, wherein avoidance holes are respectively formed at end points of the test fixing grooves.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922461962.8U CN211626885U (en) | 2019-12-31 | 2019-12-31 | Many specifications of integral type thrust testing arrangement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922461962.8U CN211626885U (en) | 2019-12-31 | 2019-12-31 | Many specifications of integral type thrust testing arrangement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211626885U true CN211626885U (en) | 2020-10-02 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922461962.8U Active CN211626885U (en) | 2019-12-31 | 2019-12-31 | Many specifications of integral type thrust testing arrangement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211626885U (en) |
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2019
- 2019-12-31 CN CN201922461962.8U patent/CN211626885U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: An integrated multi specification thrust testing device Effective date of registration: 20230919 Granted publication date: 20201002 Pledgee: Tongren branch of China Construction Bank Corp. Pledgor: Guizhou Tongren Xujing Photoelectric Technology Co.,Ltd. Registration number: Y2023980057364 |