CN213594528U - Lightweight unmanned aerial vehicle carries on equipment linkage - Google Patents
Lightweight unmanned aerial vehicle carries on equipment linkage Download PDFInfo
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- CN213594528U CN213594528U CN202021501765.0U CN202021501765U CN213594528U CN 213594528 U CN213594528 U CN 213594528U CN 202021501765 U CN202021501765 U CN 202021501765U CN 213594528 U CN213594528 U CN 213594528U
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- unmanned aerial
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Abstract
The utility model relates to an unmanned aerial vehicle carries on equipment technical field, in particular to lightweight unmanned aerial vehicle carries on equipment linkage, include: a base, under which a slideway is arranged; a slider slidable in the slide; the fastening screw is vertically arranged on the side surface of the slide way, is vertical to the moving direction of the slide block and is positioned above the slide block; the locking block is arranged in the slide way, the locking block is fixedly connected with the end part of the fastening screw, and the locking block and the sliding block are positioned on the same plane; and the locking groove is arranged on the side surface of the sliding block, and when the sliding block moves to a specified position, the locking block is clamped into the locking groove. The embodiment of the utility model provides a pair of lightweight unmanned aerial vehicle carries on equipment linkage inserts the slider back in the slide completely, through rotatory fastening screw, makes fastening screw drive the latch segment and removes, goes into the locking groove when the latch segment card, realizes the locking of slider and slide, makes the carry device steadiness better.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle carries on equipment technical field, in particular to lightweight unmanned aerial vehicle carries on equipment linkage.
Background
Unmanned aerial vehicle carries on equipment fixing needs to install fixedly through simple and easy carry device, however this kind of simple and easy carry device among the prior art, the structure is too simple, and the fixed reliability of installation is relatively poor, and the steadiness is relatively poor, if consider to use multiple fastening bolt to fix, but the steadiness can effectively promote but its dismouting efficiency of inconvenient carry device and unmanned aerial vehicle again. Therefore, how to make and satisfy the firm reliable performance of installation, the mounting device that can ensure mounting device and unmanned aerial vehicle quick assembly disassembly efficiency again is the difficult problem that needs the solution to technical personnel in this field.
SUMMERY OF THE UTILITY MODEL
An embodiment of the utility model provides a lightweight unmanned aerial vehicle carries on equipment linkage for solve the poor problem of current carry device steadiness.
In order to solve the problem that above-mentioned background art provided, the embodiment of the utility model provides a lightweight unmanned aerial vehicle carries on equipment linkage, include: a base, under which a slideway is arranged; the sliding block can slide in the slide way and is used for connecting equipment carried by the unmanned aerial vehicle; the fastening screw is vertically arranged on the side surface of the slide way, is vertical to the moving direction of the slide block and is positioned above the slide block; the locking block is arranged in the slide way, the locking block is fixedly connected with the end part of the fastening screw, and the locking block and the sliding block are positioned on the same plane; and the locking groove is arranged on the side surface of the sliding block, and when the sliding block moves to a specified position, the locking block is clamped in the locking groove.
Preferably, a transverse pipe is fixedly arranged above the base, a base is arranged at the end part of the transverse pipe, and an antenna is fixedly arranged on the base.
Preferably, a connecting pipe is fixedly arranged at the position of the base corresponding to the transverse pipe, and the transverse pipe is connected with the connecting pipe through a movable joint.
Preferably, a plurality of grooves are uniformly formed in the end portions of the transverse pipe and the connecting pipe in the axial direction, protruding strips are formed between the grooves in an adjacent mode, the arc angles corresponding to the grooves and the protruding strips are the same, and the protruding strips can be inserted into the grooves.
Preferably, the arc angle of the groove and the convex strip is 60 degrees.
The utility model has the advantages that:
the embodiment of the utility model provides a pair of lightweight unmanned aerial vehicle carries on equipment linkage inserts the slider back in the slide completely, through rotatory fastening screw, makes fastening screw drive the latch segment and removes, goes into the locking groove when the latch segment card, realizes the locking of slider and slide, makes the carry device steadiness better.
Additional features and advantages of the invention will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by the practice of the invention. The objectives and other advantages of the invention will be realized and attained by the structure particularly pointed out in the written description and claims hereof as well as the appended drawings.
The technical solution of the present invention is further described in detail by the accompanying drawings and examples.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention.
In the drawings:
FIG. 1 is a schematic structural view of a slider and a base according to an embodiment of the present invention;
FIG. 2 is a schematic view of the fastening screw and the slide rail of the present invention;
FIG. 3 is a schematic view of the middle cross tube and the antenna;
fig. 4 is a schematic view of the cooperation between the middle horizontal tube and the connecting tube of the present invention.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.
Example 1
As shown in fig. 1 and 2, the embodiment of the utility model provides a lightweight unmanned aerial vehicle carries on equipment linkage, include: a base 1, under which a slideway 2 is arranged; the sliding block 3 can slide in the slideway 2, and the sliding block 3 is used for connecting equipment carried by the unmanned aerial vehicle; the fastening screw 4 is vertically arranged on the side surface of the slide way 2, the fastening screw 4 is vertical to the moving direction of the slide block 3, and the fastening screw 4 is positioned above the slide block 3; the locking block 5 is arranged inside the slide way 2, the locking block 5 is fixedly connected with the end part of the fastening screw 4, and the locking block 5 and the slide block 3 are positioned on the same plane; and the locking groove 6 is arranged on the side surface of the sliding block 3, and when the sliding block 3 moves to a specified position, the locking block 5 is clamped in the locking groove 6.
In the above embodiment, after the sliding block 3 is completely inserted into the sliding way 2, the fastening screw 4 is rotated to drive the locking block 5 to move, and when the locking block 5 is clamped into the locking groove 6, the sliding block 3 and the sliding way 2 are locked, so that the mounting device is better in stability.
Example 2
As shown in fig. 3 and 4, a transverse pipe 7 is fixedly arranged above the base 1, the transverse pipe 7 is a carbon fiber pipe, a base 8 is arranged at the end of the transverse pipe 7, and an antenna 9 is fixedly arranged on the base 8.
A connecting pipe 10 is fixedly arranged at the position of the base 8 corresponding to the transverse pipe 7, and the transverse pipe 7 is connected with the connecting pipe 10 through a movable joint 11; the tip of violently managing 7 and connecting pipe 10 all evenly sets up a plurality of recesses 12 along the axial, and is adjacent form protruding strip 13 between the recess 12, the circular arc angle that recess 12 and protruding strip 13 correspond is the same, protruding strip 13 can insert in the recess 12, in this embodiment, the circular arc angle that recess 12 and protruding strip 13 correspond is 60.
In the above embodiment, the transverse tube 7 and the base 8 are connected through the connecting tube 10 and the movable joint 11, so that the antenna 9 is convenient to disassemble; through inserting protruding strip 13 in recess 12, at first will violently manage 7 and connecting pipe 10 and dock, then lock union 11, make violently manage 7 and connecting pipe 10 butt joint more firm, the phenomenon that can not appear rocking, pine takes off, when the circular arc angle that recess 12 and protruding strip 13 correspond was 60, the firm nature was better when making violently manage 7 and connecting pipe 10 butt joint convenience.
It will be apparent to those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention. Thus, if such modifications and variations of the present invention fall within the scope of the claims and their equivalents, the present invention is also intended to include such modifications and variations.
Claims (5)
1. The utility model provides a lightweight unmanned aerial vehicle carries on equipment linkage, its characterized in that includes:
a base, under which a slideway is arranged;
the sliding block can slide in the slide way and is used for connecting equipment carried by the unmanned aerial vehicle;
the fastening screw is vertically arranged on the side surface of the slide way, is vertical to the moving direction of the slide block and is positioned above the slide block;
the locking block is arranged in the slide way, the locking block is fixedly connected with the end part of the fastening screw, and the locking block and the sliding block are positioned on the same plane;
and the locking groove is arranged on the side surface of the sliding block, and when the sliding block moves to a specified position, the locking block is clamped in the locking groove.
2. The suspension device for light unmanned aerial vehicle carrying equipment according to claim 1, wherein a transverse pipe is fixedly arranged above the base, a base is arranged at an end of the transverse pipe, and an antenna is fixedly arranged on the base.
3. The suspension device for light unmanned aerial vehicle carrying equipment according to claim 2, wherein a connecting pipe is fixedly arranged at a position of the base corresponding to the transverse pipe, and the transverse pipe is connected with the connecting pipe through a movable joint.
4. The suspension device for light unmanned aerial vehicle carrying equipment according to claim 3, wherein a plurality of grooves are uniformly formed in the end portions of the transverse pipe and the connecting pipe along the axial direction, a protruding strip is formed between every two adjacent grooves, the arc angles corresponding to the grooves and the protruding strips are the same, and the protruding strips can be inserted into the grooves.
5. The suspension device for light-weight unmanned aerial vehicle carrying equipment according to claim 4, wherein the arc angle corresponding to the groove and the protruding strip is 60 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021501765.0U CN213594528U (en) | 2020-07-27 | 2020-07-27 | Lightweight unmanned aerial vehicle carries on equipment linkage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021501765.0U CN213594528U (en) | 2020-07-27 | 2020-07-27 | Lightweight unmanned aerial vehicle carries on equipment linkage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213594528U true CN213594528U (en) | 2021-07-02 |
Family
ID=76583420
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021501765.0U Active CN213594528U (en) | 2020-07-27 | 2020-07-27 | Lightweight unmanned aerial vehicle carries on equipment linkage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213594528U (en) |
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2020
- 2020-07-27 CN CN202021501765.0U patent/CN213594528U/en active Active
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