CN217624118U - Unmanned aerial vehicle carries device with buffer structure - Google Patents
Unmanned aerial vehicle carries device with buffer structure Download PDFInfo
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- CN217624118U CN217624118U CN202221441848.4U CN202221441848U CN217624118U CN 217624118 U CN217624118 U CN 217624118U CN 202221441848 U CN202221441848 U CN 202221441848U CN 217624118 U CN217624118 U CN 217624118U
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- aerial vehicle
- unmanned aerial
- kuppe
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Abstract
The utility model discloses an unmanned aerial vehicle carry device with buffer structure, including the unmanned aerial vehicle main part, the kuppe is installed to the bottom of unmanned aerial vehicle main part, the inside of kuppe has the string carrier through quick detach structure joint, the bottom fixed mounting of unmanned aerial vehicle main part has the bolster, the top laminating of string carrier is in the bottom of bolster. The utility model has the advantages that: the mounting frame is installed in the inside of kuppe behind the loading object, can improve the anti-wind and the anti-turbulent flow ability of unmanned aerial vehicle main part after the mounting through utilizing the kuppe. The bolster can suppress the mount frame after the installation spacing promptly, can play the effect of buffering again when descending, slows down the impact force when unmanned aerial vehicle main part descends. The inside of the kuppe is carried in the quick detach structure installation of carrying frame utilization, sets up the spout on the fixed block in the kuppe, and the hanging frame utilizes couple department to slide in spout department to drop in draw-in groove department after rotatory, easy dismounting.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle accessory technical field specifically is an unmanned aerial vehicle carry device with buffer structure.
Background
An unmanned plane, called an unmanned plane for short, is an unmanned plane operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer.
When object one side of present unmanned aerial vehicle carry is planar structure, the air resistance that unmanned aerial vehicle received at the in-process of transporting is big more, and unmanned aerial vehicle is unbalanced easily, and anti-wind air resistance pressure intensity ability is worse to and present carry device dismouting inconvenient, and do not have buffer structure, the vibrations that the descending in-process received are great.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle carry device with buffer structure who proposes.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides an unmanned aerial vehicle carry device with buffer structure, includes the unmanned aerial vehicle main part, the kuppe is installed to the bottom of unmanned aerial vehicle main part, the inside of kuppe has the carry frame through the quick detach structure joint, the bottom fixed mounting of unmanned aerial vehicle main part has the bolster, the top laminating of carry frame is in the bottom of bolster.
Preferably, the quick detach structure includes the fixed block, fixed block fixed connection is in the inside both sides of kuppe, the spout has been seted up on the lateral wall of fixed block, be provided with the draw-in groove in the cell body of spout, the joint of string carrier frame is in the draw-in groove.
Preferably, the hanging frame comprises a carrying frame body, hooks are fixedly connected to two sides of the carrying frame body, and telescopic support legs are fixedly connected to the bottom of the carrying frame body.
Preferably, the telescopic supporting foot comprises a sleeve and a movable rod, the movable rod moves in the sleeve, the sleeve is fixedly installed on the side face of the luggage carrier, a fastening piece is installed on the surface of the sleeve, and a supporting foot body is fixedly connected to the bottom of the movable rod.
Preferably, the bottom of unmanned aerial vehicle main part is provided with the mounting groove, the top fixedly connected with cardboard of kuppe, the cardboard joint is in the mounting groove.
The utility model has the advantages that:
first, the utility model provides an unmanned aerial vehicle carry device with buffer structure, carry and install in the inside of kuppe behind the loading object, can improve the anti-wind and the anti-turbulent flow ability of carrying back unmanned aerial vehicle main part through utilizing the kuppe.
Second, bolster can suppress the mount frame after the installation spacing promptly, can play the effect of buffering again when descending, the impact force when slowing down the unmanned aerial vehicle main part and descending.
Third, the inside of the kuppe is carried in the quick detach structure installation to the mount frame, sets up the spout on the fixed block in the kuppe, and the mount frame utilizes couple department to slide in spout department to fall in draw-in groove department after the rotation, easy dismounting, this moment, the bolster can also suppress the couple.
Drawings
FIG. 1 is a schematic diagram of the basic structure of the present invention;
FIG. 2 is a bottom view of the deflector portion of the present invention;
FIG. 3 is a schematic view of the structure of the quick release structure of the present invention;
fig. 4 is an enlarged view of the structure of the part a in fig. 1 of the present invention.
1. An unmanned aerial vehicle main body; 2. a dome; 3. a quick release structure; 301. a fixed block; 302. a chute; 303. a card slot; 4. hanging a carrier; 401. a carrying frame body; 402. hooking; 403. a retractable leg; 4031. a sleeve; 4032. a movable rod; 4033. a fastener; 4034. a leg body; 5. a buffer member; 6. mounting grooves; 7. provided is a clamping plate.
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 efforts all belong to the protection scope of the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and to simplify the description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore should not be construed as limiting the present invention.
As shown in fig. 1-4, the utility model provides a pair of unmanned aerial vehicle carry device with buffer structure, including unmanned aerial vehicle main part 1, kuppe 2 is installed to the bottom of unmanned aerial vehicle main part 1, and there is carry frame 4 inside of kuppe 2 through 3 joints of rapid disassembly structure, and the bottom fixed mounting of unmanned aerial vehicle main part 1 has bolster 5, and the top laminating of carry frame 4 is in the bottom of bolster 5. Kuppe 2 is the streamlined cover body in fact, according to aerodynamic analysis research, when high-speed removal in the air, can play the effect of reposition of redundant personnel water conservancy diversion to the air, during the use, mount frame 4 installs the inside at kuppe 2 behind the loaded object, can improve the anti-wind and the anti-turbulent flow ability of unmanned aerial vehicle main part 1 after the mount through utilizing kuppe 2, the mount can load on the mount frame 4 of installation, use as the standard, the structure that mount frame 4 loaded the installation object here limits and introduces, mount frame 4 utilizes quick detach structure 3 to install the inside of mounting kuppe 2, be convenient for carry out the dismouting, simultaneously after its installation, bolster 5 contradicts at the top of mount frame 4, bolster 5 can be an elastic component or a set of buffer structure, the drawing uses the spring as an example, 5 can suppress the mount frame 4 after the installation spacing promptly, can play the effect of buffering again when descending, the impact force when slowing down unmanned aerial vehicle main part 1 descends.
Quick detach structure 3 includes fixed block 301, and fixed block 301 fixed connection has seted up spout 302 in the inside both sides of kuppe 2 on the lateral wall of fixed block 301, is provided with draw-in groove 303 in the cell body of spout 302, and the joint of mount frame 4 is in draw-in groove 303. The sliding groove 302 is formed in the fixing block 301 in the air guide sleeve 2, the mounting frame 4 slides at the sliding groove 302 through the hook 402 and falls at the clamping groove 303 after rotating, and at the moment, the hook 402 can be further pressed by the buffer part 5.
The hanging rack 4 comprises a hanging rack body 401, hooks 402 are fixedly connected to two sides of the hanging rack body 401, and telescopic support legs 403 are fixedly connected to the bottom of the hanging rack body 401. The object carrying frame body 401 is an object carrying and hanging main structure, and the hook 402 can correspond to the quick release structure 3, so that the object carrying frame 4 is convenient to disassemble and assemble, and the telescopic support legs 403 can support the ground.
The telescopic leg 403 comprises a sleeve 4031 and a movable bar 4032, wherein the movable bar 4032 moves in the sleeve 4031, the sleeve 4031 is fixedly mounted on the side surface of the carrier rack, a fastener 4033 is mounted on the surface of the sleeve 4031, and a leg body 4034 is fixedly connected to the bottom of the movable bar 4032. Unmanned aerial vehicle main part 1 all can follow ground and take off and land when going up and down, utilizes the movable bar 4032 can be in sleeve 4031 internalization, utilizes fastener 4033 to carry out the elasticity, and fastener 4033 can set up to the bolt, adjusts support height, makes the carry thing can not contact ground influence when going up and down and balance.
The bottom of unmanned aerial vehicle main part 1 is provided with mounting groove 6, and the top fixedly connected with cardboard 7 of kuppe 2, 7 joints of cardboard are in mounting groove 6. Rotate kuppe 2 and can make cardboard 7 joint or break away from mounting groove 6 promptly to can be convenient for carry out the dismouting to kuppe 2.
The working principle is as follows: kuppe 2 is the streamlined cover body in fact, according to aerodynamic analysis research, when high-speed removal in the air, can play the effect of reposition of redundant personnel water conservancy diversion to the air, during the use, mount frame 4 installs the inside at kuppe 2 behind the loaded object, can improve the anti-wind and the anti-turbulent flow ability of unmanned aerial vehicle main part 1 after the mount through utilizing kuppe 2, the mount can load on the mount frame 4 of installation, use as the standard, the structure that mount frame 4 loaded the installation object here limits and introduces, mount frame 4 utilizes quick detach structure 3 to install the inside of mounting kuppe 2, be convenient for carry out the dismouting, simultaneously after its installation, bolster 5 contradicts at the top of mount frame 4, bolster 5 can be an elastic component or a set of buffer structure, the drawing uses the spring as an example, 5 can suppress the mount frame 4 after the installation spacing promptly, can play the effect of buffering again when descending, the impact force when slowing down unmanned aerial vehicle main part 1 descends. Set up spout 302 on fixed block 301 in kuppe 2, carry frame 4 and utilize couple 402 to be in spout 302 department and slide to fall in draw-in groove 303 department after the rotation, at this moment, bolster 5 can also suppress couple 402, carries thing support body 401 for carrying thing, string thing major structure, and couple 402 can be corresponding with quick detach structure 3, makes 4 easy dismounting of carry frame, and telescopic stabilizer blade 403 can support ground. Unmanned aerial vehicle main part 1 all can follow ground and take off and land when going up and down, utilizes the movable bar 4032 can be in sleeve 4031 internalization, utilizes fastener 4033 to carry out the elasticity, and fastener 4033 can set up to the bolt, adjusts support height, makes the carry thing can not contact ground influence when going up and down and balance. Rotate kuppe 2 and can make cardboard 7 joint or break away from mounting groove 6 promptly to can be convenient for carry out the dismouting to kuppe 2.
The foregoing shows and describes the basic principles, essential features, and advantages of the invention. It should be understood by those skilled in the art that the present invention is not limited by the above embodiments, and the description in the above embodiments and the description is only preferred examples of the present invention, and is not intended to limit the present invention, and that the present invention can have various changes and modifications without departing from the spirit and scope of the present invention, and these changes and modifications all fall into the scope of the claimed invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. The utility model provides an unmanned aerial vehicle carries device with buffer structure, includes unmanned aerial vehicle main part (1), its characterized in that: kuppe (2) are installed to the bottom of unmanned aerial vehicle main part (1), there is hanging frame (4) inside of kuppe (2) through quick detach structure (3) joint, the bottom fixed mounting of unmanned aerial vehicle main part (1) has bolster (5), the top laminating of hanging frame (4) is in the bottom of bolster (5).
2. The unmanned aerial vehicle mounting device with buffer structure of claim 1, characterized in that: quick detach structure (3) include fixed block (301), fixed block (301) fixed connection has been seted up spout (302) in the inside both sides of kuppe (2) on the lateral wall of fixed block (301), be provided with draw-in groove (303) in the cell body of spout (302), hang carrier (4) joint in draw-in groove (303).
3. The unmanned aerial vehicle mounting device with buffer structure of claim 1, characterized in that: the hanging rack (4) comprises a rack body (401), hooks (402) are fixedly connected to two sides of the rack body (401), and telescopic support legs (403) are fixedly connected to the bottom of the rack body (401).
4. The unmanned aerial vehicle mounting device with buffer structure of claim 3, characterized in that: the telescopic supporting foot (403) comprises a sleeve (4031) and a movable rod (4032), wherein the movable rod (4032) moves in the sleeve (4031), the sleeve (4031) is fixedly installed on the side face of the carrier rack, a fastener (4033) is installed on the surface of the sleeve (4031), and a supporting foot body (4034) is fixedly connected to the bottom of the movable rod (4032).
5. An unmanned aerial vehicle mounting device with buffer structure of claim 1, characterized in that: the bottom of unmanned aerial vehicle main part (1) is provided with mounting groove (6), the top fixedly connected with cardboard (7) of kuppe (2), cardboard (7) joint is in mounting groove (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221441848.4U CN217624118U (en) | 2022-06-10 | 2022-06-10 | Unmanned aerial vehicle carries device with buffer structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221441848.4U CN217624118U (en) | 2022-06-10 | 2022-06-10 | Unmanned aerial vehicle carries device with buffer structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217624118U true CN217624118U (en) | 2022-10-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221441848.4U Active CN217624118U (en) | 2022-06-10 | 2022-06-10 | Unmanned aerial vehicle carries device with buffer structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217624118U (en) |
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2022
- 2022-06-10 CN CN202221441848.4U patent/CN217624118U/en active Active
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