CN220996778U - Unmanned aerial vehicle mounting mechanism - Google Patents

Unmanned aerial vehicle mounting mechanism Download PDF

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Publication number
CN220996778U
CN220996778U CN202322181610.3U CN202322181610U CN220996778U CN 220996778 U CN220996778 U CN 220996778U CN 202322181610 U CN202322181610 U CN 202322181610U CN 220996778 U CN220996778 U CN 220996778U
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CN
China
Prior art keywords
unmanned aerial
aerial vehicle
mounting
vehicle body
groove
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CN202322181610.3U
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Chinese (zh)
Inventor
冼博特
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Kunshan Yifei Aviation Intelligent Technology Co ltd
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Kunshan Yifei Aviation Intelligent Technology Co ltd
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Priority to CN202322181610.3U priority Critical patent/CN220996778U/en
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Publication of CN220996778U publication Critical patent/CN220996778U/en
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Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle mounting mechanism, which comprises an unmanned aerial vehicle body, wherein brackets are fixedly arranged on two sides of the bottom of the unmanned aerial vehicle body, a mounting frame is arranged at the bottom of the unmanned aerial vehicle body, mounting grooves are formed on two sides of the upper end of the mounting frame, mounting blocks are slidably arranged in the two mounting grooves, the upper ends of the mounting blocks are fixedly connected with the lower end of the unmanned aerial vehicle body, sliding holes are formed in groove walls on one side, deviating from the two mounting grooves, of the two mounting blocks, clamping rods are slidably arranged in the sliding holes, one ends of the clamping rods extend into the mounting grooves, clamping grooves matched with the clamping rods are formed in the side walls of the mounting blocks, strip-shaped holes are formed in the rod walls of the clamping rods, and a propping mechanism is fixedly arranged in the strip-shaped holes. The utility model is convenient for dismounting the mounting frame, reduces the labor intensity of staff, can provide locking for the clamping mechanism and improves the stability of the mounting structure.

Description

Unmanned aerial vehicle mounting mechanism
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle mounting mechanism.
Background
Unmanned aircraft, for short, "unmanned aircraft," is unmanned aircraft that is maneuvered using a radio remote control device and a self-contained programming device, or is operated autonomously, either entirely or intermittently, by an on-board computer. The unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.
In the prior art, a plurality of bolts are generally adopted to disassemble and assemble the mounting frame, so that the time and the labor are wasted, the efficiency is low, the labor intensity of workers is increased, and the unmanned aerial vehicle mounting mechanism is provided.
Disclosure of utility model
The utility model aims to provide the unmanned aerial vehicle mounting mechanism which is convenient for dismounting the mounting frame, reduces the labor intensity of workers, can provide locking for the clamping mechanism, and improves the stability of the mounting structure so as to solve the problems in the prior art.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
The utility model provides an unmanned aerial vehicle mounting mechanism, includes the unmanned aerial vehicle body, the bottom both sides of unmanned aerial vehicle body are all fixed and are equipped with the support, the bottom of unmanned aerial vehicle body is provided with the mount, the mounting groove has all been seted up to the upper end both sides of mount, two all slide in the mounting groove and be equipped with the installation piece, the upper end of installation piece all with the lower extreme fixed connection of unmanned aerial vehicle body, two the slide hole has all been seted up to one side cell wall that the installation groove deviates from mutually, the downthehole sliding of slide is equipped with the draw-in lever, the one end of draw-in lever extends to the mounting inslot, the draw-in groove with draw-in lever matched with is seted up to the lateral wall of installation piece, the bar hole has been seted up to the bar wall of draw-in lever, bar is fixed to be equipped with to tight mechanism, the one end that the draw-in lever is located the slide hole is rotated through the pivot and is connected with the circular block, the other end of circular block extends to the slide hole outside, circular slot has all been seted up to the pore wall of slide hole both sides.
Preferably, the abutting mechanism comprises a limiting rod, the limiting rod is arranged in the bar-shaped hole in a sliding mode at one side close to the circular block, two ends of the limiting rod are fixedly connected with the wall of the sliding hole, and a side rod wall of the limiting rod, far away from the circular block, is fixedly connected with a first spring.
Preferably, the locking mechanism comprises a locking rod, the locking rod is arranged in the circular groove in a sliding mode, one end of the locking rod extends to the outside of the circular groove, a through groove matched with the locking rod is formed in the side wall of the circular block, and a second spring is fixedly arranged at the bottom of the circular groove.
Preferably, one end of the circular block extending to the outside of the sliding hole is fixedly connected with a pull ring.
Preferably, one end of the locking rod, which is positioned outside the circular groove, is provided with a spherical surface.
Preferably, the first spring and the second spring are always in a compressed state.
Compared with the prior art, the utility model has the beneficial effects that:
This unmanned aerial vehicle mounting mechanism, through the clamping lever that is equipped with, the circular piece, support tight mechanism and locking mechanism, 90 rotate the pull ring, the pull ring drives the circular piece and rotates, logical groove on the circular piece is ejecting with the locking lever simultaneously, the circular piece no longer by the locking this moment, the pulling pull ring can be through circular piece pulling clamping lever, in the mounting groove is gone into to the installation piece card, loosen the pull ring, in the draw-in groove on the installation piece was gone into to first spring promotion clamping lever card, 90 rotate the pull ring once more, the pull ring drives logical groove and locking lever looks joint on the circular piece, the locking lever can prevent that the clamping lever from relieving the joint with the draw-in groove by oneself, and locking lever and logical groove cooperate can make the circular piece can not rotate by oneself.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle mounting mechanism.
Fig. 2 is an enlarged schematic view of a portion a of fig. 1.
Fig. 3 is a schematic side view of the circular block of fig. 2.
In the figure: 1. a mounting rack; 2. mounting the equipment body; 3. an unmanned aerial vehicle body; 4. a bracket; 5. a locking lever; 6. a circular block; 7. a pull ring; 8. a clamping rod; 9. a mounting block; 10. a first spring; 11. a limit rod; 12. and a second spring.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only 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.
Referring to fig. 1 to 3, the present utility model provides a technical solution:
the utility model provides an unmanned aerial vehicle mounting mechanism, including unmanned aerial vehicle body 3, unmanned aerial vehicle body 3's bottom both sides are all fixed and are equipped with support 4, unmanned aerial vehicle body 3's bottom is provided with mount 1, mount 1's bottom is fixed and is equipped with mount equipment body 2 mount 1 and set up to the U-shaped, the mounting groove has all been seted up to mount 1's upper end both sides, all slide in two mounting grooves and be equipped with installation piece 9, the upper end of installation piece 9 all with unmanned aerial vehicle body 3's lower extreme fixed connection, the slide hole has all been seted up to one side cell wall that two mounting grooves deviate from mutually, the slide is equipped with draw-in bar 8 in the slide hole, the one end of draw-in bar 8 extends to the mounting groove in, the draw-in groove with draw-in bar 8 matched with is seted up to installation piece 9's lateral wall.
The bar wall of the clamping rod 8 is provided with a bar hole, the bar hole is internally fixed with a propping mechanism, the propping mechanism comprises a limiting rod 11, the limiting rod 11 is arranged at one side of the bar hole close to the circular block 6 in a sliding manner, two ends of the limiting rod 11 are fixedly connected with the wall of the sliding hole, and the bar wall of the limiting rod 11 is far away from one side of the circular block 6, and is fixedly connected with a first spring 10.
One end of the clamping rod 8 positioned in the sliding hole is rotationally connected with a circular block 6 through a rotating shaft, the other end of the circular block 6 extends to the outside of the sliding hole, one end of the circular block 6 extending to the outside of the sliding hole is fixedly connected with a pull ring 7, and the pull ring 7 is convenient for pulling the circular block 6.
Round grooves are formed in the walls of the upper side and the lower side of the sliding hole respectively, a locking mechanism is fixedly arranged in each of the two round grooves, each locking mechanism comprises a locking rod 5, each locking rod 5 is slidably arranged in each round groove, one end of each locking rod 5 extends to the outside of each round groove, through grooves matched with the corresponding locking rods 5 are formed in the side walls of the round blocks 6, second springs 12 are fixedly arranged at the bottoms of the grooves, spherical surfaces are formed in one ends of the locking rods 5 located outside the corresponding round grooves, and the first springs 10 and the second springs 12 are always in a compressed state.
When the mounting frame 1 is installed, 90-degree rotation pull ring 7, pull ring 7 drive circular piece 6 rotate, simultaneously circular piece 6 is gone up logical groove with locking lever 5 ejecting, circular piece 6 no longer is locked this moment, pulling pull ring 7 can be through circular piece 6 pulling clamping lever 8, in installing block 9 card income mounting groove, loosen pull ring 7, first spring 10 promotes clamping lever 8 card income clamping groove on the installing block 9, 90-degree rotation pull ring 7 once more, pull ring 7 drives logical groove and locking lever 5 looks joint on the circular piece 6, locking lever 5 can prevent clamping lever 8 from releasing the joint with the draw-in groove by oneself, and locking lever 5 and logical groove cooperate can make circular piece 6 can not rotate by oneself.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides an unmanned aerial vehicle mounting mechanism, includes unmanned aerial vehicle body (3), its characterized in that: the utility model provides a mounting device for unmanned aerial vehicle, includes unmanned aerial vehicle body (3), bottom both sides of unmanned aerial vehicle body (3) are all fixed be equipped with support (4), the bottom of unmanned aerial vehicle body (3) is provided with mount (1), the bottom of mount (1) is fixed be equipped with mount equipment body (2) mount (1) set up to the U-shaped, the mounting groove has all been seted up to the upper end both sides of mount (1), two equal sliding in the mounting groove is equipped with installation piece (9), the upper end of installation piece (9) all with the lower extreme fixed connection of unmanned aerial vehicle body (3), two the slide hole has all been seted up to one side cell wall that the installation groove deviates from mutually, the slide is downthehole slip be equipped with draw-in bar (8), the one end of draw-in bar (8) extends to the mounting groove in, the bar wall of installation piece (9) has been seted up the bar hole, bar downthehole fixed being equipped with supports tight mechanism, one end that draw-in bar (8) is located in the downthehole one end through rotating block (6), the round hole extension of both sides all has round hole extension (6), round extension mechanism (6) is equipped with the round hole extension.
2. The unmanned aerial vehicle mounting mechanism of claim 1, wherein: the supporting and tightening mechanism comprises a limiting rod (11), the limiting rod (11) is arranged in the strip-shaped hole in a sliding mode at one side, close to the round block (6), of the limiting rod, two ends of the limiting rod (11) are fixedly connected with the wall of the sliding hole, and a side rod wall, far away from the round block (6), of the rod wall of the limiting rod (11) is fixedly connected with a first spring (10).
3. The unmanned aerial vehicle mounting mechanism of claim 1, wherein: the locking mechanism comprises a locking rod (5), the locking rod (5) is arranged in a circular groove in a sliding mode, one end of the locking rod (5) extends to the outside of the circular groove, a through groove matched with the locking rod (5) is formed in the side wall of the circular block (6), and a second spring (12) is fixedly arranged at the bottom of the circular groove.
4. The unmanned aerial vehicle mounting mechanism of claim 1, wherein: one end of the round block (6) extending to the outside of the sliding hole is fixedly connected with a pull ring (7).
5. A drone mounting mechanism according to claim 3, wherein: one end of the locking rod (5) positioned outside the circular groove is provided with a spherical surface.
6. The unmanned aerial vehicle mounting mechanism of claim 2, wherein: the first spring (10) and the second spring (12) are always in a compressed state.
CN202322181610.3U 2023-08-14 2023-08-14 Unmanned aerial vehicle mounting mechanism Active CN220996778U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202322181610.3U CN220996778U (en) 2023-08-14 2023-08-14 Unmanned aerial vehicle mounting mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202322181610.3U CN220996778U (en) 2023-08-14 2023-08-14 Unmanned aerial vehicle mounting mechanism

Publications (1)

Publication Number Publication Date
CN220996778U true CN220996778U (en) 2024-05-24

Family

ID=91086848

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202322181610.3U Active CN220996778U (en) 2023-08-14 2023-08-14 Unmanned aerial vehicle mounting mechanism

Country Status (1)

Country Link
CN (1) CN220996778U (en)

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