CN218892690U

CN218892690U - Novel unmanned aerial vehicle of support disconnect-type

Info

Publication number: CN218892690U
Application number: CN202223066008.7U
Authority: CN
Inventors: 周旭东
Original assignee: Individual
Current assignee: Sichuan Semefei Technology Co ltd
Priority date: 2022-11-18
Filing date: 2022-11-18
Publication date: 2023-04-21
Anticipated expiration: 2032-11-18

Abstract

The utility model discloses a novel unmanned aerial vehicle with a separated support, which relates to the technical field of unmanned aerial vehicles and comprises an unmanned aerial vehicle main body, wherein a power supply source is fixedly arranged at the top end of the unmanned aerial vehicle main body, a support arm is fixedly arranged at one side of the power supply source, a rotating motor is fixedly arranged at the top end of the support arm, a wing is fixedly arranged at the output end of the rotating motor, shooting equipment is fixedly arranged at the bottom end of the unmanned aerial vehicle main body, and a camera is fixedly arranged at the front end of the shooting equipment. The utility model provides a novel unmanned aerial vehicle with a separated bracket, which supplies power to a rotating motor through a power supply source, then drives a wing to rotate through starting the rotating motor, and lifts a main body of the unmanned aerial vehicle through the rotation of the wing, so that maintenance personnel can conveniently lift the bracket off to maintain the main body of the unmanned aerial vehicle, and further, the unmanned aerial vehicle bracket is effectively and conveniently detached and installed through the arrangement of a sliding groove, a sliding block, the unmanned aerial vehicle bracket, a buckle and a movable shaft.

Description

Novel unmanned aerial vehicle of support disconnect-type

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a novel unmanned aerial vehicle with a separated bracket.

Background

The drone is a drone that is maneuvered with a radio remote control device and a self-contained programming device. Unmanned aerial vehicles can be classified into military and civilian applications according to the field of application. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In civil aspect, the unmanned aerial vehicle and the industrial application are really just needed by the unmanned aerial vehicle; 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, the application of the unmanned aerial vehicle is greatly expanded, and the developed countries are also actively expanding the application of industries and developing unmanned aerial vehicle technologies. The unmanned aerial vehicle support is installed in unmanned aerial vehicle's bottom promptly for be used for supporting unmanned aerial vehicle's part when unmanned aerial vehicle lands or takes off. The following problems exist in the prior art:

1. the existing novel unmanned aerial vehicle with the separated bracket cannot be conveniently detached from the unmanned aerial vehicle, so that when maintenance personnel maintain the unmanned aerial vehicle, the bracket is detached through complicated operation, and the unmanned aerial vehicle is convenient to repair;

2. the novel unmanned aerial vehicle of current support disconnect-type does not have absorbing device, when unmanned aerial vehicle returns to the journey and falls to the ground, leads to unmanned aerial vehicle to fall to the ground unstably, can turn on one's side and damage unmanned aerial vehicle if serious, can reduce unmanned aerial vehicle's practicality like this.

Disclosure of Invention

In order to solve the technical problems, the utility model adopts the following technical scheme:

the utility model provides a novel unmanned aerial vehicle of support disconnect-type, includes the unmanned aerial vehicle main part, the top fixed mounting of unmanned aerial vehicle main part has the power supply, one side fixed mounting of power supply has the support arm, the top fixed mounting of support arm has the rotating electrical machines, the output fixed mounting of rotating electrical machines has the wing, the bottom fixed mounting of unmanned aerial vehicle main part has shooting equipment, the front end fixed mounting of shooting equipment has the camera, the sliding tray has been seted up to the bottom of unmanned aerial vehicle main part, the sliding block has been placed to the internal surface of sliding tray, the bottom fixed mounting of sliding block has the unmanned aerial vehicle support, the bottom of unmanned aerial vehicle main part is provided with the buckle, one side middle part movable mounting of buckle has the loose axle.

The technical scheme of the utility model is further improved as follows: the utility model discloses a unmanned aerial vehicle support, including unmanned aerial vehicle support, connecting rod, damping spring, movable block, wear pad, the both sides fixed mounting has the connecting rod around unmanned aerial vehicle support bottom, damping spring's bottom fixed mounting has damping spring, damping spring's bottom fixed mounting has the movable block, the bottom fixed mounting of movable block has the wear pad.

The technical scheme of the utility model is further improved as follows: the sliding grooves are four in number, and the four sliding grooves are respectively formed in four corners of the bottom end of the unmanned aerial vehicle main body.

The technical scheme of the utility model is further improved as follows: the buckle is square, the buckle setting is located the below of sliding tray in the bottom of unmanned aerial vehicle main part.

The technical scheme of the utility model is further improved as follows: the connecting rods are four in number, and the four connecting rods are respectively fixed on the front side and the rear side of the bottom ends of the two unmanned aerial vehicle supports.

The technical scheme of the utility model is further improved as follows: the movable block is square, and the middle part of the movable block is movably connected with the surface of the connecting rod.

By adopting the technical scheme, compared with the prior art, the utility model has the following technical progress:

1. the utility model provides a novel unmanned aerial vehicle with a separated bracket, which supplies power to a rotating motor through a power supply source, drives a wing to rotate through starting the rotating motor, lifts an unmanned aerial vehicle main body through rotation of the wing, then manually controls the unmanned aerial vehicle main body to photograph and collect data in the sky by using shooting equipment and a camera, and after the endurance time is finished, the unmanned aerial vehicle main body is returned through an automatic return function, then when the unmanned aerial vehicle needs to be maintained, a buckle can be opened through the arrangement of a movable shaft by a maintainer, and then the unmanned aerial vehicle main body can be taken down through the integral forward sliding of the unmanned aerial vehicle main body, wherein the unmanned aerial vehicle main body can be conveniently and quickly taken down through the arrangement of a sliding groove and a sliding block, so that the maintenance personnel can conveniently take down the bracket to maintain the unmanned aerial vehicle main body, and then the unmanned aerial vehicle main body can be effectively and conveniently detached and installed through the arrangement of the sliding groove, the sliding block, the unmanned aerial vehicle main body, the buckle and the movable shaft.

2. The utility model provides a novel unmanned aerial vehicle with a separated bracket, which is characterized in that the front side and the rear side of the unmanned aerial vehicle are provided with the connecting rods, the damping springs and the movable blocks, so that the unmanned aerial vehicle body can be damped during landing, moreover, the phenomenon that the unmanned aerial vehicle body is damaged due to rollover during landing can be effectively avoided, then, the abrasion-resistant pads are arranged at the bottom ends of the movable blocks, the unmanned aerial vehicle body can be effectively prevented from rubbing the unmanned aerial vehicle bracket during landing, the unmanned aerial vehicle bracket is damaged, and furthermore, the service life of the unmanned aerial vehicle bracket can be effectively prolonged, so that a device with damping is realized, and further, the practicability of the device is effectively improved through the arrangement of the connecting rods, the damping springs, the movable blocks and the abrasion-resistant pads.

Drawings

FIG. 1 is a schematic structural view of a novel unmanned aerial vehicle with separated brackets;

FIG. 2 is a schematic diagram of a sliding groove connection of the present utility model;

FIG. 3 is a schematic diagram of a slider connection according to the present utility model;

FIG. 4 is a schematic view of a shock absorbing spring connection in accordance with the present utility model.

In the figure: 1. an unmanned aerial vehicle main body; 2. a power supply; 3. a support arm; 4. a rotating electric machine; 5. a wing; 6. a photographing device; 7. a camera; 8. a sliding groove; 9. a sliding block; 10. an unmanned aerial vehicle bracket; 11. a buckle; 12. a movable shaft; 13. a connecting rod; 14. a damping spring; 15. a movable block; 16. wear-resistant pad.

Detailed Description

The utility model is further illustrated by the following examples:

example 1

As shown in fig. 1-4, the utility model provides a novel unmanned aerial vehicle with separated support, which comprises an unmanned aerial vehicle main body 1, wherein a power supply 2 is fixedly arranged at the top end of the unmanned aerial vehicle main body 1, a support arm 3 is fixedly arranged at one side of the power supply 2, a rotating motor 4 is fixedly arranged at the top end of the support arm 3, a wing 5 is fixedly arranged at the output end of the rotating motor 4, a shooting device 6 is fixedly arranged at the bottom end of the unmanned aerial vehicle main body 1, a camera 7 is fixedly arranged at the front end of the shooting device 6, a sliding groove 8 is formed in the bottom end of the unmanned aerial vehicle main body 1, a sliding block 9 is arranged on the inner surface of the sliding groove 8, an unmanned aerial vehicle support 10 is fixedly arranged at the bottom end of the sliding block 9, a buckle 11 is arranged at the bottom end of the unmanned aerial vehicle main body 1, and a movable shaft 12 is movably arranged at one side middle part of the buckle 11.

In this embodiment, supply power for rotating electrical machines 4 through power supply 2, then drive wing 5 through starting rotating electrical machines 4 and rotate, rethread wing 5's rotation rises unmanned aerial vehicle main part 1, then utilize shooting equipment 6 and camera 7 to take a photograph in the sky through artifical unmanned aerial vehicle main part 1 of control, after the time of endurance is over, return to the air through unmanned aerial vehicle main part 1's automatic function of returning to the air, then when the rethread unmanned aerial vehicle needs to maintain, can open buckle 11 through the setting of loose axle 12 through the maintenance personal, then through taking off unmanned aerial vehicle support 10 whole forward slip, wherein through the setting of sliding tray 8 and sliding block 9, can convenient and fast take off unmanned aerial vehicle support 10, thereby make things convenient for the maintenance personal to lift off the support and maintain unmanned aerial vehicle main part 1, and then through sliding tray 8, sliding block 9, unmanned aerial vehicle support 10, buckle 11 and loose axle 12's setting, effectual convenience is with unmanned aerial vehicle support 10 dismantlement and installation.

Example 2

As shown in fig. 1-4, on the basis of embodiment 1, the present utility model provides a technical solution: preferably, the front and back both sides fixed mounting of unmanned aerial vehicle support 10 bottom has connecting rod 13, and the bottom fixed mounting of connecting rod 13 has damping spring 14, and damping spring 14's bottom fixed mounting has movable block 15, and movable block 15's bottom fixed mounting has wear pad 16.

In this embodiment, through having set up connecting rod 13, damping spring 14 and movable block 15 in unmanned aerial vehicle support 10's front and back both sides, can play the absorbing effect to unmanned aerial vehicle main part 1 when falling to the ground, moreover can effectually avoid unmanned aerial vehicle main part 1 to appear turning on one's side and lead to unmanned aerial vehicle main part 1's damage phenomenon when falling to the ground, then through having set up wear pad 16 in movable block 15's bottom, can effectually prevent unmanned aerial vehicle main part 1 to produce friction to unmanned aerial vehicle support 10 when falling to the ground, damage unmanned aerial vehicle support 10, moreover can effectually improve unmanned aerial vehicle support 10's life, thereby realized having the absorbing device, and then through connecting rod 13, damping spring 14, movable block 15 and wear pad 16's setting, effectually improved the practicality of device.

The working principle of the novel unmanned aerial vehicle with the separated bracket is specifically described below.

As shown in fig. 1-4, when using, supply power for rotating electrical machines 4 through power supply 2, then drive wing 5 through starting rotating electrical machines 4 and rotate, rethread wing 5's rotation rises unmanned aerial vehicle main part 1, then utilize shooting equipment 6 and camera 7 to take a photograph in the sky through artifical unmanned aerial vehicle main part 1 of control, after the time of endurance is over, return to the air through unmanned aerial vehicle main part 1's automatic function of returning to the air, then when rethread unmanned aerial vehicle needs maintenance, can open buckle 11 through the setting of loose axle 12, then through taking off unmanned aerial vehicle support 10 whole forward slip, wherein through the setting of sliding tray 8 and sliding block 9, can convenient and fast take off unmanned aerial vehicle support 10, thereby make things convenient for the maintenance personnel to lift the support off and maintain unmanned aerial vehicle main part 1, and then through sliding tray 8, sliding block 9, unmanned aerial vehicle support 10, buckle 11 and loose axle 12's setting, effectual convenience is with unmanned aerial vehicle support 10 dismantlement installation.

When unmanned aerial vehicle returns to the ground, through having set up connecting rod 13, damping spring 14 and movable block 15 in the front and back both sides of unmanned aerial vehicle support 10, can play the absorbing effect to unmanned aerial vehicle main part 1 when the ground, moreover can effectually avoid unmanned aerial vehicle main part 1 to appear turning on one's side and lead to unmanned aerial vehicle main part 1's damage phenomenon when the ground, then through having set up wear pad 16 in movable block 15's bottom, can effectually prevent unmanned aerial vehicle main part 1 and produce the friction to unmanned aerial vehicle support 10 when the ground, damage to unmanned aerial vehicle support 10, moreover can effectually improve unmanned aerial vehicle support 10's life, thereby realized having the absorbing device, and then through connecting rod 13, damping spring 14, movable block 15 and wear pad 16's setting, the effectual practicality that improves the device.

The foregoing utility model has been generally described in great detail, but it will be apparent to those skilled in the art that modifications and improvements can be made thereto. Accordingly, it is intended to cover modifications or improvements within the spirit of the inventive concepts.

Claims

1. The utility model provides a novel unmanned aerial vehicle of support disconnect-type, includes unmanned aerial vehicle main part (1), its characterized in that: the intelligent unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein a power supply source (2) is fixedly arranged at the top end of the unmanned aerial vehicle body (1), a supporting arm (3) is fixedly arranged at one side of the power supply source (2), a rotating motor (4) is fixedly arranged at the top end of the supporting arm (3), a wing (5) is fixedly arranged at the output end of the rotating motor (4), a shooting device (6) is fixedly arranged at the bottom end of the unmanned aerial vehicle body (1), a camera (7) is fixedly arranged at the front end of the shooting device (6), a sliding groove (8) is formed in the bottom end of the unmanned aerial vehicle body (1), a sliding block (9) is arranged on the inner surface of the sliding groove (8), an unmanned aerial vehicle support (10) is fixedly arranged at the bottom end of the sliding block (9), a buckle (11) is arranged at the bottom end of the unmanned aerial vehicle body (1), and a movable shaft (12) is movably arranged at one side middle part of the buckle (11).

2. The novel unmanned aerial vehicle with separated brackets according to claim 1, wherein: the unmanned aerial vehicle support comprises an unmanned aerial vehicle support body, and is characterized in that connecting rods (13) are fixedly mounted on the front side and the rear side of the bottom end of the unmanned aerial vehicle support body (10), damping springs (14) are fixedly mounted on the bottom ends of the connecting rods (13), movable blocks (15) are fixedly mounted on the bottom ends of the damping springs (14), and wear-resisting pads (16) are fixedly mounted on the bottom ends of the movable blocks (15).

3. The novel unmanned aerial vehicle with separated brackets according to claim 1, wherein: the number of the sliding grooves (8) is four, and the four sliding grooves (8) are respectively formed in four corners of the bottom end of the unmanned aerial vehicle main body (1).

4. The novel unmanned aerial vehicle with separated brackets according to claim 1, wherein: the buckle (11) is square, and the buckle (11) is arranged at the bottom of the unmanned aerial vehicle main body (1) and is positioned below the sliding groove (8).

5. The novel unmanned aerial vehicle with separated brackets according to claim 2, wherein: the four connecting rods (13) are arranged in total, and the four connecting rods (13) are respectively fixed on the front side and the rear side of the bottom ends of the two unmanned aerial vehicle brackets (10).

6. The novel unmanned aerial vehicle with separated brackets according to claim 2, wherein: the movable block (15) is square, and the middle part of the movable block (15) is movably connected with the surface of the connecting rod (13).