CN217673255U

CN217673255U - Unmanned aerial vehicle shoots device with protection machanism

Info

Publication number: CN217673255U
Application number: CN202220123391.6U
Authority: CN
Inventors: 司艳红; 任伏虎; 黄飞跃; 许燕燕; 龙家俊; 汪凯
Original assignee: Zhongke Yunyao Dongguan Technology Co ltd
Current assignee: Zhongke Yunyao Dongguan Technology Co ltd
Priority date: 2022-01-18
Filing date: 2022-01-18
Publication date: 2022-10-28
Anticipated expiration: 2032-01-18

Abstract

The utility model discloses an unmanned aerial vehicle shoots device with protection machanism relates to unmanned aerial vehicle and shoots the field, the device comprises a device body, the positive symmetrical fixedly connected with wing of the device body top left and right sides, the front of wing is provided with the protecting crust, the window has been seted up in the positive centre of protecting crust, the left and right sides symmetry of window is provided with the reinforcement piece, two positive symmetrical threaded connection of reinforcement piece have the bolt, the left and right sides symmetry of bolt is provided with the extension piece, the spout has been seted up to the positive symmetry of two extension piece back of the body one side of mutually the back, two relative lateral symmetries of spout are provided with logical groove, two front and the back that lead to the inslot chamber are symmetrical and are provided with the movable block, the side fixedly connected with slider of movable block. An unmanned aerial vehicle shoots device with protection machanism, this device can protect camera department, avoids leading to damaging because the collision, and when meetting the striking again, can effectively reduce the impact, avoids damaging.

Description

Unmanned aerial vehicle shoots device with protection machanism

Technical Field

The utility model relates to an unmanned aerial vehicle shoots the field, in particular to unmanned aerial vehicle shoots device with protection machanism.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, is a general name of an unmanned aerial vehicle in fact, and can be divided into several categories of unmanned helicopters, unmanned fixed-wing aircrafts, unmanned multi-rotor aircrafts, unmanned airships and unmanned umbrella-wing aircrafts from the technical perspective.

In chinese utility model patent application no: CN202121040954.7 discloses an unmanned aerial vehicle shoots device with protection machanism, including unmanned aerial vehicle body, shock attenuation spare and protection piece, base fixed connection in the supporting shoe bottom, the protection piece includes guard plate, support bar, third spring and limiting plate, support bar symmetry fixed connection in unmanned aerial vehicle body one side, guard plate sliding connection in between the support bar, limiting plate sliding connection in unmanned aerial vehicle body one side, just the limiting plate bottom with the guard plate laminating, this device can not protect unmanned aerial vehicle's front, the back and top, bottom, and the spring is not damping spring, causes secondary damage to unmanned aerial vehicle easily.

Therefore, it is necessary to provide a drone shooting device with a protection mechanism to solve the above problems.

SUMMERY OF THE UTILITY MODEL

The utility model discloses a main aim at provides an unmanned aerial vehicle shoots device with protection machanism can effectively solve the problem in the background art.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides an unmanned aerial vehicle shoots device with protection machanism, includes the device body, the positive symmetrical fixedly connected with wing of the device body top left and right sides, the front of wing is provided with the protecting crust, the window has been seted up in the positive centre of protecting crust, the left and right sides symmetry of window is provided with reinforcing block, two reinforcing block positive centre symmetrical threaded connection has the bolt, the left and right sides symmetry of bolt is provided with the extension piece, two the spout has been seted up to the centre symmetry of the back one side of the back of the body of the extension piece back of the body one side opposite, two the bilateral symmetry that the spout is relative is provided with logical groove, two it is provided with the movable block to lead to the front and the back symmetry of groove inner chamber, the side fixedly connected with slider of movable block, the one end of slider is provided with first damping spring, the top and the bottom symmetrical fixedly connected with first fixed column of movable block, the activity groove has seted up in the centre of first fixed column one end, the inner chamber of activity groove is provided with the elasticity post, the one end fixedly connected with second damping spring of extension piece, the one end fixedly connected with second damping spring.

Preferably, two reinforcing block symmetry fixed connection is in the centre at the protective housing left and right sides back, reinforcing block passes through bolt fixed connection in the front of device body, the window has five, every the window symmetry is seted up in the protective housing front, top, bottom and left and right sides.

Preferably, the two lengthening blocks are symmetrically and fixedly connected to the left side and the right side of the device body, and the through grooves are symmetrically formed in the inner cavities of the two lengthening blocks.

Preferably, the movable block is matched with the through groove in size, the sliding block is matched with the sliding groove in size, the movable block is movably connected into the inner cavity of the through groove, the sliding block is movably connected into the inner cavity of the sliding groove, the number of the first damping springs is two, and the front and the back of the first damping springs are symmetrically and fixedly connected to one side, opposite to the movable block, of the left side and the right side.

Preferably, the number of the first fixed columns is eight, the left side is four, the first fixed columns are symmetrically and fixedly connected to the top portions and the bottom portions of the two movable blocks on the left side in a back-to-back mode, the right side is four, the first fixed columns are symmetrically and fixedly connected to the top portions and the bottom portions of the two movable blocks on the right side in a back-to-back mode, and the elastic columns are movably connected to the inner cavity of the first fixed columns through the movable grooves.

Preferably, the number of the second fixing columns is eight, the right side is four, the second fixing columns are symmetrically and fixedly connected to the back of the top and the bottom of the right side lengthened block, the left side is four, the second fixing columns are symmetrically and fixedly connected to the back of the top and the bottom of the left side lengthened block, and the other end of the second damping spring is fixedly connected to the outer wall of the first fixing column.

Advantageous effects

Compared with the prior art, the utility model discloses following beneficial effect has:

1. this unmanned aerial vehicle shooting device with protection machanism through the bolt that sets up, can fix the reinforcement piece in the front of device body to this can fix the protective housing in the front of device body, can play the protective effect for the camera of device body through the protective housing that sets up, in order to avoid being collided by debris and lead to damaging on the way in flight, through a plurality of windows that set up, makes the protective housing can not shelter from the shooting sight of camera.

2. This unmanned aerial vehicle shooting device with protection machanism through the movable block that sets up, receives when the collision at the front or the back of device body, and the movable block can drive the slider and remove to the inner chamber of spout, and the movable block can play the cushioning effect through the first damping spring that sets up this moment to this reduces the damage that causes the device body.

3. This unmanned aerial vehicle shooting device with protection machanism through the elastic column that sets up, receives the collision at the top of device body or bottom, and the elastic column can be pushed away to the inner chamber of first fixed column through the movable groove to this reduces the collision that top and bottom received, drives first fixed column when removing at the movable block, can reduce the impact of first fixed column and second fixed column through the second damping spring that sets up, avoids the damage of structure.

Drawings

FIG. 1 is a front schematic view of the present invention;

FIG. 2 is an enlarged view of the present invention at A in FIG. 1;

fig. 3 is a schematic structural diagram of the inner cavity of the protective shell of the present invention.

In the figure: 1. a device body; 2. an airfoil; 3. a protective shell; 4. a window; 5. a reinforcing block; 6. a bolt; 7. lengthening the block; 8. a chute; 9. a through groove; 10. a movable block; 11. a slider; 12. a first damping spring; 13. a first fixed column; 14. a movable groove; 15. an elastic column; 16. a collision mass; 17. a second damping spring; 18. and a second fixing column.

Detailed Description

In order to make the utility model realize, the technical means, the creation characteristics, the achievement purpose and the efficacy are easy to understand and understand, the utility model is further explained by combining the specific implementation mode.

As shown in fig. 1-3, an unmanned aerial vehicle shooting device with a protection mechanism comprises a device body 1, wings 2 are symmetrically and fixedly connected to the centers of the left side and the right side of the top of the device body 1, a protection shell 3 is arranged on the front surface of each wing 2, a window 4 is arranged in the center of the front surface of each protection shell 3, reinforcing blocks 5 are symmetrically arranged on the left side and the right side of each window 4, bolts 6 are symmetrically and symmetrically connected to the centers of the back surfaces of the left side and the right side of each protection shell 3 through screws 6, five windows 4 are arranged on the front surface of the device body 1, each window 4 is symmetrically arranged on the front surface, the top part, the bottom part and the left side of each protection shell 3, lengthening blocks 7 are symmetrically arranged on the left side and the right side of each bolt 6, sliding grooves 8 are symmetrically arranged on the centers of the opposite sides of the two lengthening blocks 7, through grooves 9 are symmetrically arranged on one side of the two sliding grooves 8, two lengthening blocks 7 are symmetrically and fixedly connected to the left side and the right side of a device body 1, two through grooves 9 are symmetrically arranged in inner cavities of the two lengthening blocks 7, movable blocks 10 are symmetrically arranged on the front sides and the back sides of the inner cavities of the two through grooves 9, slide blocks 11 are fixedly connected to the side edges of the movable blocks 10, one ends of the slide blocks 11 are provided with first damping springs 12, the movable blocks 10 are matched with the through grooves 9 in size, the slide blocks 11 are matched with the slide grooves 8 in size, the movable blocks 10 are movably connected in the inner cavities of the through grooves 9, the slide blocks 11 are movably connected in the inner cavities of the slide grooves 8, the number of the first damping springs 12 is two, the front sides and the back sides of the two first damping springs 12 are symmetrically and fixedly connected to one sides of the movable blocks 10 on the left side and the right side, the tops and the bottoms of the movable blocks 10 are symmetrically and fixedly connected with first fixing columns 13, and a movable groove 14 is arranged in the center of one end of the first fixing columns 13, an inner cavity of the movable groove 14 is provided with eight elastic columns 15, eight first fixed columns 13 are arranged, four first fixed columns 13 on the left side are symmetrically and fixedly connected to one side of the two movable blocks 10 on the left side, which are back to back, symmetrically and fixedly connected to one side of the two movable blocks 10 on the right side, which are back to back, the elastic columns 15 are movably connected in the inner cavity of the first fixed columns 13 through the movable groove 14, one end of each elastic column 15 is fixedly connected with a collision block 16, the top and the bottom of the lengthened block 7 are symmetrically and fixedly connected with a second damping spring 17, one end of each second damping spring 17 is fixedly connected with a second fixed column 18, eight second fixed columns 18 are arranged, four second fixed columns 18 on the right side are symmetrically and fixedly connected to one side of the right lengthened block 7, which is back to back, and four second fixed columns 18 on the left side are symmetrically and fixedly connected to one side of the top and the back to back of the left lengthened block 7, the other end of the second damping spring 17 is fixedly connected to the outer wall of the first fixing column 13, the reinforcing block 5 can be fixed on the front surface of the device body 1 through the arranged bolt 6, so that the protective shell 3 can be fixed on the front surface of the device body 1, the protective effect can be achieved for the camera of the device body 1 through the arranged protective shell 3, and the damage caused by the collision of sundries in the flying process is avoided, the protective shell 3 can not block the shooting sight of the camera through the arranged windows 4, when the front surface or the back surface of the device body 1 is collided, the movable block 10 can drive the sliding block 11 to move towards the inner cavity of the sliding groove 8, at the moment, the movable block 10 can play a damping role through the arranged first damping spring 12, so that the damage to the device body 1 is reduced, and when the top or the bottom of the device body 1 is collided through the arranged elastic column 15, the elastic column 15 can be pushed to the inner cavity of the first fixed column 13 through the movable groove 14, so that the collision between the top and the bottom is reduced, and when the movable block 10 drives the first fixed column 13 to move, the impact force between the first fixed column 13 and the second fixed column 18 is reduced through the arranged second damping spring 17, and the damage of the structure is avoided.

It should be noted that, the utility model relates to an unmanned aerial vehicle shoots device with protection machanism, to consolidate 5 through bolt 6 fixing in the front of device body 1 during the use, a plurality of windows of camera accessible 4 of device body 1 carry out the omnidirectional and shoot this moment, when the top or the bottom of device body 1 receive the striking, impact block 16 can drive elastic column 15 and remove to the inner chamber of first fixed column 13 through movable groove 14, reduce the impact with this, when the front and the back of device body 1 receive the striking, movable block 10 can drive slider 11 and remove to the inner chamber of spout 8, can reduce the impact through first damping spring 12 this moment, play the protecting effect with this.

The foregoing shows and describes the basic principles and principal features of the invention, together with the advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides a device is shot to unmanned aerial vehicle with protection machanism, includes device body (1), its characterized in that: the device comprises a device body (1), wings (2) are fixedly and symmetrically connected to the center of the left side and the right side of the top of the device body (1), a protective shell (3) is arranged on the front of each wing (2), a window (4) is formed in the front center of each protective shell (3), reinforcing blocks (5) are symmetrically arranged on the left side and the right side of each window (4), a bolt (6) is connected to the front center of each reinforcing block (5) in a threaded manner, elongated blocks (7) are symmetrically arranged on the left side and the right side of each bolt (6), sliding grooves (8) are symmetrically formed in the center of one side, opposite to each other, of each elongated block (7), through grooves (9) are symmetrically formed in one side, movable blocks (10) are symmetrically arranged on the front side and the back side of each elongated block (7), a first damping spring (12) is arranged at one end of each sliding block (11), first damping springs (13) are symmetrically and fixedly connected to the top and the bottom of each movable block (10), a movable groove (14) is formed in the center of one end of each first fixed column (13), a second damping spring (15) is symmetrically connected to one end of each elongated block (17), one end of the second damping spring (17) is fixedly connected with a second fixing column (18).

2. The unmanned aerial vehicle shooting device with the protection mechanism of claim 1, characterized in that: two reinforcing block (5) symmetry fixed connection is in the centre at the protecting crust (3) left and right sides back, reinforcing block (5) pass through bolt (6) fixed connection in the front of device body (1), window (4) have five, every window (4) symmetry is seted up in protecting crust (3) front, top, bottom and left and right sides.

3. The unmanned aerial vehicle shooting device with the protection mechanism of claim 1, characterized in that: two lengthening blocks (7) are symmetrically and fixedly connected to the left side and the right side of the device body (1), and the through grooves (9) are symmetrically arranged in the inner cavities of the two lengthening blocks (7).

4. The unmanned aerial vehicle shooting device with the protection mechanism of claim 1, characterized in that: the size looks adaptation of movable block (10) and logical groove (9), the size looks adaptation of slider (11) and spout (8), movable block (10) swing joint is in the inner chamber that leads to groove (9), slider (11) swing joint is in the inner chamber of spout (8), first damping spring (12) have two, two the front and the symmetrical fixed connection in left and right sides movable block (10) relative one side of back of first damping spring (12).

5. The unmanned aerial vehicle shooting device with the protection mechanism of claim 1, characterized in that: first fixed column (13) have eight, and the left side is four first fixed column (13) symmetry fixed connection is in the one side that back of the body was carried on the back in two movable block (10) tops in the left side and bottom, and the right side is four first fixed column (13) symmetry fixed connection is in the one side that back of the body was carried on the back in two movable block (10) tops in the right side and bottom, elasticity post (15) are through activity groove (14) swing joint in the inner chamber of first fixed column (13).

6. The unmanned aerial vehicle shooting device with the protection mechanism of claim 1, characterized in that: the number of the second fixing columns (18) is eight, the number of the second fixing columns (18) on the right side is four, the second fixing columns (18) are symmetrically and fixedly connected to one side, back to back, of the top and the bottom of the right side lengthened block (7), the second fixing columns (18) are symmetrically and fixedly connected to one side, back to back, of the top and the bottom of the left side lengthened block (7), and the other ends of the second damping springs (17) are fixedly connected to the outer wall of the first fixing column (13).