CN214296435U - Novel aerial survey unmanned aerial vehicle - Google Patents

Abstract

The utility model relates to a novel aerial survey unmanned aerial vehicle aims at solving the novel aerial survey unmanned aerial vehicle among the current prior art, when unmanned aerial vehicle falls to the ground, can't carry out the cushioning effect to unmanned aerial vehicle, and then leads to the inside original paper of unmanned aerial vehicle to cause the damage easily, and then the technical problem of the normal use of easy unmanned aerial vehicle, including the rectangular board; the top of rectangular plate is equipped with the diaphragm, the equal rigid coupling in top left and right sides of diaphragm has the short piece, the top of straight board is equipped with unmanned aerial vehicle, the below of diaphragm is equipped with buffer, the utility model discloses have the cooperation through rectangular plate, diaphragm, short piece, unmanned aerial vehicle, straight board and buffer, the horizontal pole drives the down tube and rotates, and the down tube stretches first spring, and the horizontal pole compresses the second spring, and then realizes the buffering to the diaphragm, and then realizes the buffering to unmanned aerial vehicle, avoids when unmanned aerial vehicle falls to the ground, can't carry out the cushioning effect to unmanned aerial vehicle, and then leads to the inside original paper of unmanned aerial vehicle to cause the damage, and then leads to unmanned aerial vehicle's normal use.

Description

Novel aerial survey unmanned aerial vehicle

Technical Field

The utility model relates to a novel aerial survey unmanned aerial vehicle especially relates to a novel aerial survey unmanned aerial vehicle.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.

Novel aerial survey unmanned aerial vehicle among the prior art, when unmanned aerial vehicle fell to the ground, can't carry out the cushioning effect to unmanned aerial vehicle, and then lead to the inside original paper of unmanned aerial vehicle to cause the damage easily, and then easy unmanned aerial vehicle's normal use, and the novel aerial survey unmanned aerial vehicle among the prior art, the staff of not being convenient for dismantles the device, and then the staff of not being convenient for maintains and maintains the device, the staff operation of not being convenient for.

Disclosure of Invention

The utility model aims to overcome prior art not enough, adapt to reality needs, provide a novel aerial survey unmanned aerial vehicle to solve the novel aerial survey unmanned aerial vehicle among the current prior art, when unmanned aerial vehicle falls to the ground, can't carry out the cushioning effect to unmanned aerial vehicle, and then lead to the inside original paper of unmanned aerial vehicle to cause the damage easily, and then easy unmanned aerial vehicle's normal use technical problem.

In order to realize the utility model discloses a purpose, the utility model discloses the technical scheme who adopts does:

designing a novel aerial survey unmanned aerial vehicle, which comprises a long plate; the top of long slab is equipped with the diaphragm, the equal rigid coupling in top left and right sides of diaphragm has the short block, the top of short block respectively with the bottom left and right sides fixed connection of straight board, the top of straight board is equipped with unmanned aerial vehicle, the below of diaphragm is equipped with buffer.

The buffer device comprises an inclined rod, a cross rod, a first spring, a second spring, a short rod and a long block.

The bottom of horizontal pole respectively with the top left and right sides fixed connection of long slab, the preceding terminal surface one side of horizontal pole all rotates with the preceding terminal surface one side of down tube through the round pin axle with the opposite side and is connected, the preceding terminal surface opposite side of down tube rotates through round pin axle and preceding terminal surface one side of short rod to be connected, the preceding terminal surface opposite side of short rod rotates through the round pin axle and is connected with the bottom of diaphragm, the one end rigid coupling of down tube has first spring, the other end of first spring and one side and the opposite side fixed connection of long piece, the top of long piece respectively with the bottom left and right sides fixed connection of diaphragm, the bottom recess inner wall rigid coupling of long piece has the second spring, the bottom of second spring and the top fixed connection of horizontal pole.

The long blocks are distributed in an axisymmetric manner by taking the long plate as an axis.

And a moving device is arranged above the straight plate.

The moving device comprises a long rod, a round rod, a first inclined block, a first sliding rod, a curved block and a sliding block.

The bottom of first slide bar and the top left and right sides fixed connection of straight board, the outer wall slip joint of first slide bar has the slider, the top rigid coupling of slider has bent piece, the top rigid coupling of bent piece has first sloping, the one end rigid coupling of first sloping has the round bar, the outer wall one side of round bar and one side recess clearance fit of stock, the top of stock and unmanned aerial vehicle's bottom left and right sides fixed connection, the outer wall below of stock respectively with the left and right sides inner wall clearance fit of straight board.

And a rotating device is arranged above the straight plate.

The rotating device comprises a threaded rod, a second sliding rod, a transverse block, a second inclined block and a square block.

The bottom of second slide bar respectively with the top left and right sides fixed connection of straight board, the outside slip joint of second slide bar has the crossblock, the one end rigid coupling of crossblock has the square, the inner wall threaded connection of square has the threaded rod, the bottom of threaded rod is passed through the bearing and is connected with the top left and right sides rotation of straight board, the one end rigid coupling of square has the second sloping block, one side of second sloping block is laminated with one side of first sloping block mutually.

And a handle is fixedly connected above the outer wall of the threaded rod.

The second sliding rod and the transverse block form a sliding structure.

The beneficial effects of the utility model reside in that:

through the rectangular plate, the diaphragm, the short piece, unmanned aerial vehicle, straight board and buffer, make the device when using, rebound when can be through the rectangular plate atress, the rectangular plate drives the horizontal pole upwards, the horizontal pole drives the down tube and rotates, the down tube is stretched to first spring, the horizontal pole compresses the second spring, and then realize the buffering to the diaphragm, and then realize the buffering to unmanned aerial vehicle, avoid when unmanned aerial vehicle falls to the ground, can't carry out the cushioning effect to unmanned aerial vehicle, and then lead to the inside original paper of unmanned aerial vehicle to cause the damage, and then lead to unmanned aerial vehicle's normal use.

Through the rectangular plate, the diaphragm, the short piece, unmanned aerial vehicle, straight board, mobile device and rotating device's cooperation, make the device when using, can pass through the rotation threaded rod, the threaded rod drives the square rebound, the square drives the second sloping upward movement, outwards stimulate first sloping, first sloping drives the outside removal of round bar, and then make the round bar leave one side recess of stock, and then realize the dismantlement to the device, and then the staff of being convenient for maintains and maintains the device, the staff of being convenient for operates.

Drawings

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

fig. 2 is a schematic view of the threaded rod, the second slide bar and the cross block of the present invention;

fig. 3 is a schematic view of the first sloping block, the second sloping block and the curved block of the present invention;

fig. 4 is a schematic view of the first spring, the second spring and the long block of the present invention.

In the figure: 1. long plate, 2, buffer, 201, down tube, 202, horizontal pole, 203, first spring, 204, second spring, 205, quarter butt, 206, long piece, 3, mobile device, 301, stock, 302, round bar, 303, first sloping block, 304, first slide bar, 305, bent block, 306, slider, 4, rotating device, 401, threaded rod, 402, second slide bar, 403, horizontal block, 404, second sloping block, 405, square, 5, diaphragm, 6, short block, 7, unmanned aerial vehicle, 8, straight plate.

Detailed Description

The invention will be further described with reference to the following figures and examples:

example 1: a novel aerial survey unmanned aerial vehicle comprises a long plate 1; a transverse plate 5 is arranged above the long plate 1, short blocks 6 are fixedly connected to the left side and the right side of the top of the transverse plate 5, the tops of the short blocks 6 are fixedly connected with the left side and the right side of the bottom of the straight plate 8 respectively, an unmanned aerial vehicle 7 is arranged above the straight plate 8, a buffer device 2 is arranged below the transverse plate 5, the buffer device 2 comprises an inclined rod 201, a cross rod 202, a first spring 203, a second spring 204, a short rod 205 and a long block 206, the bottom of the cross rod 202 is fixedly connected with the left side and the right side of the top of the long plate 1 respectively, one side and the other side of the front end surface of the cross rod 202 are rotatably connected with one side of the front end surface of the inclined rod 201 through a pin shaft, the other side of the front end surface of the inclined rod 201 is rotatably connected with one side of the front end surface of the short rod 205 through a pin shaft, the other side of the front end surface of the short rod 205 is rotatably connected with the bottom of the transverse plate 5 through a pin shaft, the short rod 205 can rotate at the bottom of the transverse plate 5 when stressed, one end of the inclined rod 201 is fixedly connected with the first spring 203, first spring 203 gives the opposite power when down tube 201 atress removes all the time, the other end of first spring 203 and one side and the opposite side fixed connection of long piece 206, long piece 206 uses long board 1 to be the axisymmetric distribution as the axle, design like this can play better cushioning effect to unmanned aerial vehicle 7, the top of long piece 206 respectively with the bottom left and right sides fixed connection of diaphragm 5, the bottom recess inner wall rigid coupling of long piece 206 has second spring 204, second spring 204 gives long piece atress removal opposite power all the time, the bottom of second spring 204 and the top fixed connection of horizontal pole 202.

The top of bar 8 is equipped with mobile device 3, mobile device 3 includes stock 301, round bar 302, first sloping block 303, first slide bar 304, bent block 305 and slider 306, the bottom of first slide bar 304 and the top left and right sides fixed connection of bar 8, the outer wall slip joint of first slide bar 304 has slider 306, slider 306 can slide from side to side at first slide bar 304 outer wall during the atress, the top rigid coupling of slider 306 has bent block 305, the top rigid coupling of bent block 305 has first sloping block 303, the one end rigid coupling of first sloping block 303 has round bar 302, outer wall one side and one side recess clearance fit of stock 301 of round bar 302, can move about one side recess of stock 301 when round bar 302 atress, the top of stock 301 and unmanned aerial vehicle 7's bottom left and right sides fixed connection, the outer wall below of stock 301 respectively with the left and right sides inner wall clearance fit of bar 8.

Rotating device 4 is arranged above straight plate 8, rotating device 4 includes threaded rod 401, second slide bar 402, horizontal block 403, second sloping block 404 and square 405, the bottom of second slide bar 402 is respectively with the top left and right sides fixed connection of straight plate 8, the outside slip joint of second slide bar 402 has horizontal block 403, second slide bar 402 constitutes sliding construction with horizontal block 403, horizontal block 403 can slide from top to bottom at the outer wall of second slide bar 402 when atress, the one end rigid coupling of horizontal block 403 has square 405, the inner wall threaded connection of square 405 has threaded rod 401, the outer wall top rigid coupling of threaded rod 401 has the handle, the handle is convenient for the staff to rotate threaded rod 401, the bottom of threaded rod 401 is connected with the top left and right sides of straight plate 8 through the bearing and is rotated, the one end rigid coupling of square 401 has second sloping block 404, one side of second sloping block 404 laminates with one side of first sloping block 303.

Firstly, when the unmanned aerial vehicle 7 lands, the long plate 1 moves upwards when being stressed, the long plate 1 drives the cross rod 202 to move upwards, the cross rod 202 drives the inclined rod 201 to rotate, the inclined rod 201 stretches the first spring 203, the cross rod 202 compresses the second spring 204, further realizing the buffering of the transverse plate 5 and further realizing the buffering of the unmanned aerial vehicle 7, avoiding the incapability of buffering the unmanned aerial vehicle 7 when the unmanned aerial vehicle 7 lands, thereby causing damage to the elements inside the drone 7, and consequently causing normal use of the drone 7, when the device needs to be maintained, the threaded rod 401 is rotated, the threaded rod 401 drives the block 405 to move upwards, the block 405 drives the second inclined block 404 to move upwards, the first inclined block 303 is pulled outwards, the first inclined block 303 drives the round rod 302 to move outwards, and then make round bar 302 leave one side recess of stock 301, and then realize the dismantlement to the device, and then be convenient for the staff to maintain and maintain the device.

The embodiment of the present invention discloses a preferred embodiment, but not limited thereto, and those skilled in the art can easily understand the spirit of the present invention according to the above embodiment, and make different extensions and changes, but do not depart from the spirit of the present invention, all of which are within the protection scope of the present invention.

Claims (6)

1. A novel aerial survey unmanned aerial vehicle comprises a long plate; the method is characterized in that: a transverse plate is arranged above the long plate, short blocks are fixedly connected to the left side and the right side of the top of the transverse plate, the tops of the short blocks are fixedly connected with the left side and the right side of the bottom of the straight plate respectively, an unmanned aerial vehicle is arranged above the straight plate, and a buffer device is arranged below the transverse plate;

the buffer device comprises an inclined rod, a cross rod, a first spring, a second spring, a short rod and a long block;

the bottom of horizontal pole respectively with the top left and right sides fixed connection of long slab, the preceding terminal surface one side of horizontal pole all rotates with the preceding terminal surface one side of down tube through the round pin axle with the opposite side and is connected, the preceding terminal surface opposite side of down tube rotates through round pin axle and preceding terminal surface one side of short rod to be connected, the preceding terminal surface opposite side of short rod rotates through the round pin axle and is connected with the bottom of diaphragm, the one end rigid coupling of down tube has first spring, the other end of first spring and one side and the opposite side fixed connection of long piece, the top of long piece respectively with the bottom left and right sides fixed connection of diaphragm, the bottom recess inner wall rigid coupling of long piece has the second spring, the bottom of second spring and the top fixed connection of horizontal pole.

2. A novel aerial survey drone as claimed in claim 1, characterized in that: the long blocks are distributed in an axisymmetric manner by taking the long plate as an axis.

3. A novel aerial survey drone as claimed in claim 1, characterized in that: a moving device is arranged above the straight plate;

the moving device comprises a long rod, a round rod, a first inclined block, a first sliding rod, a curved block and a sliding block;

the bottom of first slide bar and the top left and right sides fixed connection of straight board, the outer wall slip joint of first slide bar has the slider, the top rigid coupling of slider has bent piece, the top rigid coupling of bent piece has first sloping, the one end rigid coupling of first sloping has the round bar, the outer wall one side of round bar and one side recess clearance fit of stock, the top of stock and unmanned aerial vehicle's bottom left and right sides fixed connection, the outer wall below of stock respectively with the left and right sides inner wall clearance fit of straight board.

4. A novel aerial survey drone as claimed in claim 1, characterized in that: a rotating device is arranged above the straight plate;

the rotating device comprises a threaded rod, a second sliding rod, a transverse block, a second inclined block and a square block;

the bottom of second slide bar respectively with the top left and right sides fixed connection of straight board, the outside slip joint of second slide bar has the crossblock, the one end rigid coupling of crossblock has the square, the inner wall threaded connection of square has the threaded rod, the bottom of threaded rod is passed through the bearing and is connected with the top left and right sides rotation of straight board, the one end rigid coupling of square has the second sloping block, one side of second sloping block is laminated with one side of first sloping block mutually.

5. The novel aerial survey unmanned aerial vehicle of claim 4, wherein: and a handle is fixedly connected above the outer wall of the threaded rod.

6. The novel aerial survey unmanned aerial vehicle of claim 4, wherein: the second sliding rod and the transverse block form a sliding structure.

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