CN214649012U

CN214649012U - Assembled geological mineral exploration unmanned aerial vehicle

Info

Publication number: CN214649012U
Application number: CN202120014075.0U
Authority: CN
Inventors: 李志东
Original assignee: Zhongshan Nuclear Industry Group 214 Brigade Co ltd
Current assignee: Zhongshan Nuclear Industry Group 214 Brigade Co ltd
Priority date: 2021-01-05
Filing date: 2021-01-05
Publication date: 2021-11-09
Anticipated expiration: 2031-01-05

Abstract

The utility model discloses an assembled unmanned aerial vehicle for geological mineral exploration, including fuselage, a plurality of screw, a plurality of bottom support and camera, a plurality of cylindrical grooves have been seted up on the lateral wall of fuselage, the equal threaded connection of every cylindrical groove internal thread has the wing support, the screw rotates to be connected on the lateral wall of wing support, the pinhole has all been seted up on the lateral wall of every bottom support, a plurality of spacing grooves have all been seted up on the lateral wall of fuselage, equal fixedly connected with balance plate on the lateral wall of every bottom support. The utility model discloses a set up stop device and cylindrical groove, when pulling the spacer pin, the limiting plate can compress spacing spring, when the deformation of spacing spring reached certain degree, the spacer pin can deviate from in the pinhole, and then can tear the bottom support off from the fuselage fast; when the wing support is rotated, the wing support can be put into the cylindrical groove, so that the space occupied by the whole unmanned aerial vehicle device is reduced, and the unmanned aerial vehicle device is convenient to carry for a long distance.

Description

Assembled geological mineral exploration unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to an assembled unmanned aerial vehicle for geological mineral exploration.

Background

In recent years, the unmanned aerial vehicle industry has been rapidly developed, and the kinds of unmanned aerial vehicles are continuously derived, so that the unmanned aerial vehicles are closely related to the lives of people.

Drones are commonly used to perform certain specialized tasks, particularly in harsh environments, such as in the field, where geological mineral exploration may be required, and tend to be relatively bulky, as it may require on-site sampling by the drone. But most geology mineral exploration unmanned aerial vehicle can't all carry out the quick split of structure, even can carry out the folding of support or wing a bit, still occupy great space after nevertheless folding to the staff of not being convenient for carries on long-distance. Based on this problem, the utility model provides a solution.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that exists among the prior art, and the assembled unmanned aerial vehicle for geology mineral exploration who proposes.

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

an assembled unmanned aerial vehicle for geological mineral exploration, which comprises a machine body, a plurality of propellers, a plurality of bottom brackets and a camera, a plurality of cylindrical grooves are arranged on the side wall of the machine body, the internal thread of each cylindrical groove is in threaded connection with a wing bracket, the propeller is rotationally connected to the side wall of the wing bracket, the lower end of the fuselage is provided with a plurality of mounting grooves, each bottom bracket is connected in the mounting groove in a sliding way, the side wall of each bottom bracket is provided with a pin hole, a plurality of limiting grooves are arranged on the side wall of the machine body, a limiting device capable of limiting the pin hole is arranged in each limiting groove, the side wall of each bottom bracket is fixedly connected with a balance plate, the lower end of each balance plate is provided with a buffer slot, all install the buffer that can prevent that unmanned aerial vehicle from receiving violent impact in vertical direction in every dashpot.

Preferably, stop device includes the spacer pin of sliding connection in the spacing inslot, along the axis direction cover has spacing spring on the spacer pin, fixedly connected with limiting plate on the lateral wall of spacer pin.

Preferably, the buffer device comprises a buffer block which is slidably connected in the buffer groove, and the buffer block is elastically connected to the inner top of the buffer groove through a buffer spring.

Preferably, the lower extreme of fuselage has been seted up and has been accomodate the groove, accomodate the interior top fixedly connected with magnet in groove, camera sliding connection is in accomodating the inslot, fixedly connected with arm-tie on the lateral wall of camera.

Preferably, one end of the wing support close to the cylindrical groove is fixedly connected with an end baffle, and a stop block is fixedly connected to the inner wall of the cylindrical groove.

Preferably, the distance between the two side walls of the buffer block is slightly smaller than the distance between the two inner walls of the buffer groove, and the thickness of the buffer block is one centimeter.

The utility model discloses following beneficial effect has:

1. by arranging the limiting device and the cylindrical groove, when the limiting pin is pulled, the limiting plate can compress the limiting spring, and when the limiting spring deforms to a certain degree, the limiting pin can be disengaged from the pin hole, so that the bottom support can be quickly detached from the body; when the wing support is rotated, the wing support can be put into the cylindrical groove, so that the space occupied by the whole unmanned aerial vehicle device is reduced, and the unmanned aerial vehicle device is convenient to carry for a long distance;

2. through setting up buffer, when unmanned aerial vehicle descends, under buffer spring's elastic action, the buffer block can produce elastic contact with ground, prevents that unmanned aerial vehicle from leading to the fact the damage to unmanned aerial vehicle owing to strike great when falling to the ground, and this can play the effect of protection to unmanned aerial vehicle to a certain extent.

Drawings

Fig. 1 is a schematic structural view of an assembled unmanned aerial vehicle for geological and mineral exploration, which is provided by the utility model;

fig. 2 is an enlarged schematic view of the structure at a position a of the assembled unmanned aerial vehicle for geological and mineral exploration, provided by the utility model;

fig. 3 is the utility model provides an assembled geology is enlarged schematic diagram of unmanned aerial vehicle's B department for mineral exploration's structure.

In the figure: the aircraft comprises a fuselage 1, a propeller 2, a wing support 3, a bottom support 4, a camera 5, a column-shaped groove 6, a baffle plate 7 at the end part, a stop dog 8, a mounting groove 9, a pin hole 10, a limit groove 11, a limit pin 12, a limit plate 13, a limit spring 14, a balance plate 15, a buffer groove 16, a buffer spring 17, a buffer block 18, a storage groove 19, a magnet 20 and a pull plate 21.

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.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", 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 simplicity of description, and do not indicate or imply that the device or element being 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.

Referring to fig. 1-3, an assembled unmanned aerial vehicle for geological mineral exploration comprises a machine body 1, a plurality of propellers 2, a plurality of bottom supports 4 and a camera 5, wherein a containing groove 19 is formed in the lower end of the machine body 1, a magnet 20 is fixedly connected to the inner top of the containing groove 19, the camera 5 is slidably connected to the containing groove 19, and a pull plate 21 is fixedly connected to the side wall of the camera 5. A plurality of cylindrical grooves 6 are formed in the side wall of the machine body 1, and the inner threads of each cylindrical groove 6 are in threaded connection with the wing support 3. It should be noted that the threaded region on the wing support 3 is only provided near one end of the cylindrical slot 6, which prevents the propeller 2 from squeezing against the fuselage 1. One end of the wing support 3 close to the cylindrical groove 6 is fixedly connected with an end baffle 7, the inner wall of the cylindrical groove 6 is fixedly connected with a stop dog 8, and the propeller 2 is rotatably connected to the side wall of the wing support 3.

A plurality of mounting grooves 9 have been seted up to the lower extreme of fuselage 1, every equal sliding connection of bottom support 4 is in mounting groove 9, pinhole 10 has all been seted up on the lateral wall of every bottom support 4, a plurality of spacing grooves 11 have all been seted up on the lateral wall of fuselage 1, all install in every spacing groove 11 and can carry out spacing stop device to pinhole 10, stop device includes the spacer pin 12 of sliding connection in spacing groove 11, it has spacing spring 14 to overlap along the axis direction on the spacer pin 12, fixedly connected with limiting plate 13 on the lateral wall of spacer pin 12.

Equal fixedly connected with balance plate 15 on the lateral wall of every bottom support 4, buffer slot 16 has all been seted up to the lower extreme of every balance plate 15, all installs the buffer that can prevent that unmanned aerial vehicle from receiving violent impact in vertical direction in every buffer slot 16. The buffer device comprises a buffer block 18 which is slidably connected in the buffer groove 16, and the buffer block 18 is elastically connected to the inner top of the buffer groove 16 through a buffer spring 17. The distance between the two side walls of the buffer block 18 is slightly smaller than the distance between the two inner walls of the buffer groove 16, and the thickness of the buffer block 18 is one centimeter.

In the use process, when the limiting pin 12 is pulled, the limiting plate 13 compresses the limiting spring 14, and when the limiting spring 14 deforms to a certain degree, the limiting pin 12 can be separated from the pin hole 10, so that the bottom bracket 4 can be quickly detached from the machine body 1; when the wing support 3 is rotated, the wing support 3 can be collected into the cylindrical groove 6, so that the space occupied by the whole unmanned aerial vehicle device is reduced; in this way, the bottom bracket can be separated from the fuselage 1, and the wing bracket 3 can be collected in the cylindrical groove 6, so that the integral structure of the unmanned aerial vehicle device can be reduced to a certain extent, and the unmanned aerial vehicle device is convenient to carry for a long distance; when unmanned aerial vehicle descends, under buffer spring 17's elastic action, buffer block 18 can produce elastic contact with ground, prevents that unmanned aerial vehicle from causing the damage to unmanned aerial vehicle owing to assaulting great when falling to the ground, and this can play the effect of protection to unmanned aerial vehicle to a certain extent. In addition, can put into accommodating groove 19 with camera 5, magnet 20 can attract camera 5's metal casing, prevents that camera 5 from accomodating the interior roll-off of groove 19, only needs to pull loose arm-tie 21 alright follow and accomodate the interior roll-off of groove 19 with camera 5 during the use.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. An assembled unmanned aerial vehicle for geological mineral exploration comprises a machine body (1), a plurality of propellers (2), a plurality of bottom supports (4) and a camera (5), and is characterized in that a plurality of cylindrical grooves (6) are formed in the side wall of the machine body (1), a wing support (3) is in threaded connection with the internal thread of each cylindrical groove (6), the propellers (2) are rotatably connected to the side wall of the wing support (3), a plurality of mounting grooves (9) are formed in the lower end of the machine body (1), each bottom support (4) is in sliding connection with the inside of each mounting groove (9), pin holes (10) are formed in the side wall of each bottom support (4), a plurality of limiting grooves (11) are formed in the side wall of the machine body (1), and limiting devices capable of limiting the pin holes (10) are mounted in each limiting groove (11), equal fixedly connected with balance plate (15) on the lateral wall of every bottom support (4), buffer slot (16) have all been seted up to the lower extreme of every balance plate (15), all install the buffer that can prevent that unmanned aerial vehicle from receiving violent impact in vertical direction in every buffer slot (16).

2. The assembled unmanned aerial vehicle for geological mineral exploration according to claim 1, wherein the limiting device comprises a limiting pin (12) slidably connected in a limiting groove (11), a limiting spring (14) is sleeved on the limiting pin (12) along the axial direction, and a limiting plate (13) is fixedly connected to the side wall of the limiting pin (12).

3. The unmanned aerial vehicle for assembled geological mineral exploration according to claim 1, wherein said buffer device comprises a buffer block (18) slidably connected in a buffer tank (16), said buffer block (18) being elastically connected to the inner top of the buffer tank (16) through a buffer spring (17).

4. The assembled unmanned aerial vehicle for geological mineral exploration according to claim 1, wherein a receiving groove (19) is formed in the lower end of the fuselage (1), a magnet (20) is fixedly connected to the inner top of the receiving groove (19), the camera (5) is slidably connected to the receiving groove (19), and a pulling plate (21) is fixedly connected to the side wall of the camera (5).

5. The assembled unmanned aerial vehicle for geological mineral exploration according to claim 1, wherein an end baffle (7) is fixedly connected to one end of the wing support (3) close to the cylindrical groove (6), and a stop block (8) is fixedly connected to the inner wall of the cylindrical groove (6).

6. The assembled unmanned aerial vehicle for geological mineral exploration according to claim 3, wherein the distance between two side walls of said buffer block (18) is slightly smaller than the distance between two inner walls of said buffer tank (16), and the thickness of said buffer block (18) is one centimeter.