CN216401754U

CN216401754U - Durable type delivery unmanned aerial vehicle

Info

Publication number: CN216401754U
Application number: CN202023247398.9U
Authority: CN
Inventors: 陈远高
Original assignee: Shenzhen Gaodafei Technology Co ltd
Current assignee: Shenzhen Gaodafei Technology Co ltd
Priority date: 2020-12-29
Filing date: 2020-12-29
Publication date: 2022-04-29
Anticipated expiration: 2030-12-29

Abstract

The utility model discloses a durable goods-delivery unmanned aerial vehicle, in particular to the technical field of unmanned aerial vehicles, which comprises a vehicle body, a plurality of arms horizontally arranged on the vehicle body and rotor wing assemblies arranged on the arms; a bearing mechanism for bearing the goods is arranged below the machine body and is detachably connected with the machine body through a connecting structure; a base plate is fixed at the bottom of the bearing part, a plurality of grooves are uniformly formed in the lower end of the base plate, each groove is provided with a rubber block which is connected with the groove in a sliding mode, and the rubber blocks are fixed with the grooves through first elastic pieces; when the unmanned aerial vehicle body lands, the wear-resistant rubber plate can prevent the bottom of the bearing mechanism from being worn, and the first elastic piece and the rubber block are matched to play a role in buffering during landing, so that the unmanned aerial vehicle body is more durable; in addition, this bearing mechanism can dismantle with unmanned aerial vehicle and be connected, has improved the flexibility, has simple structure reasonable, convenient to use's characteristics.

Description

Durable type delivery unmanned aerial vehicle

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a durable goods delivery unmanned aerial vehicle.

Background

Unmanned aircraft, also called "drone" for short, is an unmanned aircraft operated by means of radio remote control devices and self-contained program control devices, or autonomously operated by an on-board computer, either completely or intermittently. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and 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 developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

At present, the unmanned aerial vehicle for transporting goods is used for enabling the goods box to be easily scratched along with friction between the goods box and the ground due to the fact that the goods box is generally contacted with the ground when the goods are placed, and therefore the goods box is easy to damage due to the fact that the unmanned aerial vehicle is used for multiple times.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a durable goods delivery unmanned aerial vehicle, which aims to solve at least one of the defects in the prior art.

In order to achieve the purpose, the utility model provides the following technical scheme: a durable goods-delivery unmanned aerial vehicle comprises a body, a plurality of arms horizontally arranged on the body and rotor wing assemblies arranged on the arms;

a bearing mechanism for bearing goods is arranged below the machine body, and the bearing mechanism is detachably connected with the machine body through a connecting structure;

the bearing mechanism is provided with a bearing part and an enclosing structure vertically arranged around the bearing part;

the bottom of bearing part is fixed with the backing plate, the backing plate lower extreme is evenly opened has a plurality of recess, all have rather than equal sliding connection rubber piece on each the recess, the rubber piece pass through first elastic component with the recess is fixed.

In a further improvement of the present invention, an installation portion is fixed to the enclosure structure at an end away from the bearing portion.

In a further improvement of the present invention, the connecting structure has a first connecting portion fixed on the body and a second connecting portion fixed on the mounting portion, and the first connecting portion and the second connecting portion are detachably connected.

The utility model is further improved, the first connecting part is provided with an installation block, a connecting column which is arranged at the bottom of the installation block and is provided with a hollow part, and limiting blocks which are arranged at two sides of the connecting column and are symmetrically arranged; the second connecting portion is provided with a fixing seat, an opening, a limiting portion, a positioning column and a second elastic piece, wherein the opening is formed in the upper end of the fixing seat and used for allowing the limiting block to penetrate, the limiting portion is arranged on one side of the opening and used for allowing the limiting block to be matched and locked, the positioning column is arranged between the openings and fixed to the fixing seat, and the second elastic piece is sleeved on the positioning column.

In a further development of the utility model, the hollow is adapted to the positioning post.

According to the further improvement of the utility model, the limiting block of the first connecting part and the limiting part of the second connecting part can be pressed against each other under the action of the second elastic part.

In a further improvement of the utility model, the backing plate is a wear-resistant rubber plate.

According to the further improvement of the utility model, the enclosure structure is sleeved with the elastic protection piece.

Compared with the prior art, the utility model has at least the following beneficial effects:

the durable goods-delivery unmanned aerial vehicle comprises a vehicle body, a plurality of arms horizontally arranged on the vehicle body and rotor wing assemblies arranged on the arms; a bearing mechanism for bearing goods is arranged below the machine body, and the bearing mechanism is detachably connected with the machine body through a connecting structure; the bearing mechanism is provided with a bearing part and an enclosing structure vertically arranged around the bearing part; a base plate is fixed at the bottom of the bearing part, a plurality of grooves are uniformly formed in the lower end of the base plate, a rubber block is arranged on each groove and is connected with the groove in a sliding mode, and the rubber blocks are fixed with the grooves through the first elastic pieces; through the design, when the unmanned aerial vehicle body lands, the wear-resistant rubber plate can prevent the bottom of the bearing mechanism from being worn, and the first elastic piece and the rubber block are matched to play a role in buffering during the landing, so that the unmanned aerial vehicle body is more durable; in addition, this bearing mechanism can dismantle with unmanned aerial vehicle and be connected, has improved the flexibility, has simple structure reasonable, convenient to use's characteristics.

Drawings

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

FIG. 2 is a schematic illustration of an explosive structure according to the present invention;

FIG. 3 is a partial schematic view of the present invention;

FIG. 4 is an enlarged view of the portion A of FIG. 3 according to the present invention;

FIG. 5 is an enlarged view of the portion B of FIG. 2 according to the present invention;

FIG. 6 is an enlarged view of the portion C of FIG. 2 according to the present invention;

fig. 7 is a partial structural view of the second connecting portion according to the present invention.

In the figure: 1. a body; 2. a horn; 3. a rotor assembly; 4. a carrying mechanism; 401. a bearing part; 402. a fence structure; 403. a base plate; 404. a groove; 405. a rubber block; 406. a first elastic member; 407. an installation part; 408. a guard; 5. a connecting structure; 501. a first connection portion; 502. a second connecting portion; 503. mounting blocks; 504. a hollow part; 505. connecting columns; 506. a limiting block; 507. a fixed seat; 508. an opening; 509. a limiting part; 510. a positioning column; 512. a second elastic member.

Detailed Description

In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention.

Referring to fig. 1 to 7, the technical solution adopted by the present embodiment is as follows: a durable goods-delivery unmanned aerial vehicle is characterized by comprising a vehicle body 1, a plurality of arms 2 horizontally mounted on the vehicle body 1, and rotor wing assemblies 3 mounted on the arms 2; a bearing mechanism 4 for bearing goods is arranged below the machine body 1, and the bearing mechanism 4 is detachably connected with the machine body 1 through a connecting structure 5; the bearing mechanism 4 comprises a bearing part 401 and a surrounding structure 402 vertically arranged around the bearing part 401; a backing plate 403 is fixed at the bottom of the bearing part 401, a plurality of grooves 404 are uniformly formed at the lower end of the backing plate 403, a rubber block 405 is slidably connected with each groove 404, and the rubber block 405 is fixed with the grooves 404 through the first elastic piece 406; the pad 403 is a wear-resistant rubber plate.

However, when the unmanned aerial vehicle body descends, through the backing plate 403 made of wear-resistant rubber, the phenomenon of wearing and tearing can be prevented from appearing in the bottom of the bearing mechanism 4, and through the cooperation of first elastic component 406 and rubber block 405, the effect of buffering can be played when descending, thereby making the unmanned aerial vehicle body more durable.

An installation part 407 is fixed on the enclosure structure 402 and at one end far away from the bearing part 401, the enclosure structure 402 is used for protecting the carried goods so as to play a role of protection, the installation part 407 is plate-shaped and is fixedly arranged at the middle position of the upper end of the enclosure structure 402, the connection structure 5 is provided with a first connection part 501 fixed on the machine body 1 and a second connection part 502 fixed on the installation part 407, and the first connection part 501 is detachably connected with the second connection part 502; the first connecting part 501 is provided with a mounting block 503, a connecting column 505 which is arranged at the bottom of the mounting block 503 and is provided with a hollow part 504, and limiting blocks 506 which are arranged at two sides of the connecting column 505 and are symmetrically arranged; the second connecting portion 502 has a fixing seat 507, an opening 508 disposed at the upper end of the fixing seat 507 for the limiting block 506 to penetrate through, a limiting portion 509 disposed at one side of the opening 508 for the limiting block 506 to be locked in a matching manner, a positioning post 510 disposed between the openings 508 and fixed to the fixing seat 507, and a second elastic member 512 sleeved on the positioning post 510; the hollow portion 504 is matched with the positioning column 510; the limiting block 506 of the first connecting portion 501 and the limiting portion 509 of the second connecting portion 502 can be pressed against each other under the action of the second elastic element 512.

Specifically, when unmanned aerial vehicle and bearing mechanism 4 assemble, aim at opening 508 of second connecting portion 502 through the stopper 506 with first connecting portion 501, and press and block it into, simultaneously, reference column 510 penetrates in the well kenozooecium 504 of spliced pole 505, and second elastic component 512 is held up the outside of pressing at fixing base 507, then through rotating first connecting portion 501, make stopper 506 support and press in the bottom of spacing 509, under the effect of second elastic component 512, make stopper 506 closely support with spacing 509 and press, thereby it is convenient fast to install.

The enclosure structure 402 is sleeved with a flexible shielding member 408, and the shielding member 408 is in close contact with the enclosure structure 402, and the shielding member 408 is detachable and convenient to use.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The detachable installation mode has various modes, for example, a mode of matching with a buckle through plugging, for example, a mode of connecting through a bolt, and the like.

The conception, the specific structure and the technical effects of the present invention are clearly and completely described above in connection with the embodiments and the accompanying drawings, so that the objects, the features and the effects of the present invention can be fully understood. It is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and those skilled in the art can obtain other embodiments without inventive effort based on the embodiments of the present invention, and all embodiments are within the protection scope of the present invention. In addition, all the coupling/connection relationships mentioned herein do not mean that the components are directly connected, but mean that a better coupling structure can be formed by adding or reducing coupling accessories according to specific implementation conditions.

The above embodiments are only for further illustration of the present invention, and should not be construed as limiting the scope of the present invention, and the technical engineers in the art can make insubstantial modifications and adaptations of the present invention based on the above disclosure and disclosure of the utility model.

Claims

1. A durable goods-delivery unmanned aerial vehicle is characterized by comprising a vehicle body (1), a plurality of arms (2) horizontally arranged on the vehicle body (1) and rotor wing assemblies (3) arranged on the arms (2);

a bearing mechanism (4) for bearing goods is arranged below the machine body (1), and the bearing mechanism (4) is detachably connected with the machine body (1) through a connecting structure (5);

the bearing mechanism (4) is provided with a bearing part (401) and a surrounding structure (402) vertically arranged around the bearing part (401);

the bottom of bearing part (401) is fixed with backing plate (403), a plurality of recess (404) have evenly been opened to backing plate (403) lower extreme, all have on each recess (404) rather than equal sliding connection have block rubber (405), block rubber (405) through first elastic component (406) with recess (404) are fixed.

2. A durable delivery drone as claimed in claim 1, wherein: an installation part (407) is fixed at one end of the enclosing structure (402) far away from the bearing part (401).

3. A durable delivery drone as claimed in claim 2, wherein: connection structure (5) have first connecting portion (501) of fixing on fuselage (1) and fix second connecting portion (502) of installation department (407), first connecting portion (501) with second connecting portion (502) can be dismantled and be connected.

4. A durable delivery drone as claimed in claim 3, wherein: the first connecting part (501) is provided with a mounting block (503), a connecting column (505) which is arranged at the bottom of the mounting block (503) and is provided with a hollow part (504), and limiting blocks (506) which are arranged at two sides of the connecting column (505) and are symmetrically arranged; the second connecting portion (502) is provided with a fixing seat (507), an opening (508) which is arranged at the upper end of the fixing seat (507) and used for the limiting block (506) to penetrate through, a limiting portion (509) which is arranged on one side of the opening (508) and used for the limiting block (506) to be matched and locked, a positioning column (510) which is arranged between the openings (508) and fixed with the fixing seat (507), and a second elastic part (512) which is sleeved on the positioning column (510).

5. A durable delivery drone as claimed in claim 4, wherein: the hollow portion (504) is adapted to the positioning post (510).

6. A durable delivery drone according to any one of claims 4 to 5, characterised in that: the limiting block (506) of the first connecting part (501) and the limiting part (509) of the second connecting part (502) can be pressed against each other under the action of the second elastic piece (512).

7. A durable delivery drone as claimed in claim 1, wherein: the backing plate (403) is a wear-resistant rubber plate.

8. A durable delivery drone as claimed in claim 1, wherein: an elastic protection piece (408) is sleeved on the enclosure structure (402).