CN218172576U

CN218172576U - Unmanned aerial vehicle landing leg

Info

Publication number: CN218172576U
Application number: CN202222207953.8U
Authority: CN
Inventors: 吕晋宇; 刘智勇
Original assignee: Shanxi Yuangong General Aviation Technology Co ltd
Current assignee: Shanxi Yuangong General Aviation Technology Co ltd
Priority date: 2022-08-22
Filing date: 2022-08-22
Publication date: 2022-12-30
Anticipated expiration: 2032-08-22

Abstract

The utility model discloses an unmanned aerial vehicle landing leg, in particular to the technical field of unmanned aerial vehicles, which comprises a landing leg and an outer shell, wherein the bottom and one side wall of the outer shell are provided with openings, and the top of the outer shell is provided with a clamping hole and a plurality of connecting holes; an inner tube is arranged in the outer shell, and the inner tube and the outer shell are fixed through screws; the top and the bottom of the inner tube are both provided with openings, the top ends of the supporting legs penetrate through the inner tube and are connected with a limiting plate, and a clamping joint is connected above the limiting plate; the spring is connected with the below of limiting plate, the landing leg cover is established in the spring. The utility model discloses a set up shell body, spring and inner tube, can make limiting plate compression spring through the pulling landing leg when using, make the joint head leave the joint hole, realize the angle change of landing leg, can practice thrift the space, be convenient for unmanned aerial vehicle deposit and transportation.

Description

Unmanned aerial vehicle landing leg

Technical Field

The utility model relates to an unmanned air vehicle technique field, more specifically say, the utility model relates to an unmanned aerial vehicle landing leg.

Background

Along with the development of unmanned aerial vehicle technique, unmanned aerial vehicle's application is also more and more extensive. Because unmanned aerial vehicle has advantages such as unmanned driving, small, mobility are good according to the application, can divide into military use and civilian use. For military use, unmanned aerial vehicles are divided into reconnaissance aircraft and target drone, and the unmanned aerial vehicles and industrial application are really just needed by the unmanned aerial vehicles; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agricultural plant protection, surveying and mapping and the like, and the application of the unmanned aerial vehicle is greatly expanded.

Unmanned aerial vehicle among the prior art is because the supporting leg is mostly rigid connection structure, can't change the angle of landing leg, unmanned aerial vehicle's depositing and transportation of not being convenient for.

SUMMERY OF THE UTILITY MODEL

In order to overcome the above-mentioned defect of prior art, the embodiment of the utility model provides an unmanned aerial vehicle landing leg to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle landing leg comprises a landing leg body and an outer shell body, wherein the bottom and the side wall of one side of the outer shell body are provided with openings, and the top of the outer shell body is provided with a clamping hole and a plurality of connecting holes;

an inner tube is arranged in the outer shell, and the inner tube and the outer shell are fixed through screws;

the top and the bottom of the inner tube are both provided with openings, the top ends of the supporting legs penetrate through the inner tube and are connected with a limiting plate, and a clamping joint is connected above the limiting plate;

the spring is connected with the below of limiting plate, the landing leg cover is established in the spring.

Furthermore, the limiting plate is a circular plate, and the diameter of the limiting plate is larger than that of the clamping hole.

Further, the clamping head, the limiting plate and the supporting leg are integrally formed.

Further, the inner tube is funnel-shaped.

Further, the inner diameter value of the bottom of the inner pipe is smaller than the width value of the spring.

Furthermore, the edge of the upper surface of the limiting plate is arranged in a smooth arc surface.

The utility model has the advantages that:

through setting up shell body, spring and inner tube, can make limiting plate compression spring through the pulling landing leg when using, make the joint head leave the joint hole, realize the angle change of landing leg, can practice thrift the space, unmanned aerial vehicle's of being convenient for deposit and transportation.

Drawings

Fig. 1 is a schematic structural diagram of the present invention.

Fig. 2 is a schematic view of the external structure of the present invention.

Fig. 3 is a schematic top view of the present invention.

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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

The unmanned aerial vehicle support leg shown in the attached figures 1-3 comprises a support leg 5 and an outer shell 1, wherein the bottom and the side wall of one side of the outer shell 1 are provided with openings, and the top of the outer shell 1 is provided with a clamping hole 8 and a plurality of connecting holes 9;

an inner tube 3 is arranged in the outer shell 1, and the inner tube 3 and the outer shell 1 are fixed through screws 4;

the top and the bottom of the inner tube 3 are both provided with openings, the top ends of the supporting legs 5 penetrate through the inner tube 3 and are connected with a limiting plate 6, and a clamping joint 7 is connected above the limiting plate 6;

the spring 2 is connected below the limiting plate 6, and the supporting legs 5 are sleeved in the spring 2.

In this preferred embodiment, the limiting plate 6 is a circular plate, and the diameter of the limiting plate 6 is greater than the diameter of the fastening hole 8.

In the preferred embodiment, the snap joint 7, the stopper plate 6 and the leg 5 are integrally formed.

In the preferred embodiment, the inner tube 3 is funnel-shaped.

In the preferred embodiment, the inner diameter of the bottom of the inner tube 3 is smaller than the width of the spring 2.

In this preferred embodiment, the edge of the upper surface of the limiting plate 6 is a smooth arc surface.

The utility model discloses the theory of operation: the utility model discloses a set up shell body 1, spring 2 and inner tube 3, can make limiting plate 6 compression spring 2 through pulling landing leg 5 when using, make joint head 7 leave joint hole 8, realize the angle change of landing leg 5, can practice thrift the space, be convenient for unmanned aerial vehicle deposit and transportation.

The points to be finally explained are: first, in the description of the present application, it should be noted that, unless otherwise specified and limited, the terms "mounted," "connected," and "connected" should be understood broadly, and may be a mechanical connection or an electrical connection, or a communication between two elements, and may be a direct connection, and "upper," "lower," "left," and "right" are only used to indicate a relative positional relationship, and when the absolute position of the object to be described is changed, the relative positional relationship may be changed;

secondly, the method comprises the following steps: in the drawings of the disclosed embodiments of the present invention, only the structures related to the disclosed embodiments are referred to, and other structures can refer to the common design, and under the condition of no conflict, the same embodiment and different embodiments of the present invention can be combined with each other;

and finally: the foregoing is illustrative of the preferred embodiments of the present invention, and is not to be construed as limiting the invention, and any modifications, equivalent alterations, improvements and the like made within the spirit and principle of the invention are intended to be included within the scope of the invention.

Claims

1. An unmanned aerial vehicle landing leg, includes landing leg (5), its characterized in that: the novel portable multifunctional electric heating cooker also comprises an outer shell (1), wherein the bottom and the side wall of one side of the outer shell (1) are provided with openings, and the top of the outer shell (1) is provided with a clamping hole (8) and a plurality of connecting holes (9);

an inner pipe (3) is arranged in the outer shell (1), and the inner pipe (3) and the outer shell (1) are fixed through a screw (4);

the top and the bottom of the inner pipe (3) are both provided with openings, the top ends of the supporting legs (5) penetrate through the inner pipe (3) and are connected with a limiting plate (6), and a clamping joint (7) is connected above the limiting plate (6);

the lower part of the limiting plate (6) is connected with a spring (2), and the supporting legs (5) are sleeved in the spring (2).

2. The unmanned aerial vehicle landing leg of claim 1, wherein: the limiting plate (6) is a circular plate, and the diameter of the limiting plate (6) is larger than that of the clamping hole (8).

3. An unmanned aerial vehicle landing leg according to claim 1 or 2, wherein: the clamping head (7), the limiting plate (6) and the supporting leg (5) are integrally formed.

4. The unmanned aerial vehicle landing leg of claim 1, wherein: the inner tube (3) is arranged in a funnel shape.

5. The unmanned aerial vehicle landing leg of claim 4, wherein: the bottom inner diameter value of the inner pipe (3) is smaller than the width value of the spring (2).

6. The unmanned aerial vehicle landing leg of claim 1, wherein: the edge of the upper surface of the limiting plate (6) is arranged in a smooth arc surface.