CN210503154U

CN210503154U - Unmanned aerial vehicle convenient to accomodate

Info

Publication number: CN210503154U
Application number: CN201921021960.0U
Authority: CN
Inventors: 李世忠
Original assignee: Foshan Zhongzhi Guangyuan Technology Co Ltd
Current assignee: Foshan Zhongzhi Guangyuan Technology Co Ltd
Priority date: 2019-07-02
Filing date: 2019-07-02
Publication date: 2020-05-12
Anticipated expiration: 2029-07-02

Abstract

The utility model discloses an unmanned aerial vehicle convenient to accomodate, including fuselage, horn, wing, its characterized in that: be equipped with on the fuselage and be used for accomodating the chamber of accomodating of wing, be equipped with articulated seat on the lateral wall of the organism of accomodating the intracavity, the horn includes first folding arm, the folding arm of second, first folding arm pass through first articulated elements articulate in articulate on the seat, the folding arm fixed connection wing of second, first folding arm the second is folded the arm and is passed through the articulated connection of second articulated elements. The utility model discloses a set up on the fuselage and accomodate the chamber for wing and horn are accomodate in accomodating the chamber, have avoided the horn folding opportunity wing expose and carry the problem that the process was damaged easily colliding outward, and simultaneously, the wing plays the guard action to the wing when being provided with the unmanned aerial vehicle flight of guard circle all around.

Description

Unmanned aerial vehicle convenient to accomodate

Technical Field

The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned aerial vehicle convenient to accomodate.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The existing unmanned aerial vehicle usually designs the horn into a folding structure so as to reduce the space and facilitate carrying. However, after the arms of the existing unmanned aerial vehicle are folded, the wings are still exposed outside, and collision damage to the wings is easily caused in the carrying process. Therefore, there is a need for improvements to existing foldable drones.

SUMMERY OF THE UTILITY MODEL

The to-be-solved technical problem of the utility model is to provide an unmanned aerial vehicle convenient to accomodate for the back is accomodate to the unmanned aerial vehicle wing, and the wing is not exposed outside, and difficult collision damages.

In order to solve the technical problem, the utility model discloses a technical scheme does: the utility model provides an unmanned aerial vehicle convenient to accomodate, includes fuselage, horn, wing, be equipped with on the fuselage and be used for accomodating the chamber of accomodating of wing, be equipped with articulated seat on the lateral wall of the organism of accomodating the intracavity, the horn includes the arm of folding of first folding arm, second, first folding arm through first articulated elements articulate in on the articulated seat, the arm fixed connection wing is folded to the second, first folding arm the arm is folded to the second passes through the articulated connection of second articulated elements.

Preferably, the wing comprises a motor, a rotating shaft and a blade, one end of the rotating shaft is connected with the motor, the other end of the rotating shaft is connected with the blade, and the motor is connected with the second folding arm.

Preferably, the wing further comprises a guard ring for protecting the wing, and the guard ring is arranged around the wing.

Preferably, the guard ring is made of light aluminum.

Preferably, a damper is arranged in the first hinge part and the second hinge part.

Preferably, the first folding arm is rotatable about 60 degrees about the first hinge and the second folding wing is rotatable about 180 degrees about the second hinge.

Preferably, the length of the first folding arm is greater than the length of the second folding arm.

Compared with the prior art, the utility model provides an advantage is: the storage cavity is formed in the fuselage, so that the wings and the horn are stored in the storage cavity, the problem that the wings are exposed when the horn is folded and are easy to collide and damage in the process of carrying the horn is avoided, and meanwhile the wings are provided with the protection rings around to protect the wings when the unmanned aerial vehicle flies.

Drawings

Fig. 1 is a schematic structural view of the unmanned aerial vehicle convenient for storage according to the present invention;

fig. 2 is the utility model provides an unmanned aerial vehicle's the state of accomodating schematic diagram convenient to accomodate.

In the figure, 1-machine body, 2-machine arm, 21-first folding arm, 22-second folding arm, 3-articulated seat, 4-containing cavity, 5-motor, 6-rotating shaft, 7-blade, 8-guard ring, 9-first articulated element and 10-second articulated element.

Detailed Description

The following describes the present invention with reference to the accompanying drawings. It should be noted that the description of the embodiments is provided to help understanding of the present invention, but the present invention is not limited thereto. In addition, the technical features related to the embodiments of the present invention described below may be combined with each other as long as they do not conflict with each other.

As shown in fig. 1-2, an unmanned aerial vehicle convenient to accomodate, includes fuselage 1, horn 2, wing, be equipped with on the fuselage and be used for accomodating the chamber 4 of wing, be equipped with articulated seat 3 on the lateral wall of the organism in the chamber 4 of accomodating, the horn includes the first arm 21 of folding, the arm 22 is folded to the second, first arm 21 of folding articulate through first articulated elements 9 in articulated seat 3 is last, the arm 22 fixed connection wing is folded to the second, first arm 21 of folding the arm 22 of second is through the articulated connection of second articulated elements 10.

The wing includes motor 5, pivot 6, paddle 7, motor 5 is connected to 6 one end of pivot, and paddle 7 is connected to the other end, motor 5 is connected with second folding arm 22. The wing is equipped with guard ring 8 that is used for protecting the wing all around, and the preferred light aluminum product of guard ring 8, the setting of guard ring plays the guard action to the wing when being convenient for unmanned aerial vehicle flight. Dampers are arranged in the first hinge part 9 and the second hinge part 10, so that the horn can be smoothly unfolded or folded, the shape of the horn can be fixed, and the horn is not easy to deform. The first folding arm 21 may rotate 60 degrees about the first hinge and the second folding wing may rotate 180 degrees about the second hinge. The length of the first folding arm 21 is greater than the length of the second folding arm 22.

When the folding wing is not used, the first folding arm is rotated to enable the first folding arm to rotate 60 degrees to one side close to the fuselage, and meanwhile, the second folding arm rotates 180 degrees to the direction close to the first folding arm, so that the wing is folded and stored in the storage cavity, the wing is prevented from being exposed outside, and the wing is protected. When the folding device is used, the first folding arm is rotated to be unfolded for 60 degrees, and meanwhile, the second folding arm is rotated for 180 degrees in the direction away from the first folding arm, so that the machine arm is unfolded. The utility model discloses the chamber is accomodate through setting up on the fuselage to the device for wing and horn are accomodate in accomodating the chamber, have avoided the horn folding time wing expose and carry the problem that the process was damaged easily colliding outward, and simultaneously, the wing plays the guard action to the wing when being provided with the unmanned aerial vehicle flight of guard circle all around.

The embodiments of the present invention have been described in detail with reference to the accompanying drawings, but the present invention is not limited to the described embodiments. It will be apparent to those skilled in the art that various changes, modifications, substitutions and alterations can be made in the embodiments without departing from the principles and spirit of the invention, and the scope of the invention is to be accorded the full scope of the claims.

Claims

1. The utility model provides an unmanned aerial vehicle convenient to accomodate, includes fuselage, horn, wing, its characterized in that: be equipped with on the fuselage and be used for accomodating the chamber of accomodating of wing, be equipped with articulated seat on the lateral wall of the organism of accomodating the intracavity, the horn includes first folding arm, the folding arm of second, first folding arm pass through first articulated elements articulate in articulate on the seat, the folding arm fixed connection wing of second, first folding arm the second is folded the arm and is passed through the articulated connection of second articulated elements.

2. The unmanned aerial vehicle convenient to accomodate of claim 1, wherein: the wing comprises a motor, a rotating shaft and a paddle, one end of the rotating shaft is connected with the motor, the other end of the rotating shaft is connected with the paddle, and the motor is connected with the second folding arm.

3. The unmanned aerial vehicle convenient to accomodate of claim 2, wherein: the wing also comprises a guard ring for protecting the wing, and the guard ring is arranged around the wing.

4. The unmanned aerial vehicle convenient to accomodate of claim 3, wherein: the guard ring is made of light aluminum.

5. The unmanned aerial vehicle convenient to accomodate of claim 1, wherein: dampers are arranged in the first hinge part and the second hinge part.

6. The unmanned aerial vehicle convenient to accomodate of claim 1, wherein: the first folding arm may rotate 60 degrees about the first hinge and the second folding wing may rotate 180 degrees about the second hinge.

7. The unmanned aerial vehicle convenient to accomodate of claim 6, wherein: the length of the first folding arm is greater than the length of the second folding arm.