CN217146406U - Unmanned aerial vehicle wing bracket - Google Patents

Abstract

The utility model provides an unmanned aerial vehicle wing bracket, which comprises a bracket main body, at least two nylon supports and a plurality of universal casters, wherein the bracket main body is a rectangular frame, and support bars are distributed and arranged in the frame to support the frame; the at least two nylon brackets are distributed on the rectangular frame and are vertical to the plane of the rectangle; the nylon support bracket is provided with a notch for storing and fixing the wings; the universal casters are arranged at the bottom of the bracket main body. The utility model provides a wing bracket is whole light and handy, flexible operation is simple and convenient, simple structure and manufacturing cost are lower, and can prevent the wing damage.

Description

Unmanned aerial vehicle wing bracket

Technical Field

The utility model relates to an unmanned aerial vehicle field, in particular to unmanned aerial vehicle wing bracket.

Background

The wing bracket belongs to the support equipment class, and its main effect is to park the wing, supports the long-time storage of parking before assembly and debugging of unmanned aerial vehicle wing to and can convenient and fast's transfer and take when needing. The existing unmanned aerial vehicle wing bracket adopts more reinforcing devices, so that the operation is complicated when the product is taken; secondly, a hydraulic bracket is adopted, so that the problems of oil leakage and the like can occur after a hydraulic system is used for a long time, and the stability of the bracket cannot be ensured; the device is arranged one by one, and occupies a large space when being parked.

SUMMERY OF THE UTILITY MODEL

To the problem that exists now, consider the actual wing of unmanned aerial vehicle and park the demand, the utility model provides a can park a plurality of wings, light and handy, flexible operation is simple and convenient, simple structure and the lower wing bracket of manufacturing cost.

The utility model adopts the technical scheme as follows: an unmanned aerial vehicle wing bracket comprises a bracket main body, at least two nylon supports and a plurality of universal casters, wherein the bracket main body is a rectangular frame, and support bars are distributed and installed in the frame to support the frame; the at least two nylon brackets are distributed on the rectangular frame and are vertical to the plane of the rectangle; the nylon support bracket is provided with a notch for storing and fixing the wings; the universal casters are arranged at the bottom of the bracket main body.

Furthermore, the notches on the nylon brackets arranged on the rectangular frame have different depths, and the depth of the notch on the nylon bracket from one side to the other side is from shallow to deep; the side with the shallow depth of the notch is used for placing the wingtip of the wing.

Furthermore, a rubber soft pad is adhered to the surface of the nylon support bracket and used for protecting the wing

Furthermore, each nylon support bracket is correspondingly provided with a plurality of notches for placing a plurality of wings.

Further, the bottom of the bracket main body is provided with a ground brake.

Furthermore, three nylon supports are arranged on the bracket main body and are distributed and installed on the front part, the middle part and the rear part of the rectangular frame.

Furthermore, a support piece is arranged between the nylon support bracket and the bracket main body and used for fixedly supporting the nylon support bracket.

Furthermore, a brake part is arranged on the universal caster.

Further, the bracket main body is made of aluminum alloy.

Furthermore, the nylon support bracket is made of ABS materials.

Compared with the prior art, the beneficial effects of the utility model are that: the scheme is light and handy, flexible and simple to operate, simple in structure and low in manufacturing cost, and can prevent the wings from being damaged.

Drawings

Fig. 1 is a schematic structural diagram of a wing bracket according to an embodiment of the present invention.

Reference numerals: 1-bracket main body, 2-nylon support, 3-universal caster, 4-ground brake, 5-support bar and 6-support piece.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.

Reference will now be made in detail to embodiments of the present application, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar modules or modules having the same or similar functionality throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present application and are not to be construed as limiting the present application. On the contrary, the embodiments of the application include all changes, modifications and equivalents coming within the spirit and terms of the claims appended hereto.

As shown in fig. 1, to the existing need of storing and parking wings of an unmanned aerial vehicle, the embodiment provides an unmanned aerial vehicle wing bracket, and the specific scheme is as follows:

the wing bracket of the unmanned aerial vehicle comprises a bracket main body 1, at least two nylon brackets 2 and a plurality of universal casters 3, wherein the bracket main body 1 is a rectangular frame, and supporting bars 5 are distributed in the frame and used for supporting the frame; the at least two nylon brackets 2 are distributed on the rectangular frame and are vertical to the plane of the rectangle; the nylon bracket 2 is provided with a notch for storing and fixing the wings; the plurality of casters 3 are provided at the bottom of the carriage body.

Specifically, in the present embodiment, three nylon lugs 2 are provided, and are sequentially installed at the front, middle, and rear portions of the bracket main body 1, and the interval between adjacent nylon lugs 2 is substantially the same.

In order to ensure that the wings are placed correctly, the depth of the notches on the nylon supports 2 at the front, middle and rear parts is from shallow to deep, and the nylon supports with the shallow notches are provided with nameplates which are provided with the characters of wing tips so as to distinguish the placing directions of the wings.

Meanwhile, in order to protect the wings from being damaged by the nylon support 2, rubber cushions are stuck to the surface of the nylon support 2.

In this embodiment, every nylon supports and corresponds to be equipped with four breachs on 2, can support 2 unmanned aerial vehicle's four wings to put to reduce and put the space.

In order to ensure the installation stability of the nylon bracket, two ends of the nylon bracket 2 are respectively provided with a support piece 6 to be connected with the bracket main body 1, so as to ensure that the nylon bracket 2 is still perpendicular to the bracket main body 1 after the wings are placed on the nylon bracket 2.

In this embodiment, the bottom of the bracket body 1 is provided with a ground brake 4 and a universal caster 3 for fixing the bracket when parking, and the operation is flexible and simple.

In a preferred embodiment, the universal caster 3 is provided with a braking function, and is convenient to steer and move.

In this embodiment, the bracket main body 1 adopts an optimized design, is formed by connecting aluminum alloy sections as main body materials, and has light weight, firm structure and low cost.

In this embodiment, the nylon bracket 2 is made of ABS material, and the surface is measured according to the airfoil digifax 1: 1, forming.

The wing bracket that this embodiment provided relies on three nylon to hold in the palm 4 wings of some support 2 unmanned aerial vehicles at the during operation, plays the effect of parking the wing.

The specific using method comprises the following steps: 1) one person releases the wing bracket ground brake, releases the caster brake and pushes the caster from the storage position to the use position; 2) after the position of the support is determined, the ground brake and the caster brake point are stepped on; 3) two people lift the wings on the wing bracket, the wings are lightly placed in the placing process, the wings do not collide with the surface of the wings, and the name plate on the bracket is marked with the wing tip during placing, so that the parking directions of the wings are distinguished. 4) After the wing bracket is used, the wing bracket is moved to a designated storage position, and the ground brake and the caster brake point are stepped on to prevent the bracket from freely moving.

The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims (10)

1. An unmanned aerial vehicle wing bracket is characterized by comprising a bracket main body, at least two nylon brackets and a plurality of universal casters, wherein the bracket main body is a rectangular frame, and supporting bars are distributed and arranged in the frame to support the frame; the at least two nylon brackets are distributed on the rectangular frame and are vertical to the plane of the rectangle; the nylon support bracket is provided with a notch for storing and fixing the wings; the universal casters are arranged at the bottom of the bracket main body.

2. The unmanned aerial vehicle wing bracket of claim 1, wherein the notches on the nylon brackets mounted on the rectangular frame are of different depths, the depth of the notch on the nylon bracket from one side to the other side ranging from shallow to deep; the side with the shallow depth of the notch is used for placing the wingtip of the wing.

3. The unmanned aerial vehicle wing bracket of claim 1, wherein a rubber cushion is adhered to a surface of the nylon support bracket for protecting a wing.

4. The unmanned aerial vehicle wing bracket of claim 1, wherein each nylon bracket is correspondingly provided with a plurality of notches for holding a plurality of wings.

5. An unmanned aerial vehicle wing carrier as claimed in claim 1, wherein the carrier body bottom is provided with a ground brake.

6. The unmanned aerial vehicle wing bracket of claim 1, wherein the bracket body is provided with three nylon lugs which are respectively arranged at the front, middle and rear parts of the rectangular frame.

7. The unmanned aerial vehicle wing bracket of claim 1, wherein a support member is provided between the nylon bracket and the bracket body for fixedly supporting the nylon bracket.

8. An unmanned aerial vehicle wing carrier as claimed in claim 1, wherein the casters are provided with brake members.

9. The unmanned aerial vehicle wing carrier of claim 1, wherein the carrier body is made of an aluminum alloy.

10. The unmanned aerial vehicle wing bracket of claim 1, wherein the nylon lug is made of an ABS material.

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