CN210822719U

CN210822719U - Unmanned aerial vehicle wing mounting structure

Info

Publication number: CN210822719U
Application number: CN201922003097.2U
Authority: CN
Inventors: 汪文政; 陈茁; 潘丽敏; 汪莹
Original assignee: Yango University
Current assignee: Yango University
Priority date: 2019-11-19
Filing date: 2019-11-19
Publication date: 2020-06-23
Anticipated expiration: 2029-11-19

Abstract

The utility model discloses an unmanned aerial vehicle wing mounting structure, including the unmanned aerial vehicle main part, one side of unmanned aerial vehicle main part is equipped with the steel square pole, the right side fixedly connected with plastic tubing of steel square pole, the right side fixedly connected with motor box of plastic tubing, the upper portion of motor box is equipped with the wing, the upside of steel square pole is equipped with first sleeve, the utility model discloses have four steel square poles, the steel square pole is the main tributary strut structure, for the stability of additional strengthening structure, be connected with the stiffener between four steel square poles, the inside fixedly connected with first baffle of second sleeve, the welding of one side of first baffle has first spring, the internal welding of first sleeve has the second baffle, the welding of the upper portion of second baffle has the second spring, therefore the both ends of stiffener all are equipped with the spring, can play the shock attenuation effect when playing the strengthening firmness, the right side welding of motor box has the heat dissipation aluminum sheet, has increased heat dispersion.

Description

Unmanned aerial vehicle wing mounting structure

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle wing mounting structure.

Background

The unmanned aerial vehicle that can fly generally adopts the electric motor to drive a set of wing respectively, and if unmanned aerial vehicle loses balance and will fall from the high altitude, can cause the damage of certain part especially wing, so extremely endanger unmanned aerial vehicle's life. Unmanned aerial vehicle is when outdoor flight, if wind-force is great will influence unmanned aerial vehicle's balance, and current unmanned aerial vehicle wing structural stability is relatively poor, does not have the stiffener between four back shafts to the heat dispersion of motor is relatively poor, burns out easily, for this reason, we release an unmanned aerial vehicle wing mounting structure.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle wing mounting structure 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: the utility model provides an unmanned aerial vehicle wing mounting structure, includes the unmanned aerial vehicle main part, one side of unmanned aerial vehicle main part is equipped with the steel square bar, the right side fixedly connected with plastic tubing of steel square bar, the right side fixedly connected with motor box of plastic tubing, the upper portion of motor box is equipped with the wing, the upside of steel square bar is equipped with first sleeve, the downside of steel square bar is equipped with the second sleeve, the first baffle of the inside fixedly connected with of second sleeve, one side welding of first baffle has first spring, the one end welding of first spring has the stiffener, the inside welding of first sleeve has the second baffle, the upper portion welding of second baffle has the second spring, the inside of motor box is equipped with the motor, the output shaft upper end and the wing fixed connection of motor, the right side welding of motor box has the heat dissipation aluminum sheet.

Preferably, the upper part and the lower part of the steel square bar are both provided with a first groove.

Preferably, the first sleeve and the second sleeve are respectively welded with a lug, and the lug is welded with the first groove.

Preferably, the one end welding of steel square pole has the mounting panel, be equipped with the second recess on the mounting panel.

Preferably, the inside of second recess is equipped with the shock attenuation silica gel pad, the mounting panel passes through the bolt and is connected with the unmanned aerial vehicle main part.

Preferably, the outer side of the reinforcing rod is provided with a zinc coating.

Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses have four steel square poles, the steel square pole is main tributary bearing structure, for additional strengthening's stability, is connected with the stiffener between four steel square poles, the first baffle of the inside fixedly connected with of second sleeve, the welding of one side of first baffle has first spring, the welding of first telescopic inside has the second baffle, the welding of the upper portion of second baffle has the second spring, and consequently the both ends of stiffener all are equipped with the spring, can play absorbing effect when playing strengthening the firmness, the welding of the right side of motor box has the heat dissipation aluminum sheet, has increased heat dispersion.

Drawings

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

FIG. 2 is a schematic view of the steel square bar structure of the present invention;

FIG. 3 is a schematic view of the reinforcing rod structure of the present invention;

fig. 4 is the schematic diagram of the structure of the motor box of the present invention.

In the figure: 1. an unmanned aerial vehicle main body; 2. radiating aluminum sheets; 3. a reinforcing bar; 4. a steel square bar; 5. a plastic tube; 6. an airfoil; 7. a motor box; 8. a second sleeve; 9. a first sleeve; 10. a first groove; 11. mounting a plate; 12. a second groove; 13. a bolt; 14. a bump; 15. a first baffle plate; 16. a first spring; 17. a second baffle; 18. a second spring; 19. an electric motor.

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.

Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle wing mounting structure, includes unmanned aerial vehicle main part 1, one side of unmanned aerial vehicle main part 1 is equipped with steel square bar 4, the right side fixedly connected with plastic tubing 5 of steel square bar 4, the right side fixedly connected with motor box 7 of plastic tubing 5, the upper portion of motor box 7 is equipped with wing 6, and the quantity of steel square bar 4 and wing 6 is four, for strengthening the stability between four steel square bars 4, is connected with stiffener 3 between them.

The upside of steel square bar 4 is equipped with first sleeve 9, the downside of steel square bar 4 is equipped with second sleeve 8, the first baffle 15 of the inside fixedly connected with of second sleeve 8, the welding of one side of first baffle 15 has first spring 16, the welding of the one end of first spring 16 has stiffener 3, the internal weld of first sleeve 9 has second baffle 17, the welding of the upper portion of second baffle 17 has second spring 18, the inside of motor box 7 is equipped with motor 19, motor 19's output shaft upper end and wing 6 fixed connection, the welding of the right side of motor box 7 has heat dissipation aluminum sheet 2.

Both ends of stiffener 3 all are equipped with the spring, can play the absorbing effect when playing the reinforcing firmness.

In order to make the welding more stable, the upper part and the lower part of the steel square bar 4 are provided with first grooves 10, the first sleeve 9 and the second sleeve 8 are respectively welded with a lug 14, and the lug 14 is welded with the first groove 10.

In order to make the connection between mounting panel 11 and the unmanned aerial vehicle main part 1 have the steadiness, the one end welding of steel square bar 4 has mounting panel 11, be equipped with second recess 12 on the mounting panel 11, the inside of second recess 12 is equipped with the shock attenuation silica gel pad, mounting panel 11 passes through bolt 13 and is connected with unmanned aerial vehicle main part 1.

In order to prevent rusting, the outer side of the reinforcing rod 3 is provided with a zinc coating.

Specifically, during the use, this unmanned aerial vehicle wing mounting structure has four steel square poles 4, and steel square pole 4 is main bearing structure, for additional strengthening's stability, is connected with stiffener 3 between four steel square poles 4, the first baffle 15 of the inside fixedly connected with of second sleeve 8, the welding of one side of first baffle 15 has first spring 16, the internal weld of first sleeve 9 has second baffle 17, the welding of the upper portion of second baffle 17 has second spring 18, therefore the both ends of stiffener 3 all are equipped with the spring, can play absorbing effect when playing the enhancement firmness, the welding of the right side of motor box 7 has heat dissipation aluminum sheet 2, has increased heat dispersion.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle wing mounting structure, includes unmanned aerial vehicle main part (1), its characterized in that: one side of the unmanned aerial vehicle main body (1) is provided with a steel square rod (4), the right side of the steel square rod (4) is fixedly connected with a plastic pipe (5), the right side of the plastic pipe (5) is fixedly connected with a motor box (7), the upper portion of the motor box (7) is provided with a wing (6), the upper side of the steel square rod (4) is provided with a first sleeve (9), the lower side of the steel square rod (4) is provided with a second sleeve (8), the inside of the second sleeve (8) is fixedly connected with a first baffle (15), one side of the first baffle (15) is welded with a first spring (16), one end of the first spring (16) is welded with a reinforcing rod (3), the inside of the first sleeve (9) is welded with a second baffle (17), the upper portion of the second baffle (17) is welded with a second spring (18), the inside of the motor box (7) is provided with a motor (19), the upper end of an output shaft of the motor (19) is fixedly connected with the wing (6), and a heat dissipation aluminum sheet (2) is welded on the right side of the motor box (7).

2. The wing mounting structure of an unmanned aerial vehicle of claim 1, wherein: the upper portion and the lower portion of the steel square rod (4) are provided with first grooves (10).

3. The wing mounting structure of an unmanned aerial vehicle of claim 1, wherein: the first sleeve (9) and the second sleeve (8) are respectively welded with a bump (14), and the bump (14) is welded with the first groove (10).

4. The wing mounting structure of an unmanned aerial vehicle of claim 1, wherein: the one end welding of steel square bar (4) has mounting panel (11), be equipped with second recess (12) on mounting panel (11).

5. The wing mounting structure of an unmanned aerial vehicle of claim 4, wherein: the inside of second recess (12) is equipped with the shock attenuation silica gel pad, mounting panel (11) are connected with unmanned aerial vehicle main part (1) through bolt (13).

6. The wing mounting structure of an unmanned aerial vehicle of claim 1, wherein: and a zinc coating is arranged on the outer side of the reinforcing rod (3).