CN217673162U

CN217673162U - Heavy-load foldable laser radar six-rotor unmanned aerial vehicle

Info

Publication number: CN217673162U
Application number: CN202220436366.3U
Authority: CN
Inventors: 胥伟; 张迅; 杨云龙; 李志磊; 罗凯; 邓雷
Original assignee: Nanchong Chuangnian Three Dimensional Technology Co ltd
Current assignee: Nanchong Chuangnian Three Dimensional Technology Co ltd
Priority date: 2022-03-02
Filing date: 2022-03-02
Publication date: 2022-10-28
Anticipated expiration: 2032-03-02

Abstract

The utility model belongs to the technical field of unmanned aerial vehicle technique and specifically relates to a six rotor unmanned aerial vehicle of heavy load collapsible laser radar, including unmanned aerial vehicle, the unmanned aerial vehicle outside fixedly connected with adds the boss, add the boss outside and rotate and be connected with the extension arm, add the boss outside fixedly connected with and rotate the cardboard, add the boss rear and rotate and be connected with the pivot, the pivot outside fixedly connected with rotates the cardboard, rotate the cardboard and fix the cardboard outside and all fixedly connected with the stationary blade; the utility model discloses in, through the anchor block that sets up, can let unmanned aerial vehicle's extension arm rotate, effectively solve the problem that unmanned aerial vehicle's extension arm occupied space, both sides are equipped with fixed cardboard and rotate the cardboard around the extension arm simultaneously, can will rotate cardboard and fix for the cardboard bolt fastening when unmanned aerial vehicle takes off, make things convenient for operating personnel to extend or the operation of shrink to unmanned aerial vehicle's extension arm, it is very practical.

Description

Heavy-load foldable laser radar six-rotor unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a six rotor unmanned aerial vehicle of collapsible laser radar of heavy load.

Background

Unmanned aerial vehicle for short is unmanned aerial vehicle, it is the unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to control, or by the vehicle-mounted computer completely or intermittently independently operate, unmanned aerial vehicle according to the application field, can be divided into military and civilian, for military use, unmanned aerial vehicle divide into reconnaissance plane and target plane, civil aspect, at present in the aerial photograph, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster rescue, control infectious disease, survey and drawing, news report, electric power is patrolled and examined, the application in disaster relief, film and television shooting, make romantic and so on field, the use of unmanned aerial vehicle itself has been greatly expanded, and the unmanned aerial vehicle that appears six rotors on the market, six rotor unmanned aerial vehicle is bulky, the extension arm is longer, increase the area under the condition of not using, and inconvenient carrying, therefore, propose a kind of foldable laser radar six rotor unmanned aerial vehicle of large load to the above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a six rotor unmanned aerial vehicle of collapsible laser radar of heavy load to solve the unable folding problem of six rotor unmanned aerial vehicle's the extension arm 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 a six rotor unmanned aerial vehicle of collapsible laser radar of heavy load, includes unmanned aerial vehicle, unmanned aerial vehicle outside fixedly connected with adds the anchor block, it is connected with the extension arm to add anchor block outside rotation, it rotates the cardboard to add anchor block outside fixedly connected with, it is connected with the pivot to add anchor block rear rotation, pivot outside fixedly connected with rotates the cardboard, rotate the cardboard and fix the equal fixedly connected with stationary blade in the cardboard outside.

Preferably, the rotating clamping plate and the fixed clamping plate are in contact with the extension arm, a hollow shell is fixedly connected to the outer side of the unmanned aerial vehicle, heat dissipation holes are formed in the outer side of the hollow shell, compression springs are fixedly connected to the outer side of the hollow shell, a bottom plate is fixedly connected to the other ends of the compression springs, and an extrusion plate is rotatably connected to the outer side of the bottom plate.

Preferably, the shape of rotating the cardboard is the same with the shape volume of fixed cardboard, and rotates the outside top of cardboard and fixed cardboard and all is equipped with the grooving, and the grooving width of rotating cardboard and fixed cardboard is the same with the width in extension arm outside.

Preferably, the fixing piece at the top end of the rotating clamping plate is fixedly connected with the fixing piece at the top end of the fixing clamping plate through a bolt, and the rotating clamping plate is located at the rear position of the fixing clamping plate.

Preferably, the number of the heat dissipation holes in the outer side of the hollow shell is several, and the caliber of each heat dissipation hole in the outer side of the hollow shell is 0.5cm.

Preferably, the bottom end of the extrusion plate is provided with a torsion spring, the torsion spring is located at the position of the outer side inside the bottom plate, and the extrusion plate is provided with a radian inclining from outside to inside.

Compared with the prior art, the beneficial effects of the utility model are that:

1. in the utility model, the extension arm of the unmanned aerial vehicle can be rotated through the arranged reinforcing block, so that the problem that the extension arm of the unmanned aerial vehicle occupies space is effectively solved, meanwhile, the front side and the rear side of the extension arm are provided with the fixed clamping plate and the rotating clamping plate, the rotating clamping plate and the fixed clamping plate can be fixed by bolts when the unmanned aerial vehicle takes off, and the extension or contraction operation of the extension arm of the unmanned aerial vehicle by an operator is facilitated, so that the unmanned aerial vehicle extension device is very practical;

2. the utility model discloses in, through the cavity shell and the bottom plate that set up, can place heavier goods in unmanned aerial vehicle's top, the cavity shell is located the below of bottom plate simultaneously, the cavity shell outside is equipped with the louvre, can let unmanned aerial vehicle's top still have the heat dissipation function, be connected with compression spring between bottom plate and the cavity shell simultaneously, the bottom plate top is equipped with the stripper plate, what produce when can reducing unmanned aerial vehicle flight rocks the goods that influence the bottom plate top, increase the stability of goods when the transportation, it is very practical.

Drawings

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

FIG. 2 is a schematic side view of the reinforcing block of the present invention;

FIG. 3 is a schematic view of the fixing clip plate structure of the present invention;

fig. 4 is a schematic view of the hollow shell structure of the present invention.

In the figure: 1-unmanned aerial vehicle, 2-reinforcing block, 3-extension arm, 4-rotating shaft, 5-rotating clamping plate, 6-fixing plate, 7-hollow shell, 8-bottom plate, 9-extrusion plate, 10-fixing clamping plate, 11-heat dissipation hole and 12-compression spring.

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:

a heavy-load foldable laser radar six-rotor unmanned aerial vehicle comprises an unmanned aerial vehicle 1, a reinforcing block 2 is fixedly connected to the outer side of the unmanned aerial vehicle 1, an extension arm 3 is rotatably connected to the outer side of the reinforcing block 2, a rotating clamping plate 5 is fixedly connected to the outer side of the reinforcing block 2, a rotating shaft 4 is rotatably connected to the rear side of the reinforcing block 2, a rotating clamping plate 5 is fixedly connected to the outer side of the rotating clamping plate 5 and the outer side of the fixing clamping plate 10, fixing pieces 6 are fixedly connected to the inner sides of the rotating clamping plate 5 and the inner side of the fixing clamping plate 10 and are in contact with the extension arm 3, a hollow shell 7 is fixedly connected to the middle outer side of the unmanned aerial vehicle 1, radiating holes 11 are formed in the outer side of the hollow shell 7, a compression spring 12 is fixedly connected to the outer side of the compression spring 12, an extrusion plate 9 is rotatably connected to the outer side of the bottom plate 8, the extension arm 3 of the unmanned aerial vehicle 1 can rotate through the reinforcing block 2, the problem that the space occupied by the extension arm 3 of the unmanned aerial vehicle 1 is effectively solved, a fixing clamping plate 10 and a rotating clamping plate 5 can be conveniently connected to the top end of the rotating clamping plate 5 when the rotating clamping plate 5 and the rotating clamping plate 5 is connected to the top end of the rotating clamping plate 5 and the rotating clamping plate 5, the rotating arm 10, and the rotating clamping plate 5 is connected to the rotating clamping plate 10; through cavity shell 7 and the bottom plate 8 that sets up, 11 quantity of louvres in the cavity shell 7 outside are a plurality of, and 11 bores of louvre in the cavity shell 7 outside are 0.5cm, can place heavier goods in unmanned aerial vehicle 1's top, cavity shell 7 is located the below of bottom plate 8 simultaneously, the cavity shell 7 outside is equipped with louvre 11, can let unmanned aerial vehicle 1's top still have the heat dissipation function, be connected with compression spring 12 between bottom plate 8 and the cavity shell 7 simultaneously, the bottom plate top is equipped with stripper plate 9, stripper plate 9 bottom is equipped with the torsional spring, and the torsional spring is located the inside outside position department of bottom plate 8, and stripper plate 9 is equipped with the outside-in radian that inclines, the goods that influence bottom plate 8 tops of rocking that produce when can reducing unmanned aerial vehicle 1 and fly, increase the stability of goods when the transportation, and is very practical.

The working process is as follows: extension arm 3 with unmanned aerial vehicle 1 during the use extends completely, after the extension, extension arm 3 card is in the inboard of fixed cardboard 10, stir rotation cardboard 5 this moment, will rotate cardboard 5 card at extension arm 3's rear, and use the bolt to fix fixed cardboard 10 and the stationary blade 6 that rotates the cardboard 5 outside, after finishing fixedly, place the bottom plate 8 up end in unmanned aerial vehicle 1 top with the goods, bottom plate 8 receives the weight downstream of goods, compression spring 12 takes place deformation, can let unmanned aerial vehicle 1 take off in the outside of goods with stripper plate 9 card this moment, the louvre 11 in the heat follow hollow shell 7 outside that produces when unmanned aerial vehicle 1 flies gives off, can let unmanned aerial vehicle 1's top still have the heat dissipation function, and is very practical.

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 a six rotor unmanned aerial vehicle of collapsible laser radar of heavy load, includes unmanned aerial vehicle (1), its characterized in that: unmanned aerial vehicle (1) outside fixedly connected with adds reinforcing block (2), it is connected with extension arm (3) to add reinforcing block (2) outside rotation, reinforcing block (2) outside fixedly connected with rotates cardboard (5), it is connected with pivot (4) to add reinforcing block (2) rear rotation, pivot (4) outside fixedly connected with rotates cardboard (5), rotate equal fixedly connected with stationary blade (6) in cardboard (5) and fixed cardboard (10) outside.

2. A heavy-load foldable lidar six-rotor drone according to claim 1, characterized in that: rotate cardboard (5) and fixed cardboard (10) inboard and extension arm (3) contact, outside fixedly connected with hollow shell (7) in the middle of unmanned aerial vehicle (1), the hollow shell (7) outside is equipped with louvre (11), hollow shell (7) outside fixedly connected with compression spring (12), compression spring (12) other end fixedly connected with bottom plate (8), bottom plate (8) outside is rotated and is connected with stripper plate (9).

3. A heavy-load foldable lidar six-rotor drone according to claim 1, characterized in that: the shape of rotating cardboard (5) is the same with the shape volume of fixed cardboard (10), and rotates the outside top of cardboard (5) and fixed cardboard (10) and all is equipped with the grooving, and rotates the grooving width of cardboard (5) and fixed cardboard (10) and the width in extension arm (3) outside the same.

4. A heavy-load foldable lidar six-rotor drone according to claim 1, characterized in that: the fixing plate (6) at the top end of the rotating clamping plate (5) is fixedly connected with the fixing plate (6) at the top end of the fixing clamping plate (10) through bolts, and the rotating clamping plate (5) is located at the rear position of the fixing clamping plate (10).

5. A heavy-load foldable lidar six-rotor drone according to claim 2, characterized in that: the number of the heat dissipation holes (11) on the outer side of the hollow shell (7) is a plurality, and the calibers of the heat dissipation holes (11) on the outer side of the hollow shell (7) are all 0.5cm.

6. A heavy-load foldable lidar six-rotor drone according to claim 2, characterized in that: the bottom end of the extrusion plate (9) is provided with a torsion spring, the torsion spring is positioned at the position of the inner outer side of the bottom plate (8), and the extrusion plate (9) is provided with a radian inclining from outside to inside.