CN213649889U

CN213649889U - Unmanned aerial vehicle

Info

Publication number: CN213649889U
Application number: CN202022663574.0U
Authority: CN
Inventors: 肖垚
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-11-17
Filing date: 2020-11-17
Publication date: 2021-07-09
Anticipated expiration: 2030-11-17

Abstract

The utility model discloses an unmanned aerial vehicle, including the unmanned aerial vehicle body, the unmanned aerial vehicle body includes the cabin, and the inside in cabin is provided with the battery, and one side of battery is provided with the controller, and one side of controller is provided with wireless signal transceiver module, and the both ends of cabin both sides all are provided with the retainer plate, and the inside of four retainer plates all is provided with the screw, and the bottom middle part of four screws all is provided with the pivot, and the bottom of four pivots all is provided with a driving motor, and four driving motor's bottom all is provided with fixed frame. The utility model discloses be equipped with moving part and gyro wheel in the bottom of four telescopic links, the piston rod through four telescopic links promotes moving part and gyro wheel with two supporting foot board jack-ups, and second driving motor's output shaft drives the gyro wheel and rotates for unmanned aerial vehicle can go subaerial, thereby has addd control unmanned aerial vehicle's enjoyment, and this kind of unmanned aerial vehicle structure attracts, low in manufacturing cost.

Description

Unmanned aerial vehicle

Technical Field

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

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, in the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting and the like, the use of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

Present unmanned aerial vehicle passes through controlgear and flies in the sky, and the unmanned aerial vehicle of tradition majority does not support comparatively and goes subaerial to control unmanned aerial vehicle's enjoyment has been lacked.

SUMMERY OF THE UTILITY MODEL

In order to solve the technical problem, the utility model provides a following technical scheme:

an unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body comprises a cabin, a storage battery is arranged in the cabin, a controller is arranged on one side of the storage battery, a wireless signal transceiver module is arranged on one side of the controller, fixing rings are arranged at two ends of two sides of the cabin, propellers are arranged in four fixing rings, rotating shafts are arranged in the middle of the bottom ends of four propellers, first driving motors are arranged at the bottom ends of four rotating shafts, fixing frames are arranged at the bottom ends of four first driving motors, connecting blocks are arranged at the bottom ends of four fixing frames, connecting rods are arranged at the bottom ends of four connecting blocks, telescopic rods are arranged at one sides of four connecting rods, moving parts are arranged at the bottom ends of four telescopic rods, which are positioned outside the four connecting rods, and a second driving motor is arranged at one end of each moving part, and one end of each of the four output shafts of the second driving motor is provided with a roller.

As a preferred technical scheme of the utility model, the bottom of battery, controller and radio signal transceiver module all with the inside fixed connection in cabin, controller and radio signal transceiver module all with battery electric connection, the controller passes through radio signal transceiver module and external control handle equipment electricity wireless connection.

As an optimal technical scheme of the utility model, four one side of retainer plate all with the both ends fixed connection of cabin both sides, four the retainer plate all adopts the PVC material to make.

As a preferred technical scheme of the utility model, four the both ends of fixed frame all with the both sides fixed connection of four retainer plates bottoms, four the bottom of a driving motor all with the inside fixed connection of four fixed frames.

As an optimal technical scheme of the utility model, four the top and the bottom of pivot respectively with the bottom middle part of four screws, the top fixed connection of four first driving motor output shafts, four first driving motor all with battery and controller electric connection.

As a preferred technical scheme of the utility model, four connecting block bottoms all with the top fixed connection of four connecting rods, one side of four telescopic links all with four connecting rod fixed connection, four one side on moving part top all with the piston rod bottom fixed connection of four telescopic links.

As a preferred technical scheme of the utility model, four the one end of second driving motor all with the one end fixed connection of four moving parts, four the middle part of gyro wheel one side all with four second driving motor's output shaft fixed connection, four second driving motor all with battery and controller electric connection.

As an optimal technical scheme of the utility model, four the bottom mounting of telescopic link is provided with two support sole, two the bottom of supporting the sole all is provided with the slipmat.

The utility model has the advantages that: this kind of unmanned aerial vehicle passes through moving part and the gyro wheel that four telescopic link bottoms were equipped with, and the piston rod through four telescopic links promotes moving part and gyro wheel with two supporting foot board jack-ups, and second driving motor's output shaft drives the gyro wheel and rotates for unmanned aerial vehicle can go subaerial, thereby has addd control unmanned aerial vehicle's enjoyment, and this kind of unmanned aerial vehicle structure attracts, low in manufacturing cost.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 is a schematic structural diagram of the present invention;

FIG. 2 is a schematic view of a part of the structure of the present invention;

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

fig. 4 is a schematic view of the internal structure of the nacelle of the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. a nacelle; 3. a storage battery; 4. a controller; 5. a wireless signal transceiving module; 6. a stationary ring; 7. a propeller; 8. a rotating shaft; 9. a first drive motor; 10. a fixing frame; 11. connecting blocks; 12. a connecting rod; 13. a telescopic rod; 14. a movable member; 15. a second drive motor; 16. a roller; 17. supporting the foot plate.

Detailed Description

The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.

Example (b): as shown in fig. 1-3, the utility model provides an unmanned aerial vehicle, which comprises an unmanned aerial vehicle body 1, the unmanned aerial vehicle body 1 comprises a cabin 2, a storage battery 3 is arranged in the cabin 2, a controller 4 is arranged on one side of the storage battery 3, a wireless signal transceiver module 5 is arranged on one side of the controller 4, two ends of two sides of the cabin 2 are respectively provided with a fixed ring 6, propellers 7 are arranged in the four fixed rings 6, a rotating shaft 8 is arranged in the middle of the bottom ends of the four propellers 7, a first driving motor 9 is arranged at the bottom ends of the four rotating shafts 8, a fixed frame 10 is arranged at the bottom end of each of the four first driving motors 9, a connecting block 11 is arranged at the bottom end of each of the four fixed frames 10, a connecting rod 12 is arranged at the bottom end of each of the four connecting blocks 11, a telescopic rod 13 is arranged on one side, one end of each of the four movable members 14 is provided with a second driving motor 15, and one end of each of output shafts of the four second driving motors 15 is provided with a roller 16.

Wherein, battery 3, the bottom of controller 4 and wireless signal transceiver module 5 all with cabin 2's inside fixed connection, controller 4 and wireless signal transceiver module 5 all with battery 3 electric connection, controller 4 passes through wireless signal transceiver module 5 and external control handle equipment wireless connection, through battery 3 that is equipped with in cabin 2 inside, controller 4 and wireless signal transceiver module 5, make it provide power and control for four first driving motor 9 and four second driving motor 15 through battery 3 and controller 4 in order to guarantee normal work.

Wherein, one side of four retainer plates 6 all with the both ends fixed connection at 2 both sides in cabin, four retainer plates 6 all adopt the PVC material to make, fix the both ends at 2 both sides in cabin through four retainer plates 6 that are equipped with, and four retainer plates 6 all adopt PVC to make, make it improve unmanned aerial vehicle body 1's equilibrium and weight.

Wherein, the both ends of four fixed frames 10 all with the both sides fixed connection of four 6 bottoms of retainer plates, the bottom of four first driving motor 9 all with the inside fixed connection of four fixed frames 10, through the bottom of four first driving motor 9 all with the inside fixed connection of four fixed frames 10, make it fix four first driving motor 9 in the bottom of four fixed frames 10 through four fixed frames 10.

Wherein, the top and the bottom of four pivot 8 respectively with the bottom middle part of four screws 7, the top fixed connection of four first driving motor 9 output shafts, four first driving motor 9 all with

battery

3 and 4 electric connection of controller, output shaft through four first driving motor 9 all with the bottom middle part fixed connection of four screws 7, make its four first driving motor 9's output shaft drive four screws 7 and rotate, unmanned aerial vehicle body 1 rotates through four screws 7 and flies.

Wherein, the top fixed connection of four 11 bottoms of connecting block all with four connecting rods 12, one side of four telescopic link 13 all with four connecting rods 12's fixed connection, one side on four moving part 14 tops all with the bottom fixed connection of four telescopic link 13's piston rod, one side through four moving part 14 tops all with the bottom fixed connection of four telescopic link 13's piston rod, make its four telescopic link 13's piston rod promote four moving part 14 along four connecting rods 12's outside downstream, jack-up unmanned aerial vehicle body 1, four gyro wheels 16 land.

Wherein, the one end of four second driving motor 15 all with the one end fixed connection of four moving parts 14, the middle part of four gyro wheels 16 one side all with four second driving motor 15's output shaft fixed connection, four second driving motor 15 all with

battery

3 and 4 electric connection of controller, the middle part through four gyro wheels 16 one side all with four second driving motor 15's output shaft fixed connection, make its four second driving motor 15's output shaft drive four gyro wheels 16 and rotate, make its unmanned aerial vehicle body 1 can go subaerial.

Wherein, the bottom mounting of four telescopic links 13 is provided with two support sole 17, and the bottom of two support sole 17 all is provided with the slipmat, through the slipmat that two support sole 17 and bottom that are equipped with were equipped with, makes the stable support of its unmanned aerial vehicle body 1 subaerial.

During operation, fix the both ends at 2 both sides in cabin through four retainer plates 6 that are equipped with, and four retainer plates 6 all adopt PVC to make, make it improve unmanned aerial vehicle body 1's equilibrium and weight. The bottom ends of the four first driving motors 9 are fixedly connected with the inside of the four fixed frames 10, so that the four first driving motors 9 are fixed at the bottom ends of the four fixed frames 10 through the four fixed frames 10. All with the bottom middle part fixed connection of four screws 7 through the output shaft of four first driving motor 9, make its four first driving motor 9's output shaft drive four screws 7 and rotate, unmanned aerial vehicle body 1 rotates through four screws 7 and flies. One side through four moving parts 14 tops all with the bottom fixed connection of the piston rod of four telescopic links 13, make its four telescopic links 13's piston rod promote four moving parts 14 along the outside downstream of four connecting rods 12, with unmanned aerial vehicle body 1 jack-up, four gyro wheels 16 land. All with four second driving motor 15's output shaft fixed connection through the middle part of four gyro wheels 16 one sides, make its four second driving motor 15's output shaft drive four gyro wheels 16 and rotate, make its unmanned aerial vehicle body 1 can go subaerial. Through the storage battery 3, the controller 4 and the wireless signal transceiving module 5 which are arranged in the cabin 2, the storage battery 3 and the controller 4 are used for providing power supply and control for the four first driving motors 9 and the four second driving motors 15 so as to ensure normal operation.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. An unmanned aerial vehicle comprises an unmanned aerial vehicle body (1) and is characterized in that the unmanned aerial vehicle body (1) comprises a cabin (2), a storage battery (3) is arranged in the cabin (2), a controller (4) is arranged on one side of the storage battery (3), a wireless signal receiving and transmitting module (5) is arranged on one side of the controller (4), fixing rings (6) are arranged at two ends of two sides of the cabin (2), propellers (7) are arranged in the four fixing rings (6), a rotating shaft (8) is arranged in the middle of the bottom ends of the four propellers (7), first driving motors (9) are arranged at the bottom ends of the four rotating shafts (8), fixed frames (10) are arranged at the bottom ends of the four first driving motors (9), and connecting blocks (11) are arranged at the bottom ends of the four fixed frames (10), four the bottom of connecting block (11) all is provided with connecting rod (12), four connecting rod (12) one side all is provided with telescopic link (13), four the outside that the bottom of telescopic link (13) is located four connecting rod (12) is provided with moving part (14), four the one end of moving part (14) all is provided with second driving motor (15), four the one end of second driving motor (15) output shaft all is provided with gyro wheel (16).

2. An unmanned aerial vehicle according to claim 1, wherein the bottom ends of the storage battery (3), the controller (4) and the wireless signal transceiver module (5) are all fixedly connected with the inside of the cabin (2), the controller (4) and the wireless signal transceiver module (5) are both electrically connected with the storage battery (3), and the controller (4) is wirelessly connected with an external control handle device through the wireless signal transceiver module (5).

3. An unmanned aerial vehicle according to claim 1, wherein one side of each of the four fixing rings (6) is fixedly connected with two ends of two sides of the cabin (2), and each of the four fixing rings (6) is made of PVC material.

4. An unmanned aerial vehicle according to claim 1, wherein the two ends of the four fixed frames (10) are fixedly connected with two sides of the bottom ends of the four fixed rings (6), and the bottom ends of the four first driving motors (9) are fixedly connected with the inner parts of the four fixed frames (10).

5. An unmanned aerial vehicle according to claim 1, wherein the top and bottom ends of the four rotating shafts (8) are respectively and fixedly connected with the middle of the bottom ends of the four propellers (7) and the top ends of the output shafts of the four first driving motors (9), and the four first driving motors (9) are electrically connected with the storage battery (3) and the controller (4).

6. An unmanned aerial vehicle according to claim 1, wherein the bottom ends of four connecting blocks (11) are all fixedly connected with the top ends of four connecting rods (12), one side of each of four telescopic rods (13) is fixedly connected with the top ends of four connecting rods (12), and one side of the top ends of four movable members (14) is fixedly connected with the bottom ends of piston rods of four telescopic rods (13).

7. An unmanned aerial vehicle according to claim 1, wherein one end of each of the four second driving motors (15) is fixedly connected with one end of each of the four movable members (14), the middle portion of one side of each of the four rollers (16) is fixedly connected with an output shaft of each of the four second driving motors (15), and each of the four second driving motors (15) is electrically connected with the storage battery (3) and the controller (4).

8. An unmanned aerial vehicle according to claim 1, wherein the bottom ends of the four telescopic rods (13) are fixedly provided with two supporting foot plates (17), and the bottom ends of the two supporting foot plates (17) are provided with anti-skid pads.