CN218112989U

CN218112989U - Unmanned aerial vehicle with two mesh visual structure

Info

Publication number: CN218112989U
Application number: CN202222677820.7U
Authority: CN
Inventors: 柳书博; 张红生; 李亮辰; 乔迁
Original assignee: Shaanxi Xigong University Science Park Co ltd
Current assignee: Shaanxi Xigong University Science Park Co ltd
Priority date: 2022-10-11
Filing date: 2022-10-11
Publication date: 2022-12-23
Anticipated expiration: 2032-10-11

Abstract

The utility model discloses an unmanned aerial vehicle with two mesh visual structure relates to unmanned air vehicle technical field, which comprises a bod, be provided with two mesh visual cameras on the organism, four evenly distributed's of fixedly connected with wing frame, every on the organism all install brushless motor on the wing frame, the contact has the undercarriage on the organism. The utility model discloses an add on brushless motor's output shaft and establish the connecting block, add in the outside of connecting block and establish the connecting cover, add on brushless motor and establish go-between isotructure, can carry on spacingly to go-between and flabellum through the inside joint frame of connecting cover and connecting block sliding connection, when needs are changed the flabellum, only need break away from the connecting block with the connecting cover and can accomplish the dismantlement to go-between and flabellum to can make the change of flabellum more convenient.

Description

Unmanned aerial vehicle with two mesh visual structure

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle with two mesh visual structure.

Background

Unmanned aerial vehicle is in the present that lasts the development, for satisfying people and controlling unmanned aerial vehicle to the adaptation of vision, develops two vision unmanned aerial vehicle, can be so that the vision is more comfortable, according to patent grant bulletin number: CN 205131672U provides an unmanned aerial vehicle with two mesh visual structure, this utility model discloses an unmanned aerial vehicle with two mesh visual structure, including unmanned aerial vehicle body, mount, detection device, the mount set up in the lower part of unmanned aerial vehicle body, detection device passes through the mount and is connected with the unmanned aerial vehicle body, the utility model discloses, set up two mesh visual structure, included first camera and second camera, first camera is infrared imager, infrared imager is used for gathering infrared image information, the second camera is the color camera, the color camera is used for gathering color image information, detection device sends infrared image information and color image information for control system through communication module, can solve the problem that can't satisfy the detection precision demand based on video analysis under the multiple scene through analysis infrared image information and color image information, can satisfy user's user demand. But unmanned aerial vehicle among the prior art is carrying the in-process of accomodating, and the undercarriage is great, and the occupation space that leads to unmanned aerial vehicle is great, and the undercarriage passes through the bolt to be installed and is not convenient for dismantle on the organism in addition, influences unmanned aerial vehicle's carrying to the flabellum damages easily when daily use, and the flabellum after the damage need be dismantled and is changed, but the flabellum is not convenient for dismantle the influence and change. Therefore, improvements in the prior art are needed.

SUMMERY OF THE UTILITY MODEL

The utility model provides an unmanned aerial vehicle with two mesh visual structures has solved the great unmanned aerial vehicle that leads to of undercarriage occupation space and is not portable and the technical problem of flabellum not convenient to detach.

For solving the technical problem, the utility model provides a pair of unmanned aerial vehicle with binocular vision structure, which comprises a bod, be provided with binocular vision camera on the organism, four evenly distributed's of fixedly connected with wing frame on the organism, every all install brushless motor on the wing frame, the contact has the undercarriage on the organism, the last fixedly connected with connecting block of output shaft of brushless motor, the last contact of brushless motor has the go-between, the outside fixedly connected with flabellum of go-between, the outside of connecting block is provided with the change mechanism, the inside of organism is provided with disassembly body, disassembly body includes connecting strip, stop pin, extension spring, fixedly connected with connecting strip on the undercarriage, the inside sliding connection of organism has the stop pin, be provided with the extension spring on the stop pin, the stop pin can carry on spacingly to the connecting strip.

Preferably, it includes the connecting cover, promotes piece, joint frame, guide arm, spring, square frame to change the mechanism, the outside sliding connection of connecting block has the connecting cover, the connecting cover with the connecting ring contact, sliding connection has the promotion piece on the connecting cover, promote fixedly connected with joint frame on the piece, the joint frame with connecting block sliding connection, the inside fixedly connected with guide arm of connecting cover, the outside of guide arm is provided with the spring, the guide arm with promote piece sliding connection, the shape of connecting block is square, also is square with connecting cover hookup location.

Preferably, the connecting cover is fixedly connected with a square frame, the square frame is in sliding connection with the connecting ring, and the connecting cover can drive the connecting ring to rotate through the square frame.

Preferably, one end of the spring is fixedly connected with the connecting cover, the other end of the spring is fixedly connected with the pushing block, and the spring can drive the pushing block to automatically reset through elasticity.

Preferably, the connecting strip is connected with the machine body in a sliding manner, and the limit pins are connected with the connecting strip in a sliding manner.

Preferably, one end of the tension spring is fixedly connected with the machine body, the other end of the tension spring is fixedly connected with the limit nail, and the tension spring can drive the limit nail to automatically reset through elasticity.

Compared with the prior art, the utility model provides a pair of unmanned aerial vehicle with two mesh visual structure has following beneficial effect:

the utility model provides an unmanned aerial vehicle with two mesh visual structure, establish the connecting block through adding on brushless motor's output shaft, add in the outside of connecting block and establish the connecting cover, add on brushless motor and establish go-between isotructure, can carry on spacingly to go-between and flabellum through the inside joint frame of connecting cover and connecting block sliding connection, when needs are changed the flabellum, only need break away from the connecting block with the connecting cover and can accomplish the dismantlement to go-between and flabellum, thereby can make the change of flabellum more convenient.

The utility model provides an unmanned aerial vehicle with two mesh visual structure, through add on the organism and establish the banking pin, add on the undercarriage and establish the connecting strip, add on the banking pin and establish extension spring isotructure, the elasticity that can pass through the extension spring drives the inside that the banking pin slided into the connecting strip and carries on spacingly to the undercarriage, when needs carry, can dismantle the whole volume that reduces unmanned aerial vehicle with the undercarriage through the inside roll-off with the banking pin from the connecting strip to can make unmanned aerial vehicle portable more.

Drawings

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

fig. 2 is a left side sectional view of fig. 1 of the present invention;

fig. 3 is a front view of the brushless motor of fig. 1 according to the present invention.

Fig. 4 is an enlarged view of the structure a of fig. 3 according to the present invention;

fig. 5 is an enlarged view of the structure of the part B in fig. 2 according to the present invention.

Reference numbers in the figures: 1. a body; 2. a binocular vision camera; 3. a wing frame; 4. a brushless motor; 5. a landing gear; 6. a connecting ring; 7. a fan blade; 8. a mechanism is replaced; 9. a disassembly mechanism; 10. connecting blocks; 81. a connecting cover; 82. a pushing block; 83. a clamping frame; 84. a guide bar; 85. a spring; 86. a square frame; 91. a connecting strip; 92. a limit pin; 93. a tension spring.

Detailed Description

Please refer to fig. 1, fig. 2, fig. 3, an unmanned aerial vehicle with binocular vision structure, which comprises a body 1, a binocular vision camera 2 is arranged on the body 1, four wing frames 3 are fixedly connected to the body 1 and evenly distributed, a brushless motor 4 is installed on each wing frame 3, an undercarriage 5 is contacted on the body 1, a connecting block 10 is fixedly connected to an output shaft of the brushless motor 4, a connecting ring 6 is contacted on the brushless motor 4, fan blades 7 are fixedly connected to the outer side of the connecting ring 6, a replacing mechanism 8 is arranged on the outer side of the connecting block 10, and a detaching mechanism 9 is arranged inside the body 1.

Referring to fig. 1, 3, and 4, the replacing mechanism 8 includes a connection cover 81, a pushing block 82, a clamping frame 83, a guide rod 84, a spring 85, and a square frame 86, the connection cover 81 is slidably connected to the outer side of the connection block 10, the connection cover 81 contacts with the connection ring 6, the pushing block 82 is slidably connected to the connection cover 81, the clamping frame 83 is fixedly connected to the pushing block 82, the clamping frame 83 is slidably connected to the connection block 10, the guide rod 84 is fixedly connected to the inside of the connection cover 81, the spring 85 is disposed on the outer side of the guide rod 84, the guide rod 84 is slidably connected to the pushing block 82, the connection block 10 is square, the connection position with the connection cover 81 is also square, the square frame 86 is fixedly connected to the connection cover 81, the square frame 86 is slidably connected to the connection ring 6, the connection cover 81 can drive the connection ring 6 to rotate through the square frame 86, one end of the spring 85 is fixedly connected to the connection cover 81, the other end of the spring 85 is fixedly connected to the pushing block 82, and the spring 85 can drive the pushing block 82 to automatically reset through elasticity.

Referring to fig. 1, 2, and 5, the detaching mechanism 9 includes a connecting strip 91, a limit pin 92, a tension spring 93, the landing gear 5 is fixedly connected with the connecting strip 91, the connecting strip 91 is slidably connected with the machine body 1, the machine body 1 is slidably connected with the limit pin 92, the limit pin 92 is slidably connected with the connecting strip 91, the limit pin 92 is provided with the tension spring 93, the limit pin 92 can limit the connecting strip 91, one end of the tension spring 93 is fixedly connected with the machine body 1, the other end of the tension spring 93 is fixedly connected with the limit pin 92, and the tension spring 93 can drive the limit pin 92 to automatically reset through elasticity.

The working principle is as follows: when the unmanned aerial vehicle needs to be carried, the limiting nail 92 is pulled downwards, the limiting nail 92 slides in the direction of separating from the machine body 1, the tension spring 93 is stretched, and when the limiting nail 92 separates from the connecting strip 91, the connecting strip 91 and the undercarriage 5 can be detached from the machine body 1, so that the overall size of the unmanned aerial vehicle can be reduced, and the unmanned aerial vehicle is more convenient to carry;

when needing to change flabellum 7, press two simultaneously and promote piece 82, promote piece 82 and compress spring 85, promote piece 82 and drive joint frame 83 and remove at the in-process that removes, when joint frame 83 breaks away from connecting block 10, alright with connecting cover 81 from the outside of connecting block 10 cunning down, alright remove the spacing to go-between 6 after connecting cover 81 dismantles to alright convenient dismantles go-between 6 from brushless motor 4.

Claims

1. The utility model provides an unmanned aerial vehicle with binocular vision structure, includes organism (1), its characterized in that, be provided with binocular vision camera (2) on organism (1), organism (1) is gone up four evenly distributed's of fixedly connected with wing frame (3), every all install brushless motor (4) on wing frame (3), the contact has undercarriage (5) on organism (1), fixedly connected with connecting block (10) on the output shaft of brushless motor (4), brushless motor (4) are gone up the contact and are had go-between (6), the outside fixedly connected with flabellum (7) of go-between (6), the outside of connecting block (10) is provided with change mechanism (8), the inside of organism (1) is provided with disassembly body (9), disassembly body (9) are including connecting strip (91), spacing nail (92), extension spring (93), fixedly connected with connecting strip (91) on undercarriage (5), the inside sliding connection of organism (1) has spacing nail (92), be provided with extension spring (93) on spacing nail (92).

2. The unmanned aerial vehicle with binocular vision structure of claim 1, characterized in that, change mechanism (8) including connecting cover (81), promote piece (82), joint frame (83), guide arm (84), spring (85), square frame (86), the outside sliding connection of connecting block (10) has connecting cover (81), connecting cover (81) with go up the contact of go-between (6), sliding connection has on connecting cover (81) promotes piece (82), fixedly connected with joint frame (83) on promoting piece (82), joint frame (83) with connecting block (10) sliding connection, the inside fixedly connected with guide arm (84) of connecting cover (81), the outside of guide arm (84) is provided with spring (85), guide arm (84) with promote piece (82) sliding connection.

3. Unmanned aerial vehicle with binocular vision structure of claim 2, wherein a square frame (86) is fixedly connected to the connection cover (81), and the square frame (86) is slidably connected to the connection ring (6).

4. Unmanned aerial vehicle with binocular vision structure of claim 2, wherein one end of the spring (85) is fixedly connected with the connection cover (81), and the other end of the spring (85) is fixedly connected with the pushing block (82).

5. Unmanned aerial vehicle with binocular vision structure of claim 1, wherein the connecting strip (91) is slidably connected with the machine body (1), and the limit pin (92) is slidably connected with the connecting strip (91).

6. The unmanned aerial vehicle with binocular vision structure of claim 1, wherein one end of the tension spring (93) is fixedly connected with the machine body (1), and the other end of the tension spring (93) is fixedly connected with the limit nail (92).