CN218317311U

CN218317311U - Multifunctional unmanned aerial vehicle

Info

Publication number: CN218317311U
Application number: CN202221993864.4U
Authority: CN
Inventors: 王杰惠; 胡毕寅; 陈佳鸿
Original assignee: Xinchao Technology Zhejiang Co ltd
Current assignee: Xinchao Technology Zhejiang Co ltd
Priority date: 2022-07-27
Filing date: 2022-07-27
Publication date: 2023-01-17
Anticipated expiration: 2032-07-27

Abstract

The utility model discloses a multifunctional unmanned aerial vehicle, including flight platform, flight platform's lower extreme has set firmly a plurality of year thing hooks, flight platform's lower extreme symmetry has set firmly a plurality of pillars, all is equipped with a plurality of locating holes on the every pillar, is equipped with the loading board between a plurality of pillars, is equipped with fixed establishment on the loading board, and one side of every pillar has all set firmly the connecting rod, and the lower extreme of connecting rod is provided with damper, the utility model discloses rational in infrastructure, fixed position on a plurality of pillars through the adjustable loading board of fixed establishment to adjust the interval between loading board and the flight platform, so that unmanned aerial vehicle carries to the article of co-altitude, and can be convenient for article hook through a plurality of year thing hooks and put to unmanned aerial vehicle, can play certain buffering shock attenuation effect at unmanned aerial vehicle rising landing in-process through damper, can play the effect of the protection of rising and falling, avoid great impact force to cause the damage and lead to unmanned aerial vehicle's life-span to subtract the weak point.

Description

Multifunctional unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field, in particular to multi-functional unmanned aerial vehicle.

Background

Transport unmanned aerial vehicle mainly utilizes the unmanned low latitude aircraft of radio remote control equipment and the program control device manipulation of self-contained for carry article, can reach the destination with article automation, it transports efficiency soon, and can reduce the human cost, consequently, uses very extensively.

But the carrying article often highly differs in size, and current unmanned aerial vehicle does not have shock attenuation buffer function when taking off to land, makes the pressure that the lift undercarriage received very big because of unmanned aerial vehicle dead weight and article weight, and unmanned aerial vehicle damages easily when taking off to land. In view of the above problems, a solution is proposed as follows.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a multifunctional unmanned aerial vehicle has and loads height-adjustable festival, takes off and lands steady advantage.

The above technical object of the present invention can be achieved by the following technical solutions:

the utility model provides a multifunctional unmanned aerial vehicle, includes flight platform, four sides of flight platform are connected with the horn, four the other end of horn all is provided with power component, flight controller and GPS receiver are installed to flight platform's upper end, the camera is installed to flight platform's front end, flight platform's lower extreme has set firmly a plurality of year thing hooks, flight platform's lower extreme symmetry has set firmly a plurality of pillars, every all be equipped with a plurality of locating holes on the pillar, it is a plurality of be equipped with the loading board between the pillar, be equipped with fixing mechanism on the loading board, fixing mechanism cooperatees with the locating hole, just the loading board passes through fixing mechanism fixed connection with a plurality of pillars, every one side of pillar all sets firmly the connecting rod, the lower extreme of connecting rod is provided with damper.

Preferably, the fixing mechanism comprises a plurality of positioning pins, a plurality of grooves are formed in the bearing plate, the positioning pins are respectively slidably located in the grooves, the bearing plate is penetrated through one end of each positioning pin and located in the corresponding positioning hole, and a reset spring is connected between the other end of each positioning pin and the inner wall of each groove.

Preferably, the shock absorption assembly comprises a shock absorption spring and a damping rod, the lower end of the connecting rod is connected with two spring seats, the damping rod is connected between the two spring seats, the shock absorption spring is arranged on the damping rod in a penetrating mode, two ends of the shock absorption spring are connected between the two spring seats respectively, and the lower end of each spring seat is fixedly provided with a buffering bag ball.

Preferably, the power assembly comprises a plurality of motors, the motors are respectively arranged on two sides of the machine arm, and self-locking paddles are arranged on output shafts of the motors.

Preferably, each strut is provided with a plurality of hook holes.

The utility model has the advantages that:

1. through the fixed position of the adjustable loading board of fixed establishment on a plurality of pillars to adjust the interval between loading board and the flight platform, so that unmanned aerial vehicle carries the article of co-altitude not, and can be convenient for article hook through a plurality of thing hooks put to unmanned aerial vehicle on.

2. Can play certain buffering shock attenuation effect at unmanned aerial vehicle lift descending in-process through damper, not only can play the protection effect to the article that transport, also can play the effect of the protection of rising and falling to unmanned aerial vehicle, avoid great impact force to cause the damage and lead to unmanned aerial vehicle's life-span to subtract the weak point to unmanned aerial vehicle.

Drawings

FIG. 1 is a schematic structural diagram of an embodiment;

fig. 2 is an enlarged view of the area a in fig. 1.

Reference numerals are as follows: 1. a flying platform; 2. a horn; 3. a power assembly; 4. a flight controller; 5. a GPS receiver; 6. a camera; 7. a carrying hook; 8. a support post; 9. positioning holes; 10. a carrier plate; 11. a fixing mechanism; 12. a connecting rod; 13. a shock absorbing assembly; 14. positioning pins; 15. a groove; 16. a return spring; 17. a damping spring; 18. a damping rod; 19. a spring seat; 20. a cushioning bladder ball; 21. a motor; 22. a self-locking paddle; 23. and (4) hook holes.

Detailed Description

The following is only the preferred embodiment of the present invention, the protection scope is not limited to this embodiment, and all technical solutions belonging to the idea of the present invention should belong to the protection scope of the present invention. It should also be noted that, for those skilled in the art, various modifications and decorations can be made without departing from the principle of the present invention, and such modifications and decorations should also be regarded as the protection scope of the present invention.

As shown in fig. 1-2, a multi-functional unmanned aerial vehicle, including flying platform 1, four sides of flying platform 1 are connected with horn 2, and the other end of four horn 2 all is provided with power component 3, is convenient for unmanned aerial vehicle flight through power component 3. Power component 3 includes a plurality of motors 21, and a plurality of motors 21 are installed respectively in the both sides of horn 2, all installs auto-lock oar 22 on a plurality of motors 21's the output shaft, rotates through a plurality of motors 21 and can drive a plurality of auto-lock oars 22 respectively and rotate, therefore a plurality of auto-lock oars 22 of accessible rotate and to realize adjusting the height and the direction of unmanned aerial vehicle flight.

Flight controller 4 and GPS receiver 5 are installed to flight platform 1's upper end, and camera 6 is installed to flight platform 1's front end, can receive the signal of unmanned aerial vehicle controller through GPS receiver 5, and through flight of 4 steerable unmanned aerial vehicles of flight controller, the picture in the place ahead when can the person of facilitating the use through camera 6 observes unmanned aerial vehicle and flies.

The lower extreme of flight platform 1 has set firmly a plurality of thing hooks 7 that carry, the lower extreme symmetry of flight platform 1 has set firmly a plurality of pillars 8, all be equipped with a plurality of locating holes 9 on every pillar 8, be equipped with loading board 10 between a plurality of pillars 8, be equipped with fixed establishment 11 on the loading board 10, fixed establishment 11 cooperatees with locating hole 9, and loading board 10 and a plurality of pillars 8 pass through fixed establishment 11 fixed connection, through the fixed position of the adjustable loading board 10 of fixed establishment on a plurality of pillars 8, thereby adjust the interval between loading board 10 and the flight platform 1, so that unmanned aerial vehicle carries the article of co-altitude not, and can be convenient for the article hook through a plurality of thing hooks 7 and put to unmanned aerial vehicle on.

Fixing mechanism 11 includes a plurality of locating pins 14, be equipped with a plurality of recesses 15 on the loading board 10, and a plurality of locating pins 14 are slidable respectively and are located a plurality of recesses 15, loading board 10 is worn to establish to the one end of locating pin 14, and be located locating hole 9, be connected with reset spring 16 between the other end of locating pin 14 and the inner wall of recess 15, through pulling locating pin 14, make the one end of locating pin 14 deviate from locating hole 9, meanwhile reset spring 16 receives the extrusion and produces elasticity, alright adjust loading board 10 to suitable position this moment, adjust the completion back, alright unclamp locating pin 14, reset spring 16 can push in locating pin 14 to the locating hole 9 that corresponds in, in order to realize fixing between loading board 10 and pillar 8, thereby accomplish the regulation to the interval between loading board 10 and the flight platform 1.

One side of every pillar 8 all sets firmly connecting rod 12, the lower extreme of connecting rod 12 is provided with damper 13, can rise the descending in-process at unmanned aerial vehicle through damper 13 and can play certain buffering shock attenuation effect, not only can play the protection effect to the article that transport, also can play the effect of the protection of rising and falling to unmanned aerial vehicle, avoids great impact force to cause the damage and lead to unmanned aerial vehicle's life-span to subtract the weak point to unmanned aerial vehicle.

Damping component 13 includes damping spring 17 and damping rod 18, the lower extreme of connecting rod 12 is connected with two spring holders 19, and damping rod 18 connects between two spring holders 19, damping spring 17 wears to establish on damping rod 18, and both ends are connected respectively between two spring holders 19, the lower extreme of spring holder 19 has set firmly buffering bag ball 20, can play preliminary buffering shock attenuation effect when unmanned aerial vehicle descending contact ground through buffering bag ball 20, later accessible damping rod 18 cooperates damping spring 17's extrusion to produce elasticity, the realization rises the buffering shock-absorbing function of descending in-process to unmanned aerial vehicle.

Every pillar 8 is last all to be equipped with a plurality of hook holes 23, can catch hold of with a hook the protection network in the outside of a plurality of pillars 8 through a plurality of hook holes 23, can play the effect of protection and block all around to the carrying article in the unmanned aerial vehicle transportation.

Claims

1. The utility model provides a multifunctional unmanned aerial vehicle, its characterized in that, includes flight platform (1), four sides of flight platform (1) are connected with horn (2), four the other end of horn (2) all is provided with power component (3), flight controller (4) and GPS receiver (5) are installed to the upper end of flight platform (1), camera (6) are installed to the front end of flight platform (1), the lower extreme of flight platform (1) has set firmly a plurality of year thing hooks (7), the lower extreme symmetry of flight platform (1) has set firmly a plurality of pillars (8), every all be equipped with a plurality of locating holes (9) on pillar (8), it is a plurality of be equipped with loading board (10) between pillar (8), be equipped with fixed establishment (11) on loading board (10), fixed establishment (11) cooperate with locating hole (9), just loading board (10) pass through fixed establishment (11) fixed connection with a plurality of pillars (8), every one side of pillar (8) all has set firmly connecting rod (12), the lower extreme of connecting rod (12) is provided with shock attenuation subassembly (13).

2. The multifunctional unmanned aerial vehicle of claim 1, wherein the fixing mechanism (11) comprises a plurality of positioning pins (14), a plurality of grooves (15) are formed in the bearing plate (10), the positioning pins (14) are slidably located in the grooves (15) respectively, one end of each positioning pin (14) penetrates through the bearing plate (10) and is located in the positioning hole (9), and a return spring (16) is connected between the other end of each positioning pin (14) and the inner wall of each groove (15).

3. The multifunctional unmanned aerial vehicle of claim 2, wherein the shock absorption assembly (13) comprises a shock absorption spring (17) and a damping rod (18), the lower end of the connecting rod (12) is connected with two spring seats (19), the damping rod (18) is connected between the two spring seats (19), the shock absorption spring (17) is arranged on the damping rod (18) in a penetrating manner, two ends of the shock absorption spring are respectively connected between the two spring seats (19), and a buffering bag ball (20) is fixedly arranged at the lower end of the spring seat (19).

4. The multifunctional unmanned aerial vehicle of claim 3, wherein the power assembly (3) comprises a plurality of motors (21), the motors (21) are respectively arranged at two sides of the horn (2), and self-locking paddles (22) are arranged on output shafts of the motors (21).

5. The multifunctional unmanned aerial vehicle of claim 4, characterized in that each of said support posts (8) is provided with a plurality of hook holes (23).