CN219601638U - Unmanned aerial vehicle's supporting equipment - Google Patents

Abstract

The utility model discloses supporting equipment of an unmanned aerial vehicle, which comprises a placing frame, wherein connecting blocks are fixedly connected to two sides of the placing frame, supporting blocks are arranged on the front side and the rear side of the bottom of the placing frame, protruding blocks are fixedly connected to two sides of the top of the supporting blocks, a long rod I is fixedly connected to one side opposite to the two protruding blocks, two sleeve blocks are slidingly connected to the surface of the long rod I, a tension spring I is sleeved on the surface of the long rod I, and two ends of the tension spring I are fixedly connected with the sleeve blocks. The utility model has the advantage of good buffering effect, and in the actual use process, the falling unmanned aerial vehicle can be contacted with the protection pad at the top of the placement frame, so that the contact area between the unmanned aerial vehicle and the supporting equipment is reduced, the surface of the unmanned aerial vehicle is prevented from being scratched, and meanwhile, the impact force caused by the falling unmanned aerial vehicle can be reduced, so that the unmanned aerial vehicle and the supporting equipment are not easy to damage, and the service lives of the unmanned aerial vehicle and the supporting equipment are prolonged.

Description

Unmanned aerial vehicle's supporting equipment

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to supporting equipment of an unmanned aerial vehicle.

Background

Unmanned aerial vehicles are called "unmanned aerial vehicles" for short, are unmanned aerial vehicles operated by radio remote control equipment and self-contained program control devices, or are operated completely or intermittently and autonomously by a vehicle-mounted computer, and compared with unmanned aerial vehicles, unmanned aerial vehicles are more suitable for the tasks of being too "fooled, dirty or dangerous", unmanned aerial vehicles can be classified into military and civil use according to application fields, and unmanned aerial vehicles are classified into reconnaissance and target aircraft.

The user can obtain the video data collected by the search and rescue unmanned aerial vehicle, and the search and rescue unmanned aerial vehicle is a multi-rotor search and rescue unmanned aerial vehicle and can hover at low altitude, so that the multi-axis mechanical arm can be controlled by a remote control mode to execute search and rescue work, such as opening a small stone or an obstacle, and the like, so that the search and rescue requirement can be met.

Although the multi-axis mechanical arm can be controlled to execute search and rescue work in a remote control mode, a certain impact force can be generated when the existing unmanned aerial vehicle falls onto the surface of supporting equipment, the unmanned aerial vehicle is easy to scrape the surface of the unmanned aerial vehicle when being in direct contact with the supporting equipment, and the like, and meanwhile, the impact force generated between the unmanned aerial vehicle and the supporting equipment can cause damage to the unmanned aerial vehicle and the supporting equipment, so that the service lives of the unmanned aerial vehicle and the supporting equipment are shortened, and the supporting equipment of the unmanned aerial vehicle is urgent to be developed for solving the problem.

Disclosure of Invention

The utility model aims to provide the supporting equipment of the unmanned aerial vehicle, which has the advantage of good buffering effect and solves the problems of the background technology.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a supporting equipment of unmanned aerial vehicle, includes the rack, the equal fixedly connected with connecting block in both sides of rack, the front side and the rear side of rack bottom all are provided with the supporting shoe, the equal fixedly connected with lug in both sides at supporting shoe top, one side fixedly connected with stock one that two lugs are relative, the surface sliding connection of stock one has two cover pieces, the surface cover of stock one is equipped with extension spring one, the both ends of extension spring one all with cover piece fixed connection, the top fixedly connected with connecting piece one of cover piece, the inner chamber rotation of connecting piece one is connected with the regulating block, the equal fixedly connected with elastic component in front side and the rear side of rack bottom, the equal fixedly connected with connecting piece two in both sides of elastic component bottom, one side and the connecting piece two rotation of regulating block, the four corners of rack bottom all is provided with the cylinder, the inner chamber sliding connection of cylinder has the kicking block, the top fixedly connected with stock two, the surface cover of stock two is equipped with extension spring two, the extension spring two, two and the inner chamber rotation of connecting piece one is connected with the connecting piece one, the inner chamber rotation of connecting piece one is connected with the connecting piece three with the connecting piece, the connecting piece is connected with the cylinder to the three respectively.

Preferably, the top of rack fixedly connected with protection pad, protection pad's shape is the arc.

Preferably, both sides at the top of the supporting block are provided with sliding grooves, the inner cavity of each sliding groove is connected with a sliding block in a sliding manner, and the top of each sliding block is fixedly connected with the corresponding sleeve block.

Preferably, the inner cavity of the sleeve block on the left side is connected with a baffle in a sliding manner, and one side of the baffle is fixedly connected with the sleeve block on the right side.

Preferably, a telescopic structure is formed between the sleeve block and the tension spring I, and the maximum moving distance of the sleeve block is equal to the deformation amount of the tension spring I.

Preferably, round holes are formed in one side of the placement frame, and the number of the round holes is three.

Compared with the prior art, the utility model has the following beneficial effects:

1. according to the utility model, through the matched use of the convex block, the first long rod, the sleeve block, the first tension spring, the first connecting piece, the adjusting block, the elastic component, the second connecting piece, the cylinder, the round block, the second long rod, the second tension spring, the fixed block and the third connecting piece, the unmanned aerial vehicle is buffered, and the supporting device of the unmanned aerial vehicle has the advantage of good buffering effect.

2. According to the utility model, through the arrangement of the protection pad, the unmanned aerial vehicle is protected, the service life of the unmanned aerial vehicle is prolonged, through the matched use of the sliding groove and the sliding block, the limit effect on the sleeve block is realized, the stability of the sleeve block during moving is improved, through the arrangement of the baffle, the effect of shielding the elastic assembly is realized, the elastic assembly is prevented from contacting with the tension spring I, and through the arrangement of the round hole, the effect of saving the manufacturing cost is realized.

Drawings

FIG. 1 is a schematic perspective view of the present utility model;

FIG. 2 is a schematic perspective view of a partial structure of the present utility model;

fig. 3 is a perspective sectional view of a partial structure of the present utility model.

In the figure: 1. a placing rack; 2. a connecting block; 3. a support block; 4. a bump; 5. a long rod I; 6. sleeving blocks; 7. a tension spring I; 8. a first connecting piece; 9. an adjusting block; 10. an elastic component; 11. a second connecting piece; 12. a cylinder; 13. round blocks; 14. a second long rod; 15. a tension spring II; 16. a fixed block; 17. a third connecting piece; 18. a protective pad; 19. a chute; 20. a slide block; 21. and a baffle.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-3, the present utility model provides a technical solution: the unmanned aerial vehicle support device comprises a placement frame 1, wherein one side of the placement frame 1 is provided with round holes, the number of the round holes is three, the effect of saving manufacturing cost is achieved through the arrangement of the round holes, the two sides of the placement frame 1 are fixedly connected with connecting blocks 2, the front side and the rear side of the bottom of the placement frame 1 are respectively provided with a support block 3, the two sides of the top of the support block 3 are fixedly connected with bumps 4, one side opposite to the two bumps 4 is fixedly connected with a long rod I5, the surface of the long rod I5 is slidingly connected with two sleeve blocks 6, the surface of the long rod I5 is sleeved with a tension spring I7, a telescopic structure is formed between the sleeve blocks 6 and the tension spring I7, the maximum moving distance of the sleeve blocks 6 is equal to the deformation of the tension spring I7, the two ends of the tension spring I7 are fixedly connected with the sleeve blocks 6, the top of the sleeve blocks 6 is fixedly connected with a connecting piece I8, the inner cavity of the first connecting piece 8 is rotationally connected with the regulating block 9, the front side and the rear side of the bottom of the placing frame 1 are fixedly connected with the elastic component 10, two sides of the bottom of the elastic component 10 are fixedly connected with the second connecting piece 11, one side of the regulating block 9 is rotationally connected with the second connecting piece 11, four corners of the bottom of the placing frame 1 are respectively provided with the cylinder 12, the inner cavity of the cylinder 12 is slidingly connected with the round block 13, the top of the round block 13 is fixedly connected with the second long rod 14, the surface of the second long rod 14 is sleeved with the second tension spring 15, two ends of the second tension spring 15 are respectively fixedly connected with the cylinder 12 and the round block 13, one end of the second long rod 14 penetrates to the outer side of the cylinder 12 and is fixedly connected with the fixed block 16, the surface of the fixed block 16 is rotationally connected with the third connecting piece 17, and the top of the third connecting piece 17 is fixedly connected with the connecting block 2.

In the utility model, the following components are added: the top fixedly connected with protection pad 18 of rack 1, the shape of protection pad 18 is the arc, through the setting of protection pad 18, has played the effect of protecting unmanned aerial vehicle, has prolonged unmanned aerial vehicle's life.

In the utility model, the following components are added: the spout 19 has all been seted up to both sides at supporting shoe 3 top, and the inner chamber sliding connection of spout 19 has slider 20, and slider 20's top and cover piece 6 fixed connection through the cooperation of spout 19 and slider 20 use, has played the effect of spacing cover piece 6, has improved the stability of cover piece 6 when removing.

In the utility model, the following components are added: the inner cavity of the left sleeve block 6 is slidably connected with a baffle 21, one side of the baffle 21 is fixedly connected with the right sleeve block 6, and the baffle 21 plays a role of shielding the elastic assembly 10 and prevents the elastic assembly 10 from contacting the tension spring 7.

Working principle: when the unmanned aerial vehicle is used, a user firstly contacts with the protection pad 18 to prevent the unmanned aerial vehicle from scraping when the unmanned aerial vehicle falls into the top of the placement frame 1, the placement frame 1 drives the connection block 2 to move when being pressed down, the connection block 2 drives the connection piece III 17 to move, the connection piece III 17 drives the fixed block 16 to move, the fixed block 16 drives the long rod II 14 to shrink into the inner cavity of the cylinder 12, the cylinder 12 drives the round block 13 to move, the round block 13 drives the tension spring II 15 to stretch, the placement frame 1 drives the elastic component 10 to move when moving downwards, the elastic component 10 drives the connection piece II 11 to move, the connection piece II drives the two connection pieces I8 to move back to back through the adjusting block 9, the connection piece I8 drives the sleeve block 6 to move, the tension spring I7 is driven to stretch when moving, the sleeve block 6 drives the baffle 21 to move, and the elastic component 10 compresses with the baffle 21 when moving downwards, so that the purpose of buffering the unmanned aerial vehicle can be achieved.

It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

The electrical components are all connected with an external main controller and 220V mains supply, and the main controller can be conventional known equipment for controlling a computer and the like.

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

Claims (6)

1. Supporting equipment of unmanned aerial vehicle, including rack (1), its characterized in that: connecting blocks (2) are fixedly connected to two sides of the placement frame (1), supporting blocks (3) are arranged on the front side and the rear side of the bottom of the placement frame (1), protruding blocks (4) are fixedly connected to two sides of the top of each supporting block (3), a long rod I (5) is fixedly connected to one side, opposite to the two protruding blocks (4), two sleeve blocks (6) are slidably connected to the surface of the long rod I (5), tension springs I (7) are sleeved on the surface of the long rod I (5), two ends of each tension spring I (7) are fixedly connected with the corresponding sleeve block (6), connecting pieces I (8) are fixedly connected to the top of each sleeve block (6), the inner cavity of the first connecting piece (8) is rotationally connected with an adjusting block (9), the front side and the rear side of the bottom of the placing frame (1) are fixedly connected with an elastic component (10), two sides of the bottom of the elastic component (10) are fixedly connected with a second connecting piece (11), one side of the adjusting block (9) is rotationally connected with the second connecting piece (11), four corners of the bottom of the placing frame (1) are respectively provided with a cylinder (12), the inner cavity of the cylinder (12) is slidably connected with a round block (13), the top of the round block (13) is fixedly connected with a second long rod (14), the surface of the second long rod (14) is sleeved with a second tension spring (15), two ends of the tension spring II (15) are fixedly connected with the cylinder (12) and the round block (13) respectively, one end of the long rod II (14) penetrates through the outer side of the cylinder (12) and is fixedly connected with the fixing block (16), the surface of the fixing block (16) is rotationally connected with the connecting piece III (17), and the top of the connecting piece III (17) is fixedly connected with the connecting block (2).

2. A support device for an unmanned aerial vehicle according to claim 1, wherein: the top of rack (1) fixedly connected with protection pad (18), protection pad (18) shape is the arc.

3. A support device for an unmanned aerial vehicle according to claim 1, wherein: both sides at the top of the supporting block (3) are provided with sliding grooves (19), an inner cavity of each sliding groove (19) is connected with a sliding block (20) in a sliding mode, and the top of each sliding block (20) is fixedly connected with the corresponding sleeve block (6).

4. A support device for an unmanned aerial vehicle according to claim 1, wherein: the inner cavity of the sleeve block (6) on the left side is connected with a baffle plate (21) in a sliding mode, and one side of the baffle plate (21) is fixedly connected with the sleeve block (6) on the right side.

5. A support device for an unmanned aerial vehicle according to claim 1, wherein: a telescopic structure is formed between the sleeve block (6) and the tension spring I (7), and the maximum moving distance of the sleeve block (6) is equal to the deformation of the tension spring I (7).

6. A support device for an unmanned aerial vehicle according to claim 1, wherein: round holes are formed in one side of the placement frame (1), and the number of the round holes is three.