CN216468550U

CN216468550U - A hanging cabin device for unmanned aerial vehicle

Info

Publication number: CN216468550U
Application number: CN202122819348.1U
Authority: CN
Inventors: 邓率; 周骏
Original assignee: Liaoning Zhongke New Material Technology Co ltd
Current assignee: Liaoning Zhongke New Material Technology Co ltd
Priority date: 2021-11-17
Filing date: 2021-11-17
Publication date: 2022-05-10
Anticipated expiration: 2031-11-17

Abstract

The utility model discloses a hanging cabin device for an unmanned aerial vehicle, which comprises a main body and two support legs, wherein the support legs are symmetrically assembled at two sides of the lower end of the main body, the lower end of the main body is fixedly assembled with a base, the lower end of the base is fixedly assembled with a hollow cylinder, a clamping plate is inserted into the inner wall of the hollow cylinder, the lower end of the clamping plate is fixedly provided with a connecting rod, the lower end of the connecting rod penetrates through the hollow cylinder and is fixedly provided with a camera, the upper end of the camera is electrically connected with a power supply inside the main body through a lead, the outer wall of the connecting rod is sleeved with a second spring, the utility model provides a hanging cabin device for an unmanned aerial vehicle, which ensures that a camera can be buffered when meeting wind resistance during working and ensures the service life of the camera.

Description

A hanging cabin device for unmanned aerial vehicle

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a hanging cabin device for an unmanned aerial vehicle.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The wide use is reconnoitered in air, is kept watch on, is communicated, is anti-dive, electronic interference etc, and current unmanned aerial vehicle electron hanging cabin camera is rigid connection with the main part, when meetting great windage, breaks easily and damages, and the practicality is poor.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a hanging cabin device for an unmanned aerial vehicle, and aims to solve the problems in the background technology.

In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides a hanging cabin device for unmanned aerial vehicle, includes main part and two landing legs, the lower extreme bilateral symmetry of main part is equipped with the landing leg, the lower extreme fixed mounting of main part has the base, the lower extreme fixed mounting of base has hollow section of thick bamboo, the inner wall of hollow section of thick bamboo is pegged graft and is had the cardboard, the lower extreme fixed mounting of cardboard has the connecting rod, the lower extreme of connecting rod runs through hollow section of thick bamboo and fixed mounting has the camera, the upper end of camera links to each other with the inside power electrical property of main part through the wire, the outer wall of connecting rod has cup jointed the second spring, the one end and the cardboard fixed mounting of second spring, the other end of second spring and the inner chamber bottom surface fixed mounting of hollow section of thick bamboo.

Preferably, the both sides of a hollow section of thick bamboo are all fixed and are equipped with limit structure, two limit structure's lower extreme fixed assembly has the support, the inner wall upper end and the camera looks adhesion of support.

Preferably, limit structure includes the diaphragm, diaphragm fixed mounting is in hollow cylinder's lateral wall, the inner wall of diaphragm runs through and is equipped with the loop bar, the lower extreme and the support fixed mounting of loop bar, the upper end fixed mounting of loop bar has a piece.

Preferably, clamping structures are fixedly assembled on two sides of the support;

the clamping structure comprises a lifting rope, one end of the lifting rope is fixedly assembled with the support, the other end of the lifting rope penetrates through the supporting leg and is fixedly assembled with a clamping block, the clamping block is made of metal, the outer side wall of the supporting leg is fixedly assembled with a magnet, and the magnet is clamped with the clamping block.

Preferably, the lower end of the inner wall of the support is fixedly provided with a buffer structure;

the buffer structure comprises a sleeve, the sleeve is fixedly assembled inside the support, a sliding rod penetrates through the inner wall of the sleeve, a bottom plate is fixedly assembled at the lower end of the sliding rod, a support plate is fixedly assembled at the upper end of the sliding rod, and the upper end of the support plate is fixedly assembled with the inner wall of the sleeve through a first spring.

Preferably, the sponge pad is filled on the inner wall of the hollow cylinder and is positioned between the clamping plate and the top surface of the inner cavity of the hollow cylinder.

Compared with the prior art, the utility model has the beneficial effects that: a hanging cabin device for an unmanned aerial vehicle forms a complete unmanned aerial vehicle frame through the matching of a main body and supporting legs, performs shooting work through a camera, is used for assembling a buffer part and fixing the camera through the connection and matching of a base and a hollow cylinder, ensures the safety of the camera, ensures that the camera can perform buffer motion under the condition of wind resistance, avoids rigid connection and damages the camera, ensures the buffer effect through the matching of a clamping plate and a second spring, and has strong practicability;

the utility model provides a hanging cabin device for an unmanned aerial vehicle, which can ensure that a camera can be buffered when meeting wind resistance during working, and ensure the service life of the camera.

Drawings

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

FIG. 2 is an enlarged view of the structure at A in FIG. 1;

FIG. 3 is an enlarged view of the structure at B in FIG. 1;

fig. 4 is an enlarged schematic view of the structure at C in fig. 1.

In the figure: the device comprises a main body 1, a supporting leg 2, a base 3, a hollow barrel 4, a clamping structure 5, a clamping block 51, a lifting rope 52, a magnet 53, a buffer structure 6, a sleeve 61, a first spring 62, a support plate 63, a slide bar 64, a bottom plate 65, a limiting structure 7, a support block 71, a movable bar 72, a transverse plate 73, a support 8, a camera 9, a sponge pad 10, a connecting bar 11, a second spring 12, a clamping plate 13 and a lead 14.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-4, the utility model provides a hanging cabin device for an unmanned aerial vehicle, which comprises a main body 1 and two support legs 2, wherein the support legs 2 are symmetrically assembled at two sides of the lower end of the main body 1, a base 3 is fixedly assembled at the lower end of the main body 1, a hollow cylinder 4 is fixedly assembled at the lower end of the base 3, a clamping plate 13 is inserted into the inner wall of the hollow cylinder 4, a connecting rod 11 is fixedly assembled at the lower end of the clamping plate 13, the lower end of the connecting rod 11 penetrates through the hollow cylinder 4 and is fixedly assembled with a camera 9, the upper end of the camera 9 is electrically connected with a power supply in the main body 1 through a wire 14, a second spring 12 is sleeved on the outer wall of the connecting rod 11, one end of the second spring 12 is fixedly assembled with the clamping plate 13, and the other end of the second spring 12 is fixedly assembled with the bottom surface of an inner cavity of the hollow cylinder 4.

Through the cooperation of main part 1 and landing leg 2, form complete unmanned aerial vehicle frame, shoot work through camera 9, through the connection cooperation of base 3 and hollow section of thick bamboo 4, be used for assembling bolster and fixed camera 9, guarantee the security of camera 9, under the big condition of windage, guarantee that camera 9 can carry out the cushioning movement, avoid rigid connection, damage camera 9, through the cooperation of cardboard 13 and second spring 12, guarantee the effect of buffering, therefore, the clothes hanger is strong in practicability.

The both sides of hollow section of thick bamboo 4 are all fixed be equipped with limit structure 7, and two limit structure 7's lower extreme fixed be equipped with support 8, the inner wall upper end and the camera looks adhesion of support 8.

Can lift camera 9 through support 8, guarantee the security of camera 9, restrict support 8 through limit structure 7 simultaneously, when camera 9 meets accident's rupture, can play the effect of protection camera 9, avoid it to drop, take place danger.

The limiting structure 7 comprises a transverse plate 73, the transverse plate 73 is fixedly assembled on the side wall of the hollow cylinder 4, the inner wall of the transverse plate 73 is provided with a movable rod 72 in a penetrating mode, the lower end of the movable rod 72 is fixedly assembled with the support 8, and the upper end of the movable rod 72 is fixedly assembled with a support block 71.

When the camera 9 is accidentally broken, the support 8 is driven to move downwards, the movable rods 72 on two sides are driven to move, the movable rods 72 drive the support 71 at the upper end to be clamped to the surface of the transverse plate 73 downwards, the support 8 is protected, the support 8 is prevented from continuously descending, and meanwhile the camera 9 is protected.

Clamping structures 5 are fixedly assembled on two sides of the support 8;

clamping structure 5 includes lifting rope 52, and lifting rope 52's one end and support 8 fixed assembly, lifting rope 52's the other end run through landing leg 2 and fixed assembly fixture block 51, and fixture block 51 is the metal material, and the fixed assembly of lateral wall of landing leg 2 has magnet 53, and magnet 53 and fixture block 51 are connected mutually.

Through the cooperation of fixture block 51 and lifting rope 52, can carry out the secondary protection to support 8, when limit structure 7 damaged equally, can pass through fixture block 51 joint on landing leg 2, play protection support 8 equally, magnet 53 can be when fixture block 51 does not use, adsorbs it, and magnetic force is less than the gravity of support 8.

The lower end of the inner wall of the support 8 is fixedly provided with a buffer structure 6;

the buffer structure 6 comprises a sleeve 61, the sleeve 61 is fixedly assembled inside the support 8, a sliding rod 64 is fixedly assembled on the inner wall of the sleeve 61 in a penetrating manner, a bottom plate 65 is fixedly assembled at the lower end of the sliding rod 64, a support plate 63 is fixedly assembled at the upper end of the sliding rod 64, and the upper end of the support plate 63 is fixedly assembled with the inner wall of the sleeve 61 through a first spring 62.

Before the support 8 contacts with the ground, the bottom plate 65 contacts with the ground in advance, the sliding rod 64 and the support plate 63 are driven to extrude the first spring 62 to deform, buffering is carried out through the elastic force of the first spring 62, and the support 8 is guaranteed to have a buffering effect.

The inner wall of the hollow cylinder 4 is filled with a foam-rubber cushion 10, and the foam-rubber cushion 10 is positioned between the clamping plate 13 and the top surface of the inner cavity of the hollow cylinder 4.

The foam-rubber cushion 10 plays a role of protecting the card 13.

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 utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a draw in cabin device for unmanned aerial vehicle which characterized in that: comprises a main body (1) and two supporting legs (2), wherein the supporting legs (2) are symmetrically assembled at the two sides of the lower end of the main body (1), the lower end of the main body (1) is fixedly provided with a base (3), the lower end of the base (3) is fixedly provided with a hollow cylinder (4), a clamping plate (13) is inserted into the inner wall of the hollow cylinder (4), the lower end of the clamping plate (13) is fixedly provided with a connecting rod (11), the lower end of the connecting rod (11) penetrates through the hollow cylinder (4) and is fixedly provided with a camera (9), the upper end of the camera (9) is electrically connected with a power supply inside the main body (1) through a lead (14), a second spring (12) is sleeved on the outer wall of the connecting rod (11), one end of the second spring (12) is fixedly assembled with the clamping plate (13), the other end of the second spring (12) is fixedly assembled with the bottom surface of the inner cavity of the hollow cylinder (4).

2. A hangar apparatus for unmanned aerial vehicles as claimed in claim 1, wherein: the both sides of hollow section of thick bamboo (4) are all fixed be equipped with limit structure (7), two the lower extreme fixed be equipped with support (8) of limit structure (7), the inner wall upper end and camera (9) the looks adhesion of support (8).

3. A hangar apparatus for unmanned aerial vehicles as claimed in claim 2, wherein: limit structure (7) include diaphragm (73), diaphragm (73) fixed assembly is in the lateral wall of hollow section of thick bamboo (4), the inner wall of diaphragm (73) runs through and is equipped with loop bar (72), the lower extreme and support (8) fixed assembly of loop bar (72), the upper end fixed assembly of loop bar (72) has a piece (71).

4. A hangar apparatus for unmanned aerial vehicles as claimed in claim 2, wherein: clamping structures (5) are fixedly assembled on two sides of the support (8);

clamping structure (5) include lifting rope (52), the one end and support (8) fixed assembly of lifting rope (52), the other end of lifting rope (52) runs through landing leg (2) and fixed assembly has fixture block (51), fixture block (51) are the metal material, the fixed magnet (53) that is equipped with of lateral wall of landing leg (2), magnet (53) and fixture block (51) looks joint.

5. A hangar apparatus for unmanned aerial vehicles as claimed in claim 2, wherein: the lower end of the inner wall of the support (8) is fixedly provided with a buffer structure (6);

the buffer structure (6) comprises a sleeve (61), the sleeve (61) is fixedly assembled inside the support (8), a sliding rod (64) penetrates through the inner wall of the sleeve (61), a bottom plate (65) is fixedly assembled at the lower end of the sliding rod (64), a support plate (63) is fixedly assembled at the upper end of the sliding rod (64), and the upper end of the support plate (63) is fixedly assembled with the inner wall of the sleeve (61) through a first spring (62).

6. A hangar apparatus for unmanned aerial vehicles as claimed in claim 1, wherein: the inner wall of the hollow cylinder (4) is filled with a spongy cushion (10), and the spongy cushion (10) is positioned between the clamping plate (13) and the top surface of the inner cavity of the hollow cylinder (4).