CN219096991U

CN219096991U - Automatic line inspection structure of unmanned aerial vehicle

Info

Publication number: CN219096991U
Application number: CN202223356113.4U
Authority: CN
Inventors: 张波
Original assignee: Jiangsu Jintian Artificial Intelligence Technology Co ltd
Current assignee: Jiangsu Jintian Artificial Intelligence Technology Co ltd
Priority date: 2022-12-14
Filing date: 2022-12-14
Publication date: 2023-05-30
Anticipated expiration: 2032-12-14

Abstract

The utility model relates to an automatic line inspection structure of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body, wherein a signal transmitter is fixedly arranged at the top of the unmanned aerial vehicle main body, a protecting shell is fixedly connected to the bottom of the unmanned aerial vehicle main body, a positioner is fixedly arranged in the protecting shell, a mounting shell is rotatably connected to the bottom of the protecting shell, a line inspection camera is fixedly arranged in the mounting shell, a buffer block is fixedly connected to the bottom of the unmanned aerial vehicle main body, a buffer rod is fixedly connected to the bottom of the buffer block, a piston is fixedly connected to one end, far away from the buffer block, of the buffer rod, and a buffer base is sleeved outside the buffer rod. This unmanned aerial vehicle automatic line structure of patrolling, through the image transmission to the remote terminal internet that patrols the line of patrolling the line camera and signal transmitter cooperation, need not the staff and arrive on the scene personally, reduce the line cost of patrolling, reduce line personnel intensity of labour, cushion when descending through piston, cavity and buffer spring cooperation.

Description

Automatic line inspection structure of unmanned aerial vehicle

Technical Field

The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to an automatic line inspection structure of an unmanned aerial vehicle.

Background

Unmanned aerial vehicle is abbreviated as "unmanned aerial vehicle", english abbreviation "UAV", is unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, or operate independently by on-vehicle computer is complete or intermittent type, unmanned aerial vehicle can divide into for military use and civilian, military use aspect, unmanned aerial vehicle divide into reconnaissance aircraft and target plane, civilian aspect, unmanned aerial vehicle + industry application is the true just need of unmanned aerial vehicle, in aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, rescue, observe wild animal, monitor infectious disease, survey, news report, electric power inspection, relief, film and television shooting, make romantic etc. the application of unmanned aerial vehicle itself has greatly been extended, developed countries are also actively expanding trade application and developing unmanned aerial vehicle technique.

The utility model discloses an unmanned aerial vehicle automatic line inspection device, including the line inspection frame structure, the line inspection frame structure includes camera C type frame, motor support frame, vertical rotation motor, line inspection camera, camera safety cover, safety cover cleaner, cleaner magnet and magnet mounting groove, the both ends of camera C type frame are provided with C type frame curb plate, motor support frame installs in C type frame curb plate one side, vertical rotation motor installs in motor support frame's one side, the inboard just is provided with the safety cover cleaner to the position of line inspection camera of camera C type frame of the utility model, when the line inspection camera rotates to being parallel with camera C type frame, the camera safety cover on line inspection camera top can scrape the contact with the clean sponge of safety cover, realizes the self-cleaning to the camera safety cover, has avoided the camera safety cover to become dirty under complicated weather environment, influences unmanned aerial vehicle's line inspection, and the practicality is stronger.

However, when unmanned aerial vehicle is accomplishing the task of patrolling the line and descending, unmanned aerial vehicle receives the rigidity striking of certain degree, and prior art does not have to patrol the line camera and buffer the protection, after long-time use, patrol the line camera and opportunity have the damage of certain degree, so propose an unmanned aerial vehicle automatic line inspection structure and solve the problem that the aforesaid was proposed.

Disclosure of Invention

Aiming at the defects of the prior art, the utility model provides an automatic line patrol structure of an unmanned aerial vehicle, which has the advantages of good buffering effect and the like, and solves the problem that the line patrol camera is not buffered and protected in the prior art, and the unmanned aerial vehicle has a certain damage to the line patrol camera when finishing line patrol task for landing.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an automatic line structure of patrolling of unmanned aerial vehicle, includes the unmanned aerial vehicle main part, the top fixedly mounted of unmanned aerial vehicle main part has signal transmitter, the bottom fixedly connected with protecting crust of unmanned aerial vehicle main part, the inside fixedly mounted of protecting crust has the locator, the bottom of protecting crust rotates and is connected with the installation shell, the inside fixedly mounted of installation shell has the line camera of patrolling, the bottom fixedly connected with buffer block of unmanned aerial vehicle main part, the bottom fixedly connected with buffer block, the one end fixedly connected with piston of buffer block is kept away from to the buffer rod, the outside of buffer rod has cup jointed the buffering base.

Further, the outside fixedly connected with buffer sleeve of buffer rod, the outside fixedly connected with buffer spring of buffer sleeve, buffer spring keeps away from the one end and the buffering base fixed connection of buffer sleeve.

Further, the inside of buffering base has seted up the cavity, piston and cavity looks adaptation.

Further, a motor is fixedly installed on the inner wall of the protective shell, and a first gear is fixedly connected to an output shaft of the motor.

Further, the inside rotation of protecting crust is connected with the pivot, the bottom and the installation shell fixed connection of pivot.

Further, the second gear is fixedly connected to the outer portion of the rotating shaft, and the first gear is meshed with the second gear.

Further, the top fixedly connected with slider of installation shell, annular spout has been seted up to the inside of protecting crust, slider sliding connection is in the inside of annular spout.

Further, the bottom fixedly connected with rubber pad of buffering base, the quantity of buffer block is four.

Compared with the prior art, the technical scheme of the application has the following beneficial effects:

this unmanned aerial vehicle automatic line structure of patrolling, through the image input to remote terminal internet that patrols the line of patrolling the line camera and signal transmitter cooperation, need not the staff and arrive on the scene personally, replace artifical conventional line of patrolling, improve the line efficiency of patrolling, reduce the line cost of patrolling, reduce line personnel intensity of labour, buffer when descending through piston, cavity and buffer spring cooperation, solved prior art and not have to the line of patrolling the line camera buffering protection, unmanned aerial vehicle is when accomplishing the line task of patrolling and descends, the line of patrolling the problem that the camera opportunity exists the damage of certain degree.

Drawings

FIG. 1 is a schematic diagram of the structure of the present utility model;

FIG. 2 is a schematic diagram of a buffer block according to the present utility model;

fig. 3 is an enlarged schematic view of the structure a shown in fig. 1 according to the present utility model.

In the figure: the unmanned aerial vehicle comprises a unmanned aerial vehicle body 1, a signal transmitter 2, a protective shell 3, a locator 4, a mounting shell 5, a line inspection camera 6, a buffer block 7, a buffer rod 8, a piston 9, a buffer base 10, a buffer sleeve 11, a buffer spring 12, a cavity 13, a motor 14, a first gear 15, a rotating shaft 16, a second gear 17 and a sliding block 18.

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.

Embodiment one:

referring to fig. 1-3, an automatic line inspection structure of an unmanned aerial vehicle in this embodiment includes an unmanned aerial vehicle body 1, a signal transmitter 2 is fixedly installed at the top of the unmanned aerial vehicle body 1, the signal transmitter 2 is connected with a remote terminal internet signal, a protecting shell 3 is fixedly connected with the bottom of the unmanned aerial vehicle body 1, a locator 4 is fixedly installed in the protecting shell 3, and the locator 4 is a GPS locator.

In this embodiment, the bottom rotation of protecting crust 3 is connected with installation shell 5, the top fixedly connected with slider 18 of installation shell 5, annular spout has been seted up to the inside of protecting crust 3, slider 18 sliding connection is in the inside of annular spout, the installation shell 5 of being convenient for rotates, improve the stability of structure, the inside fixed mounting of installation shell 5 has line inspection camera 6, gather the image information of line inspection through line inspection camera 6, remote terminal's inspection personnel can see the real-time video of returning through logging in the internet, judge the circuit condition according to real-time video, and judge position and record according to GPS location, confirm that the aircraft independently returns to descend after accomplishing a flight.

In this embodiment, the bottom fixedly connected with buffer block 7 of unmanned aerial vehicle main part 1, the bottom fixedly connected with buffer rod 8 of buffer block 7, the one end fixedly connected with piston 9 of buffer block 7 is kept away from to buffer rod 8, buffer base 10 has been cup jointed to buffer rod 8's outside, cavity 13 has been seted up to buffer base 10's inside, piston 9 and cavity 13 looks adaptation, when unmanned aerial vehicle main part 1 descends, buffer rod 8 receives inertia downwardly moving, make piston 9 extrude the inside air of cavity 13 to absorb a portion impact force.

It should be noted that, the outside fixedly connected with buffer cover 11 of buffer rod 8, the outside fixedly connected with buffer spring 12 of buffer cover 11, the one end and the buffering base 10 fixed connection that buffer cover 11 were kept away from to buffer spring 12, buffer rod 8 downwardly moving extrudees buffer spring 12 through buffer cover 11, absorb a part impact force through buffer spring 12, the bottom fixedly connected with rubber pad of buffering base 10, the quantity of buffer block 7 is four, supplementary absorption a part impact force through the rubber pad reduces the impact force that patrols line camera 6 received, the protection effect has been improved.

Embodiment two:

referring to fig. 1-3, on the basis of the first embodiment, the motor 14 is fixedly mounted on the inner wall of the protective housing 3, a first gear 15 is fixedly connected to an output shaft of the motor 14, the first gear 15 can be driven to rotate by starting the motor 14, a rotating shaft 16 is rotatably connected to the interior of the protective housing 3, the bottom of the rotating shaft 16 is fixedly connected with the mounting housing 5, a second gear 17 is fixedly connected to the exterior of the rotating shaft 16, the first gear 15 is meshed with the second gear 17, and the first gear 17 can drive the second gear 17 to rotate, so that the rotating shaft 16 drives the mounting housing 5 to rotate.

The purpose of improving the coverage range of the line inspection camera 6 is achieved when the line inspection camera is used, the mounting block 5 can be driven to rotate 360 degrees through the starting motor 14, the image information acquisition of the line inspection camera 6 is wider, and the use convenience is improved.

The working principle of the embodiment is as follows:

when the intelligent line inspection device is used, image information of line inspection is acquired through the line inspection camera 6, information is transmitted to the remote terminal internet through the signal transmitter 2, and after the position is judged and the flight is recorded according to GPS positioning, when the aircraft is confirmed to return to the landing independently, the buffer rod 8 is moved downwards by inertia, so that the piston 9 extrudes air in the cavity 13, and the buffer spring 12 is matched to absorb impact force, so that a protective effect is provided for the high line inspection camera 6.

The beneficial effects of the embodiment are as follows:

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. Without further limitation, an element defined by the phrase "comprising one … …" does not exclude the presence of other like elements in a process, method, article, or apparatus that comprises the element.

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

1. The utility model provides an automatic line structure of patrolling of unmanned aerial vehicle, includes unmanned aerial vehicle main part (1), its characterized in that: the utility model discloses a unmanned aerial vehicle, including unmanned aerial vehicle main part (1), unmanned aerial vehicle main part (1)'s top fixed mounting has signal transmitter (2), the bottom fixedly connected with protecting crust (3) of unmanned aerial vehicle main part (1), the inside fixed mounting of protecting crust (3) has locator (4), the bottom of protecting crust (3) is rotated and is connected with installing shell (5), the inside fixed mounting of installing shell (5) has line inspection camera (6), the bottom fixedly connected with buffer block (7) of unmanned aerial vehicle main part (1), the bottom fixedly connected with buffer rod (8) of buffer block (7), the one end fixedly connected with piston (9) of buffer rod (8) keep away from buffer block (7), the outside of buffer rod (8) has cup jointed buffering base (10).

2. The unmanned aerial vehicle automatic line patrol structure according to claim 1, wherein: the outer fixedly connected with buffer sleeve (11) of buffer rod (8), the outside fixedly connected with buffer spring (12) of buffer sleeve (11), the one end that buffer spring (12) kept away from buffer sleeve (11) is fixedly connected with buffer base (10).

3. The unmanned aerial vehicle automatic line patrol structure according to claim 1, wherein: the inside of buffering base (10) has offered cavity (13), piston (9) and cavity (13) looks adaptation.

4. The unmanned aerial vehicle automatic line patrol structure according to claim 1, wherein: the inner wall of the protective shell (3) is fixedly provided with a motor (14), and an output shaft of the motor (14) is fixedly connected with a first gear (15).

5. The unmanned aerial vehicle automatic line patrol structure according to claim 4, wherein: the inside rotation of protecting crust (3) is connected with pivot (16), the bottom of pivot (16) and installation shell (5) fixed connection.

6. The unmanned aerial vehicle automatic line patrol structure according to claim 5, wherein: the second gear (17) is fixedly connected to the outside of the rotating shaft (16), and the first gear (15) is meshed with the second gear (17).

7. The unmanned aerial vehicle automatic line patrol structure according to claim 1, wherein: the top fixedly connected with slider (18) of installation shell (5), annular spout has been seted up to the inside of protecting crust (3), slider (18) sliding connection is in the inside of annular spout.

8. The unmanned aerial vehicle automatic line patrol structure according to claim 1, wherein: the bottom of the buffer base (10) is fixedly connected with a rubber pad, and the number of the buffer blocks (7) is four.