CN218967207U

CN218967207U - Unmanned aerial vehicle for inspection

Info

Publication number: CN218967207U
Application number: CN202320189532.9U
Authority: CN
Inventors: 张永钢; 郭咏
Original assignee: Jiangsu Icarus Electric Uav General Technology Co ltd
Current assignee: Jiangsu Icarus Intelligent Technology Co ltd
Priority date: 2023-02-11
Filing date: 2023-02-11
Publication date: 2023-05-05
Anticipated expiration: 2033-02-11

Abstract

The utility model provides an unmanned aerial vehicle for inspection, which comprises an unmanned aerial vehicle main body shell, an outer frame plate, a solar electric plate, a protection component, peripheral components, a camera main body, an induction port, a controller, a first motor, a spiral wing, a storage battery and a line induction plate, wherein the outer frame plate is arranged at the top of the unmanned aerial vehicle main body shell, the solar electric plate is arranged in the middle of the outer frame plate, the protection component is arranged at the left side and the right side of the unmanned aerial vehicle main body shell, the peripheral components are assembled at the inner side of the unmanned aerial vehicle main body shell, the camera main body and the controller are all arranged in the unmanned aerial vehicle main body shell, the induction port is connected with the controller, the first motor is respectively arranged at the left end and the right end of the outer frame plate, the unmanned aerial vehicle can be subjected to shock absorption protection, a spotlight lamp is provided for further improving the night inspection capability of the unmanned aerial vehicle, signal interference of a magnetic field on the unmanned aerial vehicle inspection is effectively prevented, and the inspection effect is enhanced.

Description

Unmanned aerial vehicle for inspection

Technical Field

The utility model relates to an unmanned aerial vehicle for inspection, and belongs to the technical field of unmanned aerial vehicles.

Background

Unmanned aerial vehicle becomes the small-size aircraft that is equipped with to catch the pole now owing to the appearance is small and exquisite, and the energy consumption is low, and easy operation, along with this unmanned aerial vehicle technology's development and popularization, unmanned aerial vehicle is widely used to take photo by plane, agriculture, forestry. Mapping and other fields. At present, unmanned aerial vehicles can be widely used in the inspection aspect, inspection can be only carried out under the condition of good sight line in the daytime at the present stage, inspection is difficult to effectively carry out under the condition of bad sight line or at night, the internal structure of the unmanned aerial vehicle is very precise, and the unmanned aerial vehicle is easy to receive the impact of the ground during take-off and landing, so that internal precise equipment is damaged.

For this reason, chinese patent No. CN212473939U discloses an unmanned aerial vehicle of inspection usefulness, this unmanned aerial vehicle is through being equipped with spotlight cap in the bottom of the body, make unmanned aerial vehicle inspect equally under the condition of night or sight not good, the megaphone installation can send the warning simultaneously, improve the effect of inspection, unmanned aerial vehicle's landing leg is through the effectual impact force that reduces unmanned aerial vehicle landing production of bumper shock absorber, the unmanned aerial vehicle has been protected and has been conveniently inspected simultaneously, but this unmanned aerial vehicle has certain limitation when facing the great condition of secondary magnetic field signal interference, it is difficult to realize inspection work, consequently, an unmanned aerial vehicle of inspection is required to solve the problem that above-mentioned appears now urgently.

Disclosure of Invention

Aiming at the defects of the prior art, the utility model aims to provide the unmanned aerial vehicle for inspection, so as to solve the problems in the background art.

In order to achieve the above object, the present utility model is realized by the following technical scheme: unmanned aerial vehicle for inspection, including unmanned aerial vehicle main part shell, outer frame plate, solar panel, protection subassembly, peripheral component, camera main part, response port, controller, first motor, spiral wing, battery and circuit induction board, unmanned aerial vehicle main part shell top is provided with outer frame plate to solar panel is installed to outer frame plate mid portion, protection subassembly sets up the left and right sides at unmanned aerial vehicle main part shell to the assembly of peripheral component is in unmanned aerial vehicle main part shell's inboard, camera main part and controller are all installed inside unmanned aerial vehicle main part shell, and the response port is connected with the controller, outer frame plate left and right sides both ends are provided with first motor respectively, spiral wing is installed at first motor top, the battery sets up at unmanned aerial vehicle main part shell inside top to the battery is connected with the solar panel bottom, protection subassembly includes second motor, no. one expansion plate, no. two expansion plates, rubber cushion and pressure spring group, second motor bottom is provided with No. one expansion plate below and No. two expansion plates are connected with No. two expansion plates, no. two expansion plates are connected with the battery cushion, no. two expansion plates are connected with the side filter, no. two, and the filter is connected with the signal connection block is provided with the side of the metal cushion, the filter is connected with the signal connection piece, and the signal connection block is equipped with the side of the signal connection piece, the signal connection piece is equipped with the signal connection piece.

Further, the signal filter is connected inside the unmanned aerial vehicle main body shell through setting up fixed buckle.

Further, the upper end and the lower end of the pressure spring group are connected to the second expansion plate in a welding mode.

Further, a rubber cushion is additionally arranged at the bottom of the second expansion plate.

Further, a connecting wire is separately arranged between the battery pack and the spotlight.

Further, the controller is connected with the first motor, the camera body, the storage battery, the second motor and the peripheral component through a plurality of wires.

Further, the circuit induction plate is fixedly connected inside the unmanned aerial vehicle main body shell in a welding mode.

The utility model has the beneficial effects that: according to the unmanned aerial vehicle for inspection, the pressure spring set, the signal filter, the line induction plate, the spotlight and the rubber cushion are added, the plurality of wires inside the unmanned aerial vehicle main body shell are arranged through the line induction plate, so that the internal space is saved, later-stage workers can overhaul and maintain conveniently, meanwhile, the signal filter is added, the signal interference of an external magnetic field on the unmanned aerial vehicle can be prevented, the flight safety of the unmanned aerial vehicle is guaranteed, the spotlight can provide illumination for night inspection of the unmanned aerial vehicle, finally the stability of the unmanned aerial vehicle during landing can be enhanced by the rubber cushion, and the damage of vibration to internal instruments is reduced.

Drawings

Other features, objects and advantages of the present utility model will become more apparent upon reading of the detailed description of non-limiting embodiments, given with reference to the accompanying drawings in which:

fig. 1 is a schematic structural diagram of an unmanned aerial vehicle for inspection according to the present utility model;

fig. 2 is a schematic structural diagram of a protection component of an unmanned aerial vehicle for inspection according to the present utility model;

fig. 3 is a schematic plan view of an internal structure of the unmanned aerial vehicle for inspection according to the present utility model;

in the figure: the unmanned aerial vehicle comprises a 1-unmanned aerial vehicle main body shell, a 2-external frame plate, a 3-solar panel, a 4-protection component, a 5-external component, a 6-camera main body, a 7-induction port, an 8-controller, a 9-first motor, a 10-spiral wing, a 11-storage battery, a 12-circuit induction plate, a 41-second motor, a 42-first expansion plate, a 43-second expansion plate, a 44-rubber cushion, a 45-pressure spring group, a 51-battery group, a 52-spotlight lamp, a 53-metal shell, a 54-signal filter and a 55-connecting block.

Detailed Description

The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.

Referring to fig. 1-3, the present utility model provides a technical solution: an unmanned aerial vehicle for inspection comprises an unmanned aerial vehicle main body shell 1, an outer frame plate 2, a solar electric plate 3, a protection component 4, a peripheral component 5, a camera main body 6, an induction port 7, a controller 8, a first motor 9, a spiral wing 10, a storage battery 11 and a line induction plate 12, wherein the outer frame plate 2 is arranged at the top of the unmanned aerial vehicle main body shell 1, the solar electric plate 3 is arranged at the middle part of the outer frame plate 2, the protection component 4 is arranged at the left side and the right side of the unmanned aerial vehicle main body shell 1, the peripheral component 5 is assembled at the inner side of the unmanned aerial vehicle main body shell 1, the camera main body 6 and the controller 8 are arranged inside the unmanned aerial vehicle main body shell 1, the induction port 7 is connected with the controller 8, the left end and the right end of the outer frame plate 2 are respectively provided with a first motor 9, the spiral wing 10 is arranged at the top of the first motor 9, the battery 11 is arranged at the top end inside the unmanned aerial vehicle main body shell 1, the battery 11 is connected with the bottom end of the solar panel 3, the protection component 4 comprises a second motor 41, a first expansion plate 42, a second expansion plate 43, a rubber cushion 44 and a pressure spring group 45, the bottom of the second motor 41 is provided with the first expansion plate 42, the lower part of the first expansion plate 42 is connected with the second expansion plate 43, the rubber cushion 44 is arranged at the bottom end of the second expansion plate 43, the side surface of the second expansion plate 43 is provided with the pressure spring group 45, the peripheral component 5 comprises a battery pack 51, a spotlight 52, a metal shell 53, a signal filter 54 and a connecting block 55, the left side and the right side of the battery pack 51 are respectively provided with the connecting block 55, the connecting block 55 is provided with the spotlight 52, the metal shell 53 is arranged outside the sensing port 7, the signal filter 54 is arranged inside the unmanned aerial vehicle main body shell 1, and the line induction board 12 is connected to the signal filter 54.

As a first embodiment of the present utility model: the circuit induction plate 12 is inside unmanned aerial vehicle main part shell 1 through welded mode fixed connection, this design adds circuit induction plate 12 inside unmanned aerial vehicle main part shell 1, be favorable to arranging connecting wire, be convenient for save inner space, make things convenient for the staff to overhaul, all through setting up many wire interconnect between controller 8 and first motor 9, camera main part 6, battery 11, second motor 41, and peripheral hardware subassembly 5, this design is controlled through controller 8 is unified, help the staff to use unmanned aerial vehicle to patrol and examine, rubber cushion 44 has been add to No. two expansion plate 43 bottoms, the stability when this design passes through rubber cushion 44 reinforcing unmanned aerial vehicle lift, reduce unmanned aerial vehicle main part shell 1 harm simultaneously, both ends are all connected on No. two expansion plate 43 through welded mode about the pressure spring group 45, the power when being favorable to reinforcing unmanned aerial vehicle lift is used to improve unmanned aerial vehicle, have the shock attenuation effect simultaneously, be provided with connecting wire alone between battery group 51 and the spotlight assembly 52, this design is electric energy supply is improved for electric lamp 52 alone, be favorable to reducing the whole electric energy consumption of unmanned aerial vehicle, it is favorable to reducing unmanned aerial vehicle life time to patrol and examine the time, the filter is guaranteed that unmanned aerial vehicle is connected with the filter 54 through the filter, the filter is easy to reduce the external signal is connected to the unmanned aerial vehicle main part 54, the filter is connected through the filter 54 when the filter is designed to the outside, the filter is easy to reduce the filter, the filter is connected to the filter, the filter is safe, the filter is equipped with the filter, and the power when the filter is easy to use.

As a second embodiment of the present utility model: when using unmanned aerial vehicle to patrol and examine, at first can start controller 8 through the control handle, the induction port 7 gives controller 8 with signal transmission, then controller 8 carries the electric energy in the battery 11 to first motor 9 through the wire in the circuit induction board 12, first motor 9 drives spiral wing 10 and rotates, unmanned aerial vehicle rises upwards, in the flight, avoid receiving external magnetic field interference, signal filter 54 can open always, during the daytime patrol and examine, solar panel 3 can absorb solar energy and charge for battery 11, during the night patrol and examine, the staff can open spotlight lamp 52 through controller 8 and group battery 51, provide the illumination for the camera main part 6 on unmanned aerial vehicle main part shell 1, after the completion patrol and examine the task, unmanned aerial vehicle is retrieved to the staff, unmanned aerial vehicle descends the in-process, staff control second motor 41 promotes expansion plate 41, expansion plate 43 downwardly, pressure spring group 45 produces elastic potential energy in the extrusion deformation process, after rubber 44 contacts ground, elastic potential energy of pressure spring group 45 resets expansion plate 43 upwardly, the unmanned aerial vehicle can be more stable in the time of landing like this.

While the fundamental and principal features of the utility model and advantages of the utility model have been shown and described, it will be apparent to those skilled in the art that the utility model is not limited to the details of the foregoing exemplary embodiments, but may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present disclosure describes embodiments, not every embodiment is provided with a separate embodiment, and that this description is provided for clarity only, and that the disclosure is not limited to the embodiments described in detail below, and that the embodiments described in the examples may be combined as appropriate to form other embodiments that will be apparent to those skilled in the art.

Claims

1. The utility model provides an unmanned aerial vehicle for inspection, includes unmanned aerial vehicle main part shell (1), outer frame plate (2), solar panel (3), protection subassembly (4), peripheral hardware subassembly (5), camera main part (6), response port (7), controller (8), first motor (9), spiral wing (10), battery (11) and circuit induction board (12), its characterized in that, unmanned aerial vehicle main part shell (1) top is provided with outer frame plate (2) to solar panel (3) are installed to outer frame plate (2) mid portion, protection subassembly (4) set up the left and right sides at unmanned aerial vehicle main part shell (1), and peripheral hardware subassembly (5) are assembled in the inboard of unmanned aerial vehicle main part shell (1), camera main part (6) and controller (8) are all installed inside unmanned aerial vehicle main part shell (1), and response port (7) are connected with controller (8), both ends are provided with first motor (9) respectively about outer frame plate (2), first motor (9) top are installed spiral wing (10), battery (11) are installed at the left and right sides of battery (2) and are connected with unmanned aerial vehicle main part (1) top end, and solar panel (11);

the protection assembly (4) comprises a second motor (41), a first expansion plate (42), a second expansion plate (43), a rubber cushion (44) and a pressure spring set (45), wherein the first expansion plate (42) is arranged at the bottom of the second motor (41), the lower part of the first expansion plate (42) is connected with the second expansion plate (43), the rubber cushion (44) is arranged at the bottom end of the second expansion plate (43), and the pressure spring set (45) is assembled on the side surface of the second expansion plate (43);

peripheral hardware subassembly (5) are including group battery (51), spotlight lamp (52), metal casing (53), signal filter (54) and connecting block (55), group battery (51) left and right sides is provided with connecting block (55) respectively to be equipped with spotlight lamp (52) on connecting block (55), metal casing (53) set up in the induction port (7) outside, signal filter (54) set up inside unmanned aerial vehicle main part shell (1) to be connected with circuit induction board (12) on signal filter (54).

2. The unmanned aerial vehicle for inspection according to claim 1, wherein: the circuit induction board (12) is fixedly connected inside the unmanned aerial vehicle main body shell (1) in a welding mode.

3. The unmanned aerial vehicle for inspection according to claim 1, wherein: the controller (8) is connected with the first motor (9), the camera body (6), the storage battery (11), the second motor (41) and the peripheral component (5) through a plurality of wires.

4. The unmanned aerial vehicle for inspection according to claim 1, wherein: the upper end and the lower end of the pressure spring group (45) are connected to the second expansion plate (43) in a welding mode.

5. The unmanned aerial vehicle for inspection according to claim 1, wherein: a rubber cushion (44) is additionally arranged at the bottom of the second expansion plate (43).

6. The unmanned aerial vehicle for inspection according to claim 1, wherein: and a connecting wire is arranged between the battery pack (51) and the spotlight (52) independently.

7. The unmanned aerial vehicle for inspection according to claim 1, wherein: the signal filter (54) is connected inside the unmanned aerial vehicle main body shell (1) through a fixed buckle.