CN213109792U

CN213109792U - Positioning monitoring unmanned aerial vehicle for construction of small station

Info

Publication number: CN213109792U
Application number: CN202022394522.8U
Authority: CN
Inventors: 张丽璇
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-10-24
Filing date: 2020-10-24
Publication date: 2021-05-04
Anticipated expiration: 2030-10-24

Abstract

The utility model provides a positioning monitoring unmanned aerial vehicle for mini-station construction relates to the unmanned aerial vehicle technology field. This positioning monitoring unmanned aerial vehicle for construction of small-size station, including the unmanned aerial vehicle body, unmanned aerial vehicle body surface one side fixedly connected with rotor linking arm, fixed surface is connected with the connecting block on the rotor linking arm, fixed surface is connected with auxiliary drive ware on the connecting block, auxiliary drive ware upper surface swing joint has the main drive ware, main drive ware fixed surface is connected with the screw blade, fixed surface is connected with fixing bolt on the main drive ware. This small-size station construction positioning monitoring unmanned aerial vehicle through setting up shock attenuation silica gel pad, snubber block, first shock attenuation magnet and second shock attenuation magnet, has solved because unmanned aerial vehicle when the whereabouts falls to the ground, controls not good meeting and produces vibrations, has the impact force, and these impact forces not only make unmanned aerial vehicle internal component produce the damage easily, still influence work efficiency's problem.

Description

Positioning monitoring unmanned aerial vehicle for construction of small station

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a small-size station construction location monitoring unmanned aerial vehicle.

Background

An unmanned plane is an unmanned plane which is operated by utilizing a radio remote control device and a self-contained program control device, the unmanned plane is provided with no cockpit, but is provided with an autopilot, a program control device and other devices, and personnel on the ground, a naval vessel or a mother-aircraft remote control station track, position, remotely control, telemeter and digital transmission through radar and other devices. And many local terrains are dangerous or traffic jam, which is not beneficial to the direct detection of ground equipment, and the development of the unmanned aerial vehicle technology and the positioning technology effectively solves the problem.

But present unmanned aerial vehicle environmental monitoring work efficiency is low, and monitoring devices installs and dismantles the troublesome poeration, is not convenient for overhaul it and change, and because unmanned aerial vehicle falls when falling to the ground, controls that not good if can produce vibrations, has the impact force, and these impact forces not only make unmanned aerial vehicle internal component produce the damage easily, still influence work efficiency.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model provides a be not enough to prior art, the utility model provides a small-size station construction location monitoring unmanned aerial vehicle, it is low to have solved present unmanned aerial vehicle environmental monitoring work efficiency who mentions in the background art, monitoring devices installs and dismantles the troublesome poeration, be not convenient for overhaul it and change, and because unmanned aerial vehicle when falling to the ground, control not good can produce vibrations, have the impact force, these impact forces not only make unmanned aerial vehicle internal element produce the damage easily, still influence work efficiency's problem.

(II) technical scheme

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a positioning and monitoring unmanned aerial vehicle for small-sized station construction comprises an unmanned aerial vehicle body, wherein one side of the outer surface of the unmanned aerial vehicle body is fixedly connected with a rotor wing connecting arm, the upper surface of the rotor wing connecting arm is fixedly connected with a connecting block, the upper surface of the connecting block is fixedly connected with an auxiliary driver, the upper surface of the auxiliary driver is movably connected with a main driver, the outer surface of the main driver is fixedly connected with a propeller blade, the upper surface of the main driver is fixedly connected with a fixing bolt, the upper surface of the rotor wing connecting arm is embedded with an airflow hole, a power supply device is arranged inside the unmanned aerial vehicle body, a GPS positioning device is fixedly arranged inside the unmanned aerial vehicle body and positioned on the upper surface of the power supply device, a fixed mounting groove is embedded inside the unmanned aerial vehicle body, one side fixedly connected with limiting plate of fixed mounting groove inner wall is kept away from to powerful reset spring surface, the inside and detection camera joint of fixed mounting groove, unmanned aerial vehicle body bottom fixedly connected with shock attenuation silica gel pad, unmanned aerial vehicle body bottom fixedly connected with damping device, the inside snubber block that is provided with of damping device, surface swing joint has first shock attenuation magnet on the snubber block, snubber block bottom swing joint has second shock attenuation magnet, unmanned aerial vehicle body bottom fixedly connected with observes the camera.

Preferably, the airflow holes are uniformly distributed on the upper surface of the rotor wing connecting arm and penetrate through the rotor wing connecting arm.

Preferably, the auxiliary driver, the main driver, the GPS positioning device and the detection camera are electrically connected to the power supply device, and the detection camera is electrically connected to the observation camera.

Preferably, the number of shock attenuation silica gel pad is two, and is the symmetric distribution about damping device.

Preferably, the number of rotor linking arm is four, and is the symmetric distribution about the unmanned aerial vehicle body.

Preferably, the first and second damper magnets are fixed to the same pole in the damper block.

(III) advantageous effects

The utility model provides a small-size station construction location monitoring unmanned aerial vehicle. The method has the following beneficial effects:

1. this positioning monitoring unmanned aerial vehicle for small-size station construction through setting up fixed mounting groove, card festival groove, powerful reset spring and limiting plate, can make to dismantle more convenient, and stability is good, simple structure, convenient to use, it is rational in infrastructure, it is low to have solved present unmanned aerial vehicle environmental monitoring work efficiency, monitoring devices installs and dismantles the troublesome poeration, is not convenient for overhaul the problem of changing to it.

2. This small-size station construction location monitoring unmanned aerial vehicle, through setting up the shock attenuation silica gel pad, the snubber block, first shock attenuation magnet and second shock attenuation magnet, the principle that utilizes homopolar repulsion mutually, earlier the impact force that will shake the production through the shock attenuation silica gel pad weakens greatly, rethread snubber block, make vibrations effect significantly reduce once more, pass to the unmanned aerial vehicle body at last, effectively cushion to this interval, the safety of unmanned aerial vehicle body internal component and detection camera has been protected, solved because unmanned aerial vehicle falls to the ground, it can produce vibrations to control not good words, the impact force has, these not only make unmanned aerial vehicle internal component produce the impact force easily and damage, still influence work efficiency.

Drawings

Fig. 1 is a schematic structural diagram of the present invention.

Fig. 2 is a schematic side view of the present invention.

Fig. 3 is a schematic view of the bottom view of the present invention.

Fig. 4 is a schematic view of the cross-sectional structure of the present invention.

Fig. 5 is a schematic view of the local enlarged structure of the present invention.

Wherein, 1 unmanned aerial vehicle body, 2 rotor linking arms, 3 connecting blocks, 4 auxiliary drive ware, 5 main drive ware, 6 screw blade, 7 fixing bolt, 8 air current holes, 9 power supply unit, 10GPS positioner, 11 fixed mounting grooves, 12 joint grooves, 13 powerful reset spring, 14 limiting plates, 15 detection camera, 16 shock attenuation silica gel pads, 17 damping device, 18 snubber blocks, 19 first damping magnet, 20 second damping magnet, 21 observation cameras.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

The embodiment of the utility model provides a positioning monitoring unmanned aerial vehicle for construction of small-sized station, as shown in FIGS. 1-5, including unmanned aerial vehicle body 1, one side of the outer surface of unmanned aerial vehicle body 1 is fixedly connected with rotor connecting arm 2, the number of rotor connecting arms 2 is four, and is symmetrically distributed about unmanned aerial vehicle body 1, the upper surface of rotor connecting arm 2 is fixedly connected with connecting block 3, the upper surface of connecting block 3 is fixedly connected with auxiliary driver 4, the upper surface of auxiliary driver 4 is movably connected with main driver 5, the outer surface of main driver 5 is fixedly connected with propeller blade 6, the upper surface of main driver 5 is fixedly connected with fixing bolt 7, airflow hole 8 is embedded on the upper surface of rotor connecting arm 2, airflow hole 8 is uniformly distributed on the upper surface of rotor connecting arm 2, and runs through rotor connecting arm 2, power supply unit 9 is arranged inside unmanned aerial vehicle body 1, GPS positioning device 10 is fixedly installed inside, the fixing installation groove 11 is embedded in the unmanned aerial vehicle body 1, the bottom of the fixing installation groove 11 is fixedly connected with a clamping groove 12, two sides of the inner wall of the fixing installation groove 11 are fixedly connected with a strong reset spring 13, one side of the outer surface of the strong reset spring 13, which is far away from the inner wall of the fixing installation groove 11, is fixedly connected with a limiting plate 14, the fixing installation groove 11, the clamping groove 12, the strong reset spring 13 and the limiting plate 14 are arranged, so that the dismounting is more convenient, the stability is good, the structure is simple, the use is convenient, the structure is reasonable, the problems of low working efficiency of the current unmanned aerial vehicle environment monitoring, troublesome mounting and dismounting operation of a monitoring device and inconvenient maintenance and replacement of the monitoring device are solved, the inside of the fixing installation groove 11 is clamped with a detection camera 15, the bottom of the, the number of the shock absorption silica gel pads 16 is two, the shock absorption silica gel pads are symmetrically distributed about the shock absorption device 17, the shock absorption device 17 is internally provided with a shock absorption block 18, the upper surface of the shock absorption block 18 is movably connected with a first shock absorption magnet 19, the bottom of the shock absorption block 18 is movably connected with a second shock absorption magnet 20, the parts of the first shock absorption magnet 19 and the second shock absorption magnet 20 fixed in the shock absorption block 18 are homopolar, the bottom of the unmanned aerial vehicle body 1 is fixedly connected with an observation camera 21, an auxiliary driver 4, a main driver 5, a GPS positioning device 10 and a detection camera 15 are electrically connected with a power supply device 9, the detection camera 15 is electrically connected with the observation camera 21, and by arranging the shock absorption silica gel pads 16, the shock absorption block 18, the first shock absorption magnet 19 and the second shock absorption magnet 20, the principle that homopolar repulsion is applied, shock generated by the shock absorption silica, through snubber block 18 again, make vibrations effect significantly reduce once more, pass to unmanned aerial vehicle body 1 at last, effectively cushion to this within a definite time, protected 1 internal element of unmanned aerial vehicle body and detection camera 15's safety, solved because unmanned aerial vehicle falls to the ground when, control that not good can produce vibrations, have the impact force, these impact forces not only make unmanned aerial vehicle internal element produce easily and damage, still influence work efficiency's problem.

Theory of operation, in operation, earlier in the fixed mounting groove 11 is gone into to detection camera 15 card, powerful reset spring 13 makes 14 self-holding of limiting plate detect camera 15, then make through joint groove 12 that detection camera 15 stabilizes not rock from top to bottom, make main drive 5 work after that, screw blade 6 rotates, drive unmanned aerial vehicle body 1 and fly up, make unmanned aerial vehicle body 1 detect work, when detecting the completion and need descend, buffering through shock attenuation silica gel pad 16 and damping device 17, make the impact force significantly reduce, effectively cushion impact force, the safety of 1 internal element of unmanned aerial vehicle body and detection camera 15 has been protected, and simple structure, high durability and convenient use.

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

Claims

1. The utility model provides a small-size station construction positioning monitoring unmanned aerial vehicle, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle is characterized in that a rotor connecting arm (2) is fixedly connected to one side of the outer surface of the unmanned aerial vehicle body (1), a connecting block (3) is fixedly connected to the upper surface of the rotor connecting arm (2), an auxiliary driver (4) is fixedly connected to the upper surface of the connecting block (3), a main driver (5) is movably connected to the upper surface of the auxiliary driver (4), propeller blades (6) are fixedly connected to the outer surface of the main driver (5), fixing bolts (7) are fixedly connected to the upper surface of the main driver (5), an airflow hole (8) is embedded in the upper surface of the rotor connecting arm (2), a power supply device (9) is arranged in the unmanned aerial vehicle body (1), a GPS positioning device (10) is fixedly installed on the upper surface of the power supply device (9) in the unmanned aerial vehicle body (1), and a fixing, the bottom of the fixed mounting groove (11) is fixedly connected with a clamping groove (12), two sides of the inner wall of the fixed mounting groove (11) are fixedly connected with a strong reset spring (13), a limit plate (14) is fixedly connected with one side of the outer surface of the strong return spring (13) far away from the inner wall of the fixed mounting groove (11), the interior of the fixed mounting groove (11) is clamped with the detection camera (15), the bottom of the unmanned aerial vehicle body (1) is fixedly connected with a shock absorption silica gel pad (16), the bottom of the unmanned aerial vehicle body (1) is fixedly connected with a damping device (17), a damping block (18) is arranged in the damping device (17), the upper surface of the damping block (18) is movably connected with a first damping magnet (19), the bottom of the shock absorption block (18) is movably connected with a second shock absorption magnet (20), unmanned aerial vehicle body (1) bottom fixedly connected with observes camera (21).

2. The small-sized station construction positioning monitoring unmanned aerial vehicle of claim 1, characterized in that: the airflow holes (8) are uniformly distributed on the upper surface of the rotor wing connecting arm (2) and penetrate through the rotor wing connecting arm (2).

3. The small-sized station construction positioning monitoring unmanned aerial vehicle of claim 1, characterized in that: the auxiliary driver (4), the main driver (5), the GPS positioning device (10) and the detection camera (15) are electrically connected with the power supply device (9), and the detection camera (15) is electrically connected with the observation camera (21).

4. The small-sized station construction positioning monitoring unmanned aerial vehicle of claim 1, characterized in that: the number of shock attenuation silica gel pad (16) is two, and is the symmetric distribution about damping device (17).

5. The small-sized station construction positioning monitoring unmanned aerial vehicle of claim 1, characterized in that: the quantity of rotor linking arm (2) is four, and is the symmetric distribution about unmanned aerial vehicle body (1).

6. The small-sized station construction positioning monitoring unmanned aerial vehicle of claim 1, characterized in that: the parts of the first damping magnet (19) and the second damping magnet (20) fixed in the damping block (18) are homopolar.