CN210707885U - Unmanned aerial vehicle is patrolled and examined to electric power - Google Patents
Unmanned aerial vehicle is patrolled and examined to electric power Download PDFInfo
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- CN210707885U CN210707885U CN201921242731.1U CN201921242731U CN210707885U CN 210707885 U CN210707885 U CN 210707885U CN 201921242731 U CN201921242731 U CN 201921242731U CN 210707885 U CN210707885 U CN 210707885U
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Abstract
The utility model provides an electric power inspection unmanned aerial vehicle, which is provided with a flying mechanism and a carrying mechanism; the flight mechanism and the carrying mechanism are respectively connected with the unmanned aerial vehicle main body; the flying mechanism comprises more than four flying components; the flight assembly comprises a first electric telescopic rod, a motor, a rotating shaft, a second electric telescopic rod and a propeller blade; one end of the first electric telescopic rod is connected with the unmanned aerial vehicle main body, and the other end of the first electric telescopic rod is connected with the motor; the motor is connected with the rotating shaft; the propeller blade is connected with the rotating shaft through a second electric telescopic rod; first electric telescopic handle, motor and second electric telescopic handle are connected with the controller electricity respectively, and during the use, not only the first telescopic link of accessible adjusts self volume size according to flight environment, and accommodation is wide, still can change the pulling force that sprays unmanned aerial vehicle according to the mode of the weight regulation propeller blade diameter of the equipment that carries on through the second telescopic link, and the low power dissipation has improved the duration of patrolling and examining unmanned aerial vehicle.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, in particular to electric power patrols and examines unmanned aerial vehicle.
Background
The unmanned aerial vehicle is also called as an aerial robot, and is controlled by a handheld remote control or an onboard computer program control system, compared with a manned aircraft, the unmanned aerial vehicle is simple in structure and low in use cost, not only can complete tasks executed by a piloted aircraft, but also is more suitable for tasks which are not suitable for being executed by the manned aircraft, such as detection in dangerous areas, aerial rescue command and remote sensing monitoring. The unmanned aerial vehicle for electric power inspection at present mainly has four rotors, an unmanned helicopter and a fixed-wing unmanned aerial vehicle.
However, the existing power inspection unmanned aerial vehicle still has the following disadvantages:
1. because wire, shaft tower are various on the high tension transmission line, consequently cause the flight clearance little, lead to too big unmanned aerial vehicle to patrol, and unmanned aerial vehicle's usage has been restricted again to the unmanned aerial vehicle of undersize, can't adjust self volume size according to flight environment.
2. Because patrol and examine unmanned aerial vehicle and need carry on the check out test set of various weight differences according to the user demand usually, and current patrol and examine unmanned aerial vehicle adopts the mode of adjusting motor rotational speed to change unmanned aerial vehicle's pulling force usually, and the consumption is great, great reduction patrol and examine unmanned aerial vehicle's duration.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
In order to solve the above problem of the prior art, the utility model provides an unmanned aerial vehicle is patrolled and examined to electric power can be according to actual demand automatically regulated self volume, and accommodation is wide and the low power dissipation.
(II) technical scheme
In order to achieve the above object, the utility model discloses a main technical scheme include:
an electric power inspection unmanned aerial vehicle comprises an unmanned aerial vehicle main body, a controller arranged in the unmanned aerial vehicle main body, a flying mechanism and a carrying mechanism;
the flight mechanism and the carrying mechanism are respectively connected with the unmanned aerial vehicle main body;
the flying mechanism comprises more than four flying assemblies;
the flight assembly comprises a first electric telescopic rod, a motor, a rotating shaft, a second electric telescopic rod and a propeller blade;
one end of the first electric telescopic rod is connected with the unmanned aerial vehicle main body, and the other end of the first electric telescopic rod is connected with the motor;
the motor is connected with the rotating shaft;
the propeller blade is connected with the rotating shaft through the second electric telescopic rod;
the first electric telescopic rod, the motor and the second electric telescopic rod are respectively electrically connected with the controller.
Furthermore, an insulating shell is arranged outside the unmanned aerial vehicle main body.
Further, carry on the one end of mechanism with the connection can be dismantled to the unmanned aerial vehicle main part, the other end is equipped with connecting portion.
Further, the first electric telescopic rod and the second electric telescopic rod are both multi-stage electric telescopic rods.
Further, still include the supporting legs, the supporting legs with the unmanned aerial vehicle main part is connected.
(III) advantageous effects
The beneficial effects of the utility model reside in that: by arranging the flying mechanism and the carrying mechanism; the flight mechanism and the carrying mechanism are respectively connected with the unmanned aerial vehicle main body; the flying mechanism comprises more than four flying components; the flight assembly comprises a first electric telescopic rod, a motor, a rotating shaft, a second electric telescopic rod and a propeller blade; one end of the first electric telescopic rod is connected with the unmanned aerial vehicle main body, and the other end of the first electric telescopic rod is connected with the motor; the motor is connected with the rotating shaft; the propeller blade is connected with the rotating shaft through a second electric telescopic rod; first electric telescopic handle, motor and second electric telescopic handle are connected with the controller electricity respectively, and during the use, not only the first telescopic link of accessible adjusts self volume size according to flight environment, and accommodation is wide, still can change the pulling force that sprays unmanned aerial vehicle according to the mode of the weight regulation propeller blade diameter of the equipment that carries on through the second telescopic link, and the low power dissipation has improved the duration of patrolling and examining unmanned aerial vehicle.
Drawings
Fig. 1 is the embodiment of the utility model provides an unmanned aerial vehicle's overall structure schematic diagram is patrolled and examined to electric power.
[ description of reference ]
1: an unmanned aerial vehicle main body; 2: a first electric telescopic rod; 3: a motor; 4: a rotating shaft; 5: a second electric telescopic rod; 6: a propeller blade; 7: a mounting mechanism; 8: support the feet.
Detailed Description
For a better understanding of the present invention, reference will now be made in detail to the present invention, examples of which are illustrated in the accompanying drawings.
Referring to fig. 1, the power inspection unmanned aerial vehicle comprises an unmanned aerial vehicle main body, a controller arranged in the unmanned aerial vehicle main body, a flying mechanism and a carrying mechanism;
the flight mechanism and the carrying mechanism are respectively connected with the unmanned aerial vehicle main body;
the flying mechanism comprises more than four flying assemblies;
the flight assembly comprises a first electric telescopic rod, a motor, a rotating shaft, a second electric telescopic rod and a propeller blade;
one end of the first electric telescopic rod is connected with the unmanned aerial vehicle main body, and the other end of the first electric telescopic rod is connected with the motor;
the motor is connected with the rotating shaft;
the propeller blade is connected with the rotating shaft through the second electric telescopic rod;
the first electric telescopic rod, the motor and the second electric telescopic rod are respectively electrically connected with the controller.
The working principle of the utility model is as follows:
when the electric power inspection unmanned aerial vehicle is needed, the unmanned aerial vehicle is taken out, the related detection equipment is connected with the main body of the unmanned aerial vehicle through the carrying mechanism according to the requirement, the second telescopic rod is controlled by the controller to stretch and retract according to the weight of the detection equipment to reach the designated length so as to adapt to the inspection equipment with different weights, in addition, according to the fluid mechanics principle, the larger the diameter of the propeller blade is, the larger the tension is, the efficiency is improved, the technical problems that the tension of the unmanned aerial vehicle is changed by adjusting the rotating speed of the motor and the power consumption is larger in the conventional inspection unmanned aerial vehicle are effectively solved, then the controller controls the motor of each flight assembly to rotate, so as to drive the rotating shaft to rotate, the rotating shaft drives the propeller blade connected with the rotating shaft to rotate to perform electric power inspection, and in the inspection process, the controller can control the first telescopic rod to adjust the, the application range is wide.
As can be seen from the above description, by providing the flying mechanism and the carrying mechanism; the flight mechanism and the carrying mechanism are respectively connected with the unmanned aerial vehicle main body; the flying mechanism comprises more than four flying components; the flight assembly comprises a first electric telescopic rod, a motor, a rotating shaft, a second electric telescopic rod and a propeller blade; one end of the first electric telescopic rod is connected with the unmanned aerial vehicle main body, and the other end of the first electric telescopic rod is connected with the motor; the motor is connected with the rotating shaft; the propeller blade is connected with the rotating shaft through a second electric telescopic rod; first electric telescopic handle, motor and second electric telescopic handle are connected with the controller electricity respectively, and during the use, not only the first telescopic link of accessible adjusts self volume size according to flight environment, and accommodation is wide, still can change the pulling force that sprays unmanned aerial vehicle according to the mode of the weight regulation propeller blade diameter of the equipment that carries on through the second telescopic link, and the low power dissipation has improved the duration of patrolling and examining unmanned aerial vehicle.
Furthermore, an insulating shell is arranged outside the unmanned aerial vehicle main body.
According to the above description, through setting up the unmanned aerial vehicle main part is equipped with insulating housing outward, can effectively guarantee the normal work of each inside electronic component of unmanned aerial vehicle main part.
Further, carry on the one end of mechanism with the connection can be dismantled to the unmanned aerial vehicle main part, the other end is equipped with connecting portion.
According to the above description, through setting up the one end of carrying mechanism with the connection can be dismantled to the unmanned aerial vehicle main part, and the other end is equipped with connecting portion, is convenient for change carrying mechanism, sets up connecting portion moreover, is convenient for connect and patrols and examines equipment.
Further, the first electric telescopic rod and the second electric telescopic rod are both multi-stage electric telescopic rods.
According to the above description, the first electric telescopic rod and the second electric telescopic rod are both multi-stage electric telescopic rods, so that the adjustment can be conveniently carried out according to the use requirements.
Further, still include the supporting legs, the supporting legs with the unmanned aerial vehicle main part is connected.
Known by the above-mentioned description, through setting up the supporting legs, the supporting legs with the unmanned aerial vehicle main part is connected, is convenient for carry out the shock attenuation when unmanned aerial vehicle descends.
Example two
Referring to fig. 1, the power inspection unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, a controller arranged in the unmanned aerial vehicle main body 1, a flying mechanism and a carrying mechanism 7;
the flying mechanism and the carrying mechanism 7 are respectively connected with the unmanned aerial vehicle main body 1;
the flying mechanism comprises more than four flying assemblies;
the flight assembly comprises a first electric telescopic rod 2, a motor 3, a rotating shaft 4, a second electric telescopic rod 5 and a propeller blade 6;
one end of the first electric telescopic rod 2 is connected with the unmanned aerial vehicle main body 1, and the other end of the first electric telescopic rod is connected with the motor 3, and the first electric telescopic rod and the motor can be connected in a welding mode;
the motor 3 is connected with the rotating shaft 4;
the propeller blade 6 is connected with the rotating shaft 4 through the second electric telescopic rod 5;
the first electric telescopic rod 2, the motor 3 and the second electric telescopic rod 5 are electrically connected with the controller respectively.
An insulating shell is arranged outside the unmanned aerial vehicle main body 1.
Carry on mechanism 7's one end with unmanned aerial vehicle main part 1 can dismantle the connection, and the other end is equipped with connecting portion.
The first electric telescopic rod 2 and the second electric telescopic rod 5 are both multi-stage electric telescopic rods.
Still include supporting legs 8, supporting legs 8 with unmanned aerial vehicle main part 1 is connected.
The above mentioned is only the embodiment of the present invention, and not the limitation of the patent scope of the present invention, all the equivalent transformations made by the contents of the specification and the drawings, or the direct or indirect application in the related technical field, are included in the patent protection scope of the present invention.
Claims (5)
1. An electric power inspection unmanned aerial vehicle comprises an unmanned aerial vehicle main body and a controller arranged in the unmanned aerial vehicle main body, and is characterized by further comprising a flying mechanism and a carrying mechanism;
the flight mechanism and the carrying mechanism are respectively connected with the unmanned aerial vehicle main body;
the flying mechanism comprises more than four flying assemblies;
the flight assembly comprises a first electric telescopic rod, a motor, a rotating shaft, a second electric telescopic rod and a propeller blade;
one end of the first electric telescopic rod is connected with the unmanned aerial vehicle main body, and the other end of the first electric telescopic rod is connected with the motor;
the motor is connected with the rotating shaft;
the propeller blade is connected with the rotating shaft through the second electric telescopic rod;
the first electric telescopic rod, the motor and the second electric telescopic rod are respectively electrically connected with the controller.
2. The power inspection unmanned aerial vehicle of claim 1, wherein an insulating housing is provided outside the unmanned aerial vehicle body.
3. The power inspection unmanned aerial vehicle of claim 1, wherein one end of the carrying mechanism is detachably connected with the unmanned aerial vehicle main body, and the other end is provided with a connecting portion.
4. The power inspection unmanned aerial vehicle of claim 1, wherein the first and second electric telescoping rods are multi-stage electric telescoping rods.
5. The power inspection unmanned aerial vehicle of claim 1, further comprising support legs connected with the unmanned aerial vehicle main body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921242731.1U CN210707885U (en) | 2019-08-02 | 2019-08-02 | Unmanned aerial vehicle is patrolled and examined to electric power |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921242731.1U CN210707885U (en) | 2019-08-02 | 2019-08-02 | Unmanned aerial vehicle is patrolled and examined to electric power |
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| Publication Number | Publication Date |
|---|---|
| CN210707885U true CN210707885U (en) | 2020-06-09 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921242731.1U Active CN210707885U (en) | 2019-08-02 | 2019-08-02 | Unmanned aerial vehicle is patrolled and examined to electric power |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20220332410A1 (en) * | 2021-04-19 | 2022-10-20 | Hyundai Motor Company | Fail safety apparatus of air mobility |
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2019
- 2019-08-02 CN CN201921242731.1U patent/CN210707885U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20220332410A1 (en) * | 2021-04-19 | 2022-10-20 | Hyundai Motor Company | Fail safety apparatus of air mobility |
| US11787530B2 (en) * | 2021-04-19 | 2023-10-17 | Hyundai Motor Company | Fail safety apparatus of air mobility |
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