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A detection drone
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A drone and fuselage technology, applied in the field of drones, can solve the problems of troublesome disassembly and installation of the drone and the spherical mesh shell, and the drone cannot be placed on the ground stably, so as to achieve a reasonable structure setting. Effect
Active Publication Date: 2022-04-01
北京京能能源技术研究有限责任公司
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[0005] The purpose of the present invention is to propose a detection drone, to solve the troublesome disassembly and installation of the drone and the spherical mesh shell in the prior art. When the drone is not in use, it cannot be placed on the ground smoothly, but Problem with rolling back and forth on the ground
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Embodiment 1
[0033] This embodiment proposes a detection drone, such as Figure 1-3 As shown, the detection drone includes a fuselage body 1 and a protective structure 2 of the drone, the fuselage body 1 is arranged inside the protective structure 2, and an opening 201 is set on the protective structure 2, The opening 201 is disposed under the fuselage body 1 .
[0034] The opening 201 is arranged below the fuselage body 1. On the one hand, it is convenient for the fuselage body 1 to be installed / disassembled inside the protective structure 2 through the opening 201; Put it on the ground and don't roll back and forth.
[0035] In the detection drone described in the present invention, the setting of the protective structure 2 can ensure that the flight posture of the detection drone will not change too much when the collision occurs at the low-speed flight speed of the detection drone, and the internal structure and components No damage will occur and patrol missions can continue.
[00...
Embodiment 2
[0088] This embodiment proposes a control method for detecting a drone. The control method for detecting a drone uses the detection drone as described in Embodiment 1. The control method for detecting a drone specifically includes the following steps:
[0089] S101. Detecting the state of a detection drone;
[0090] S102, judging whether the state of the detection drone is in flight operation, if so, then enter S103; if not, then enter S107;
[0091] S103, controlling the extension of the telescopic component 23;
[0092] In step 103, when the detection UAV is flying, the retractable assembly 23 is controlled to extend, so that the opening 201 is reduced relative to the protective structure 2, which can better protect the detection UAV.
[0093] S104, judging whether the unmanned aerial vehicle is out of balance during flight operation, if so, then enter S105; if not, then enter S106;
[0094] S105. Control the flight balance adjustment device 400 to adjust the magnitude of ...
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Abstract
The present invention provides a detection UAV, the detection UAV includes a fuselage main body and a protective structure, the fuselage main body is arranged inside the protective structure, and a retractable component and an opening are arranged on the protective structure , the opening is disposed below the main body of the fuselage. Compared with the prior art, in the detection drone described in the present invention, the opening on the protective structure is arranged below the main body of the fuselage, on the one hand, it is convenient for the main body of the fuselage to be installed / disassembled inside the protective structure through the opening; on the other hand On the one hand, when the detection drone is not in use, it is convenient for the detection drone to be placed on the ground smoothly without rolling back and forth.
Description
technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a detection unmanned aerial vehicle. Background technique [0002] So far, inspections and inspections of internal scenes in power plant boilers mainly involve personnel building an inspection platform, and inspections and inspections on the inspection platform. This traditional inspection method requires a large number of people to spend a lot of time building and dismantling the inspection platform. On the other hand, it is impossible to quickly inspect and inspect the scene inside the boiler. [0003] The patent with application number CN201910465814.5 in the prior art discloses a new configuration omnidirectional coaxial drone, which consists of three parts: a spherical mesh shell, a three-axis internal rotation mechanism, and a coaxial unmanned helicopter. The spherical mesh shell is located on the outermost side of the drone, wrapping the internal rotating mechanism...
Claims
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