Horizontal mounting and debugging device for unmanned aerial vehicle power system
A system-level, installation and debugging technology, applied in the field of drones, can solve problems such as affecting flight operations, crashes, the inability of drones to hover stably or change the flight direction, to avoid angle offset and improve adaptation. effect of ability
Inactive Publication Date: 2019-05-10
吴清槐
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Problems solved by technology
[0003] The purpose of the present invention is to provide a horizontal installation and debugging device for the UAV power system to solve the angle deviation of the UAV motor assembly proposed in the above background technology, which may easily cause the UAV to be unable to hover stably or change during flight. The flight direction will affect the normal flight operation. In severe cases, there will be a crash, which will reduce the product quality of the drone and affect the normal use of the drone.
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[0024] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0025] see Figure 1-7 , the present invention provides a technical solution: a horizontal installation and debugging device for the power system of an unmanned aerial vehicle, including an assembly platform 1, an assembly track 12, a second track 17 and a telescopic foot support 24, and a support bracket is installed above the assembly platform 1 2, and the supporting rod 3 is installed on the supporting bracket 2, the supporting bracket 2 is a ring structure...
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The invention discloses a horizontal mounting and debugging device for an unmanned aerial vehicle power system. The horizontal mounting and debugging device comprises an assembling platform, assembling tracks, second tracks and extending-and-contracting foot supports. Carrying brackets are mounted above the assembling platform and each provided with a carrying rod. A second adjustment ring is connected to the inner side of each first adjustment ring. Each first track is mounted above the corresponding second adjustment ring and provided with a first connecting groove. The extending-and-contracting foot supports are located below the assembling platform and connected with mounting seats; and in addition, the extending-and-contracting foot supports are connected with the assembling platformthrough the mounting seats. By means of the horizontal mounting and debugging device for the unmanned aerial vehicle power system, a power motor needing to be assembled can be horizontally stabilizedand clamped conveniently, and thus, the motor can be assembled conveniently; the problem that the motor is inclined or deflected in angle in the assembling process is avoided; and assembling stabilityof the motor and flying stability of an unmanned aerial vehicle are improved.
Description
technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a horizontal installation and debugging device for a power system of an unmanned aerial vehicle. Background technique [0002] UAV is a small flying machine, which is mostly used for aerial photography or assisting in the spraying of agricultural chemicals. Most of the existing UAV parts are assembled manually by workers, which is inefficient and the assembly accuracy is not high. Instability is prone to occur during the flight, especially the assembly of the UAV power motor is particularly important. Angle deviations in the motor assembly can easily cause the UAV to be unable to hover stably or change the flight direction during the flight, affecting the normal operation. If the flight operation is serious, there will be a crash, which will reduce the product quality of the drone and affect the normal use of the drone. Contents of the invention [0003] The p...
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IPC IPC(8): B25B11/02B25B27/14
Inventor吴清槐韩叙
Owner吴清槐