A method for balancing the center of gravity of an unmanned aerial vehicle and the unmanned aerial vehicle
An unmanned aerial vehicle (UAV) and balancing technology, applied in the UAV field, can solve problems such as difficulty in normal and stable flight of UAVs, affecting the normal operation of UAVs, crashes of UAVs, etc., to ensure load consistency and improve flight performance. Reliability and service life, the effect of improving service life and reliability
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Embodiment 1
[0041] figure 1 The structure of the drone provided by the embodiment of the present invention, such as figure 1 As shown, this embodiment provides a drone, which can be applied to border defense patrol, aviation imaging, distribution distribution, construction site surveying, agricultural plant protection, manned flight, etc., this embodiment does not perform specific application scenarios for drones. limit. Further, the present embodiment will be specified as an example of a manned drone as an example, but it can be understood that the drone provided by the present invention can also be a non-carrier-type drone.
[0042] Specifically, the drone includes a body 3, a rotor 2, a flying control system, a center of gravity flattening means 1, and a landing gear 4, and the like. The body 3 is made of metal material, providing support and protection for the entire drone, and the body 3 is configured along its longitudinal centerline to ensure the stability of the drone structure; the ...
Embodiment 2
[0061] This embodiment provides a center of graft method of drone and drone, and the basic structure of the drone provided in the present embodiment is identical, only rotor 2 and flying control only. There is a difference in the setting of the system, and the present embodiment is no longer described in the same structure as the embodiment.
[0062] In the present embodiment, the rotor 2 is only provided with a set, and the rotation center axis of the rotor 2 passes through the center of gravity of the drone itself. The drive control unit includes a steering machine, and a steering machine is provided with a plurality of, configured to control the cycle pitch of the propeller in the rotoruk 2 to regulate the flight posture of the drone.
[0063] Setting of single rotorial drones is a conventional setting in the art, and the present embodiment does not limit the specific structure of single cycloneless actuators and described.
[0064] The gravity leveling method provided in this ...
Embodiment 3
[0066] This embodiment provides an engineer, and is similar to that of the first and examples of the second embodiment, the setting of the center of gravity is only different, and other settings of the drone may refer to the first embodiment or implementation. Example 2 is set, the present embodiment will not be described again.
[0067] The center of gravity trimming device 1 provided in this embodiment includes: a vertically connected first rail 11 and a second rail 12, the first rail 11 can rotate about the centerline of the longitudinal direction, and the second rail 12 can be along the first track 11. The length direction slides, slides on the second track 12, and the weight block 13 can slide in the longitudinal direction of the second track 12.
[0068] In this embodiment, the center of gravity is capable of sliding by the weight block 13 on the second track 12, the sliding action of the second track 12 on the first track 11 can be made The weight of the weight is operated ...
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