Unmanned aerial vehicle
A technology of drones and airframes, applied in the field of aircraft, can solve problems such as high cost and poor noise reduction effect, and achieve the effect of cost saving
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Embodiment 1
[0015] figure 1 It is a schematic structural diagram of a UAV provided in Embodiment 1 of the present invention. The UAV in this embodiment may be a multi-rotor UAV, such as a quad-rotor UAV, an octo-rotor UAV, and the like. refer to figure 1 , taking the quadrotor drone as an example, the drone provided in this embodiment specifically includes: a fuselage 1, the fuselage 1 is provided with at least one connecting arm 2 extending outward, each of the connecting arms 2 A housing 3 is provided on one end of the outer extension, and a first motor 4 , a noise collecting device 5 and an acoustic wave output device 6 are integrated in the housing 3 , and a first rotor connected to the first motor 4 is provided on the upper part of the housing 3 7. A control module 8 is integrated in the fuselage 1; the noise collection device 5 is used to collect the noise generated during the flight of the drone and send it to the control module 8; the control module 8 is used to control the The ...
Embodiment 2
[0026] figure 2 A schematic structural diagram of an unmanned aerial vehicle provided in Embodiment 2 of the present invention, specifically a structural schematic diagram at the housing 3. In this embodiment, on the basis of the above-mentioned embodiments, it is preferred that the housing 3 is also provided with a second The motor 9 is arranged below the first motor 4 , and the second rotor 10 connected to the second motor 9 is arranged on the lower part of the casing 3 .
[0027] Wherein, the bottom of casing 3 is provided with output hole, and the bottom of second motor 9 is provided with output shaft, and output shaft passes through the output hole of casing 3 bottom and is connected with second rotor 10, drives output shaft when second motor 9 works Rotate, and then drive the second rotor 10 to rotate.
[0028] Preferably, the noise collecting device 5 and the acoustic wave output device 6 in each of the housings 3 are arranged on the inner wall of the housing 3, and a...
Embodiment 3
[0034] In this embodiment, on the basis of Embodiment 1, it is preferable to further increase the control module 8 to be further used to control any pair of drones located on the diagonal when the UAV receives the control command of vertical ascent / vertical descent. Two first motors 4 are in working state, and other first motors 4 are turned off.
[0035] Among them, when the UAV is vertically ascending or descending, the rotor only needs to provide the buoyancy in the vertical direction, and does not need to provide the horizontal component. The two first motors 4 on the top are in working condition, while the other first motors 4 are turned off.
[0036] On the basis of the above technical solution, preferably, the control of any pair of two first motors 4 located on the diagonal to be in the working state specifically includes: controlling any pair of the two first motors 4 located on the diagonal 4 are started sequentially with a preset time difference, so that the noises...
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