Vertical takeoff power supply system, fixed wing unmanned aerial vehicle and working method
A vertical take-off and power supply system technology, applied to aircraft parts, unmanned aircraft, aircraft, etc., can solve the problems of power consumption, large power consumption, and affecting the cruising mileage and time of drones, so as to reduce power consumption, The effect of meeting the power demand and prolonging the cruising mileage and time
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Embodiment 1
[0030] like figure 1 As shown, the present embodiment 1 provides a vertical take-off power supply system, including: a power supply device 1 located on the ground; the power supply device 1 is suitable for maintaining power supply to the UAV 2 when the UAV 2 takes off vertically ; and when the UAV 2 reaches a predetermined height, the UAV 2 is separated from the power supply device 1 for power supply.
[0031] As an optional implementation of the vertical take-off power supply system, the vertical take-off power supply system also includes: an adsorption device and a charging terminal; the adsorption device is suitable for inserting the plug 102 of the charging terminal into the charging interface of the drone, and After the drone reaches a predetermined height, the adsorption device drives the charging end to fall off, so that the drone is detached from the power supply device for power supply;
[0032] Specifically, the power supply device includes: a main processor module,...
Embodiment 2
[0042] On the basis of Embodiment 1, this Embodiment 2 also provides a working method of the vertical take-off power supply system, that is, when the UAV takes off vertically, the power supply device is suitable for maintaining power supply to the UAV; and when there is no After the man-machine reaches the predetermined height, the UAV is powered off from the power supply device.
[0043] The vertical take-off power supply system also includes: an adsorption device and a charging terminal; the adsorption device is suitable for inserting the plug of the charging terminal into the charging interface of the drone, and when the drone reaches a predetermined height, the adsorption device drives the charging terminal to fall off; The man-machine is powered from the power supply device; the power supply device is provided with a wire wheel for coiling the transmission wire.
[0044] The power supply device includes: a main processor module, a main power line carrier module connected ...
Embodiment 3
[0046] On the basis of Embodiment 1, Embodiment 2 also provides an unmanned aerial vehicle.
[0047] The unmanned aerial vehicle includes: an onboard processor module, an unmanned aerial vehicle power system controlled by the onboard processor module, and the vertical take-off power supply system; The power supply system inside the man-machine is powered.
[0048] The power supply system in the drone includes: a charging and discharging control module and a lithium battery.
[0049] The power system of the UAV includes: a horizontal power subsystem 3 and a vertical power subsystem 4 controlled by an onboard processor module; wherein the horizontal power subsystem 3 is located at the fuselage and includes: a horizontal propeller mechanism; The vertical power subsystem 4 includes: a vertical propeller 401 mechanism symmetrically arranged at the left and right wings 5 places; The GPS module for man-machine positioning is connected.
[0050] The vertical propeller 401 mechani...
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Abstract
Description
Claims
Application Information
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