Bionic aircraft and control method
A technology of bionic aircraft and sensors, applied in the field of aircraft, to achieve miniaturization, improve maneuverability, and overcome the effect of flying noise
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Embodiment 1
[0057] A bionic aircraft 2, comprising
[0058] A plurality of conductive filaments 21; the conductive filaments 21 are conductive fibers with a diameter of 0.5 μm.
[0059] The electric field sensor 22 is used to obtain the distribution and intensity of the charge 1 of the atmosphere and / or clouds;
[0060] The retractable device 23 is used for retracting and retracting the conductive wire 21; the retractable device 23 includes a motor 231 and a housing box 232, the housing box 232 is provided with a rotating shaft, and the motor 231 drives the rotating shaft to rotate, and the housing box 232 is provided with an opening, and one end of the conductive wire 21 passes through the opening and is connected to the rotating shaft.
[0061] The charging device 24 controls the charge 1 amount of the conductive thread 21 through the distribution and intensity of the charges 1 in the atmosphere and / or clouds; the charging device 24 is a piezoelectric crystal.
[0062] Power supply 25...
Embodiment 2
[0066] A bionic aircraft 2, comprising
[0067] A plurality of conductive filaments 21; the conductive filaments 21 are conductive fibers with a diameter of 10.0 μm.
[0068] The electric field sensor 22 is used to obtain the distribution and intensity of the charge 1 of the atmosphere and / or clouds;
[0069] The retractable device 23 is used for retracting and retracting the conductive wire 21; the retractable device 23 includes a motor 231 and a housing box 232, the housing box 232 is provided with a rotating shaft, and the motor 231 drives the rotating shaft to rotate, and the housing box 232 is provided with an opening, and one end of the conductive wire 21 passes through the opening and is connected to the rotating shaft.
[0070] The charging device 24 controls the charge 1 amount of the conductive thread 21 through the distribution and intensity of the charges 1 in the atmosphere and / or clouds; the charging device 24 is a piezoelectric crystal.
[0071] Power supply 2...
Embodiment 3
[0075] A bionic aircraft 2, comprising
[0076] A plurality of conductive filaments 21; the conductive filaments 21 are conductive fibers with a diameter of 5.0 μm.
[0077] The electric field sensor 22 is used to obtain the distribution and intensity of the charge 1 of the atmosphere and / or clouds;
[0078] The retractable device 23 is used for retracting and retracting the conductive wire 21; the retractable device 23 includes a motor 231 and a housing box 232, the housing box 232 is provided with a rotating shaft, and the motor 231 drives the rotating shaft to rotate, and the housing box 232 is provided with an opening, and one end of the conductive wire 21 passes through the opening and is connected to the rotating shaft.
[0079] The charging device 24 controls the charge 1 amount of the conductive thread 21 through the distribution and intensity of the charges 1 in the atmosphere and / or clouds; the charging device 24 is a piezoelectric crystal.
[0080] Power supply 25...
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