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

Inactive Publication Date: 2020-12-04
福州市长乐区白英设计有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Through retrieval, there is no bionic aircraft based on this spider as a prototype in the prior art

Method used

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  • Bionic aircraft and control method
  • Bionic aircraft and control method

Examples

Experimental program
Comparison scheme
Effect test

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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PUM

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Abstract

The invention relates to the technical field of aircrafts, in particular to a bionic aircraft and a control method. The bionic aircraft comprises conductive wires, an electric field sensor used for acquiring charge distribution and intensity of the atmosphere and/or the cloud layer; a winding and unwinding device used for winding and unwinding the conductive wires; an energizing device which is used for controlling the charge quantity of the conductive wires through the charge distribution and intensity of the atmosphere and/or the cloud layer; and a power supply which is used for supplying power to the electric field sensor, the winding and unwinding device and the energizing device. The charge distribution and intensity of the atmosphere and/or the cloud layer are obtained through the electric field sensor, and the charge quantity of the conductive wires is controlled by combining the energizing device, so that the conductive wire and the electric field between the atmosphere and/orthe cloud layer interact to drive the aircraft to fly; through the bionic design, a brand-new flight mode is realized, and the design is changed from nothing to nothing; and the bionic aircraft solvesthe problem that a traditional aircraft is large in flight noise.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a bionic aircraft and a control method. Background technique [0002] In "Contemporary Biology" there is a record of a spider that utilizes the atmospheric charge (positive charge) and its own spider silk to be charged (negative charge) to spit out the spider silk and connect it with the spider body without interruption. The interaction of atmospheric charges drives the spiders to flight; the researchers exposed the spiders to laboratory-controlled electronic fields that were quantitatively equivalent to those in the atmosphere. They noticed that turning the electric field on and off caused the spiders to move up (up) or down (down), demonstrating that spiders can be airborne in the absence of wind when subjected to an electric field. [0003] By retrieval, in the prior art, there is no biomimetic aircraft that takes this kind of spider as a prototype. Contents of the inventi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/00B64C19/00G01R29/14
CPCB64C19/00B64C39/00G01R29/14
Inventor 林俊林剑白林涛
Owner 福州市长乐区白英设计有限公司
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