CN112027079A - Bionic aircraft and control method - Google Patents
Bionic aircraft and control method Download PDFInfo
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- CN112027079A CN112027079A CN202010944748.2A CN202010944748A CN112027079A CN 112027079 A CN112027079 A CN 112027079A CN 202010944748 A CN202010944748 A CN 202010944748A CN 112027079 A CN112027079 A CN 112027079A
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- conductive wire
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R29/00—Arrangements for measuring or indicating electric quantities not covered by groups G01R19/00 - G01R27/00
- G01R29/12—Measuring electrostatic fields or voltage-potential
- G01R29/14—Measuring field distribution
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- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention relates to the technical field of aircrafts, in particular to a bionic aircraft and a control method, comprising a conductive wire; the electric field inductor is used for acquiring the charge distribution and intensity of the atmosphere and/or cloud layer; the winding and unwinding device is used for winding and unwinding the conductive wire; the charging device controls the charge quantity of the conductive wire through the charge distribution and the intensity of the atmosphere and/or the cloud layer; the power supply supplies power to the electric field inductor, the winding and unwinding device and the power supply device; the electric field inductor is used for acquiring the charge distribution and the intensity of the atmosphere and/or cloud layer, and the electric field inductor is combined with the charging device to control the charge amount of the conductive wire, so that the conductive wire and the atmosphere and/or cloud layer can fly under the action of the electric field interaction; through the bionic design, a brand-new flight mode is realized, and the design is from endless to endless; the bionic aircraft overcomes the problem that the flight noise of the traditional aircraft is large.
Description
Technical Field
The invention relates to the technical field of aircrafts, in particular to a bionic aircraft and a control method.
Background
In the modern biology, a spider is recorded, which utilizes atmospheric charges (positive charges) to match with own spider silks to be charged (negative charges), spits out the spider silks without being disconnected with a spider body, and drives the spider to fly through the interaction of the spider silks and the atmospheric charges; researchers have exposed spiders to laboratory controlled electronic fields that are quantitatively equivalent to the electronic fields in the atmosphere. They noted that turning the electric field on and off caused the spiders to move up (up) or down (down), demonstrating that the spiders can airborne without wind when subjected to the electric field.
Through retrieval, no bionic aircraft taking the spider as a prototype exists in the prior art.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: a bionic aircraft using a spider as a prototype in the background technology and a control method are provided.
In order to solve the technical problems, the invention adopts a technical scheme that:
the invention has the beneficial effects that: a bionic aircraft comprises
A conductive filament;
the electric field inductor is used for acquiring the charge distribution and intensity of the atmosphere and/or cloud layer;
the winding and unwinding device is used for winding and unwinding the conductive wire;
the charging device controls the charge quantity of the conductive wire through the charge distribution and the intensity of the atmosphere and/or the cloud layer; and
and the power supply supplies power for the electric field inductor, the winding and unwinding device and the power supply device.
In order to solve the technical problem, the invention adopts another technical scheme as follows:
the control method of the bionic aircraft comprises
Setting a destination;
acquiring the charge distribution and intensity of atmosphere and/or cloud layer through an electric field inductor to obtain an optimal flight route flying to a destination, and controlling a winding and unwinding device to release a conductive wire;
the electric charge quantity of the conductive wire is controlled by the electrification device in combination with the charge distribution and the strength of the atmosphere and/or cloud layer to fly in an optimal flying route.
The invention has the beneficial effects that: the electric field inductor is used for acquiring the charge distribution and strength of the atmosphere and/or cloud layer, and the electric field inductor is combined with the energizing device to control the charge quantity of the conductive wire, so that the electric field interaction between the conductive wire and the atmosphere and/or cloud layer can drive the bionic aircraft to lift, turn and advance and retreat; because the atmospheric electric field is not uniform, the non-uniform electric field can be used for steering; through the bionic design, a brand-new flight mode is realized, and the design is from endless to endless; the bionic aircraft overcomes the problem of high flying noise of the traditional aircraft, can realize miniaturization and improves concealment; the utility model can be used as a scout plane through the camouflage of the appearance, and is difficult to be perceived by naked eyes; the conductive wires can be dispersed in a fan-shaped mode due to the fact that the conductive wires are charged in the same type, and mobility can be further improved under the action of air flow in flight. .
Drawings
FIG. 1 is a top view of a bionic aircraft according to an embodiment of the present invention;
FIG. 2 is a side view of a bionic aircraft according to an embodiment of the invention;
FIG. 3 is a schematic structural diagram of a bionic aircraft according to an embodiment of the present invention;
description of reference numerals: 1. charge (positive charge, negative charge); 2. a bionic aircraft; 21. a conductive filament; 22. an electric field inductor; 23. a retracting device; 231. a motor; 232. accommodating the box; 24. a charging device; 25. a power source; 26. a housing; 27. a thermoelectric generation film; 28. and a positioning device.
Detailed Description
In order to explain technical contents, achieved objects, and effects of the present invention in detail, the following description is made with reference to the accompanying drawings in combination with the embodiments.
Referring to fig. 1 to 3, the conductive filament 21 in fig. 1 and 2 has a negative charge 1;
a bionic aircraft 2 comprises
A conductive filament 21;
an electric field inductor 22 for acquiring the distribution and intensity of the electric charge 1 of the atmosphere and/or cloud layer;
the winding and unwinding device 23 is used for winding and unwinding the conductive wire 21;
an energizing device 24 for controlling the charge 1 amount of the conductive yarn 21 by the charge 1 distribution and intensity of the atmosphere and/or cloud layer; and
and the power supply 25 is used for supplying power to the electric field inductor 22, the winding and unwinding device 23 and the power supply device 24.
From the above description, the beneficial effects of the present invention are: the electric field inductor 22 is used for acquiring the distribution and the strength of the electric charges 1 of the atmosphere and/or cloud layer, and the electric field inductor 24 is used for controlling the amount of the electric charges 1 of the conductive wire 21, so that the electric field interaction between the conductive wire 21 and the atmosphere and/or cloud layer can drive the bionic aircraft 2 to lift, turn and advance and retreat; because the atmospheric electric field is not uniform, the non-uniform electric field can be used for steering; through the bionic design, a brand-new flight mode is realized, and the design is from endless to endless; the bionic aircraft 2 solves the problem of high flying noise of the traditional aircraft, can realize miniaturization and improves concealment; the utility model can be used as a scout plane through the camouflage of the appearance, and is difficult to be perceived by naked eyes; the conductive filaments 21 can be spread out in a fan-shaped manner due to the same electric charges 1, and the mobility can be further improved by the action of the air flow in flight.
As can be seen from the above description, the operation process of the bionic aircraft 2 includes:
the rising process: the rising can be realized by acquiring opposite charges 1 on the atmosphere and/or the cloud layer, and when the cloud layer and the atmosphere have different charges 1, the rising is realized by selecting a local electric field with stronger action (the number of the charges 1 is more) to perform interaction with the conductive wire 21;
and (3) a descending process: when the conductive wire is in the air, the electric charge 1 on the conductive wire 21 is eliminated, reduced and the property of the electric charge 1 is adjusted to realize the reduction;
turning: after the direction is selected, 1, acquiring the electric field of the atmosphere and/or cloud layer of the target area, and changing the quantity 1 of the charges and the property 1 of the charges of the conductive wire 21 to realize steering; 2. the center of gravity can be changed by winding and unwinding the conductive wire 21, so that the steering is realized; 3. the electrification amount of different conductive wires 21 can be controlled, so that the conductive wires 21 interact with each other to deviate from other conductive wires 21, the center of gravity is shifted, and the steering is realized; for example, in the flying process, a left turn is needed, a cloud layer is arranged in front of the left side, the electric field intensity of the cloud layer is obtained, the electric charge 1 of the conductive wire 21 is adjusted, and the interaction with the cloud layer electric field is preferentially selected to realize steering;
advancing and retreating processes: as with steering, can fly in an oblique up/down direction; under the condition that a plurality of conductive wires 21 are arranged, one conductive wire can selectively provide an electric field in the vertical direction, and the other conductive wire can provide an electric field in the horizontal direction, so that horizontal flight is realized;
hovering: and controlling the electric field intensity of the conductive wire 21 generated by the atmosphere and/or cloud layer to be offset with the acting force generated by the gravity of the bionic aircraft 2.
Further, the bionic aircraft further comprises a shell 26, the winding and unwinding device 23, the power supply device 24 and the power supply 25 are arranged in the shell 26, a wire outlet is formed in the shell 26, and the conductive wires 21 extend out of the bionic aircraft 2 through the wire outlet;
the energizing device 24 controls the amount of charge 1 of the housing 26.
As can be seen from the above description, the electrification of the bionic aircraft 2 can be enhanced by controlling the amount of the electric charge 1 of the housing 26 through the electrification device 24, so as to improve the maneuverability of the bionic aircraft 2.
Further, the housing 26 is streamlined, and the sectional length of the upper surface of the housing 26 is longer than the sectional length of the lower surface of the housing 26.
As can be seen from the above description, by streamlining the housing 26, the drag of flight can be reduced; by making the sectional length of the upper surface of the housing 26 longer than the sectional length of the lower surface of the housing 26, the bionic aircraft 2 can be caused to provide lift by airflow in flight by the bernoulli principle.
Further, the outer surface of the shell 26 is black, a thermoelectric generation film 27 is arranged on the outer surface of the shell 26, and the thermoelectric generation film 27 is electrically connected with the power supply 25; the lower surface of the power supply 25 is attached to the bottom of the inner wall of the shell 26, and a heat insulation layer is arranged on the other outer surface of the power supply 25.
As can be seen from the above description, the outer surface of the shell 26 is black, so that the bionic aircraft 2 can absorb heat conveniently, and the temperature inside the shell 26 is increased, because the temperature of the atmosphere is low, and the temperature is lower as the altitude is higher, the heat can be taken away during flying in the air, and because the working device is arranged inside the shell, the heat is inevitably generated, so that the temperature inside the aircraft is high, and the temperature outside the aircraft is low; through the arrangement of the thermoelectric generation film 27, the internal heat is converted into electric energy for continuous use according to the Seebeck effect principle; the lower surface of the power supply 25 is attached to the bottom of the inner wall of the shell 26, so that the battery can be conveniently cooled, and the other outer surfaces of the power supply 25 are provided with heat insulation layers, so that the battery can be prevented from being heated by the heat inside.
Furthermore, the conductive wire 21 has a plurality of conductive fibers, and the conductive fibers 21 have a diameter of 0.5 to 10.0 μm.
As can be seen from the above description, the plurality of conductive wires 21 can give the same electric charge 1 to the electric charging device 24 during flight, and since the electric charges 1 are the same, the conductive wires 21 form a fan-shaped structure due to the effect of the electric charge 1, and are convenient to store when not charged; meanwhile, the fan-shaped conductive wires 21 (with increased surface area) can facilitate the airflow to act on the fan-shaped conductive wires, and can quickly fly upwards when encountering ascending airflow; when the aircraft needs to turn, the center of gravity is changed by retracting one conducting wire 21, and then the direction is changed.
Further, the retraction device 23 comprises a motor 231 and an accommodating box 232, a rotating shaft is arranged in the accommodating box 232, the motor 231 drives the rotating shaft to rotate, an opening is formed in the accommodating box 232, and one end of the conductive wire 21 penetrates through the opening to be connected to the rotating shaft.
Further, the energizing device 24 is a piezoelectric crystal.
As is apparent from the above description, the property of the charge 1 and the amount of the charge 1 of the conductive wire 21 can be controlled by the arrangement of the piezoelectric crystal.
Further, the positioning device 28 is further included, and the positioning device 28 is one or more of GPS positioning and beidou positioning.
The control method of the bionic aircraft 2 comprises
Setting a destination;
acquiring the distribution and the intensity of the electric charge 1 of the atmosphere and/or cloud layer through the electric field inductor 22 to obtain an optimal flight route flying to a destination, and controlling the winding and unwinding device 23 to release the conductive wire 21;
the electric charge 1 quantity of the conductive thread 21 is controlled by the electrification device 24 in combination with the electric charge 1 distribution and intensity of the atmosphere and/or cloud layer to fly in an optimal flying route.
Further, the bionic aircraft 2 acquires real-time data of the distribution and intensity of the electric charges 1 in the surrounding atmosphere and/or cloud layer through the electric field inductor 22 during the flight to correct the optimal flight path in real time;
and controlling the power supply device 24 and/or the winding and unwinding device 23 to control the conductive wire 21 according to the real-time correction result.
Example one
A bionic aircraft 2 comprises
A plurality of conductive filaments 21; the conductive filaments 21 are conductive fibers having a diameter of 0.5 μm.
An electric field inductor 22 for acquiring the distribution and intensity of the electric charge 1 of the atmosphere and/or cloud layer;
the winding and unwinding device 23 is used for winding and unwinding the conductive wire 21; the winding and unwinding device 23 comprises a motor 231 and an accommodating box 232, a rotating shaft is arranged in the accommodating box 232, the motor 231 drives the rotating shaft to rotate, an opening is formed in the accommodating box 232, and one end of the conductive wire 21 penetrates through the opening to be connected to the rotating shaft.
An energizing device 24 for controlling the charge 1 amount of the conductive yarn 21 by the charge 1 distribution and intensity of the atmosphere and/or cloud layer; the energizing device 24 is a piezoelectric crystal.
The power supply 25 supplies power to the electric field inductor 22, the winding and unwinding device 23 and the power supply device 24;
the winding and unwinding device 23, the power supply device 24 and the power supply 25 are arranged in the shell 26, a wire outlet is formed in the shell 26, and the conductive wire 21 extends out of the bionic aircraft 2 through the wire outlet; the energizing device 24 controls the amount of charge 1 of the housing 26. The housing 26 is streamlined, and the sectional length of the upper surface of the housing 26 is longer than that of the lower surface of the housing 26. The outer surface of the shell 26 is black, a thermoelectric generation film 27 is arranged on the outer surface of the shell 26, and the thermoelectric generation film 27 is electrically connected with the power supply 25; the lower surface of the power supply 25 is attached to the bottom of the inner wall of the shell 26, and a heat insulation layer is arranged on the other outer surface of the power supply 25. And
Example two
A bionic aircraft 2 comprises
A plurality of conductive filaments 21; the conductive filaments 21 are conductive fibers having a diameter of 10.0 μm.
An electric field inductor 22 for acquiring the distribution and intensity of the electric charge 1 of the atmosphere and/or cloud layer;
the winding and unwinding device 23 is used for winding and unwinding the conductive wire 21; the winding and unwinding device 23 comprises a motor 231 and an accommodating box 232, a rotating shaft is arranged in the accommodating box 232, the motor 231 drives the rotating shaft to rotate, an opening is formed in the accommodating box 232, and one end of the conductive wire 21 penetrates through the opening to be connected to the rotating shaft.
An energizing device 24 for controlling the charge 1 amount of the conductive yarn 21 by the charge 1 distribution and intensity of the atmosphere and/or cloud layer; the energizing device 24 is a piezoelectric crystal.
The power supply 25 supplies power to the electric field inductor 22, the winding and unwinding device 23 and the power supply device 24;
the winding and unwinding device 23, the power supply device 24 and the power supply 25 are arranged in the shell 26, a wire outlet is formed in the shell 26, and the conductive wire 21 extends out of the bionic aircraft 2 through the wire outlet; the energizing device 24 controls the amount of charge 1 of the housing 26. The housing 26 is streamlined, and the sectional length of the upper surface of the housing 26 is longer than that of the lower surface of the housing 26. And
a positioning device 28, the positioning device 28 being a GPS positioning.
EXAMPLE III
A bionic aircraft 2 comprises
A plurality of conductive filaments 21; the conductive filaments 21 are conductive fibers having a diameter of 5.0 μm.
An electric field inductor 22 for acquiring the distribution and intensity of the electric charge 1 of the atmosphere and/or cloud layer;
the winding and unwinding device 23 is used for winding and unwinding the conductive wire 21; the winding and unwinding device 23 comprises a motor 231 and an accommodating box 232, a rotating shaft is arranged in the accommodating box 232, the motor 231 drives the rotating shaft to rotate, an opening is formed in the accommodating box 232, and one end of the conductive wire 21 penetrates through the opening to be connected to the rotating shaft.
An energizing device 24 for controlling the charge 1 amount of the conductive yarn 21 by the charge 1 distribution and intensity of the atmosphere and/or cloud layer; the energizing device 24 is a piezoelectric crystal.
The power supply 25 supplies power to the electric field inductor 22, the winding and unwinding device 23 and the power supply device 24;
the winding and unwinding device 23, the power supply device 24 and the power supply 25 are arranged in the shell 26, a wire outlet is formed in the shell 26, and the conductive wire 21 extends out of the bionic aircraft 2 through the wire outlet; the energizing device 24 controls the amount of charge 1 of the housing 26. The housing 26 is streamlined. And
the positioning device 28, the positioning device 28 is a dual mode of GPS positioning and beidou positioning.
Example four
The control method of the bionic aircraft 2 comprises the following steps
Setting a destination;
acquiring the distribution and the intensity of the electric charge 1 of the atmosphere and/or cloud layer through the electric field inductor 22 to obtain an optimal flight route flying to a destination, and controlling the winding and unwinding device 23 to release the conductive wire 21;
controlling the charge 1 amount of the conductive wire 21 by combining the charge 1 distribution and the intensity of the atmosphere and/or cloud layer through the electrification device 24 to fly in an optimal flying route;
the bionic aircraft 2 acquires real-time data of the distribution and intensity of the charges 1 in the surrounding atmosphere and/or cloud layer through the electric field inductor 22 during the flight process to correct the optimal flight path in real time;
and controlling the power supply device 24 and/or the winding and unwinding device 23 to control the conductive wire 21 according to the real-time correction result.
The above description is only an embodiment of the present invention, and not intended to limit the scope of the present invention, and all equivalent changes made by using the contents of the present specification and the drawings, or applied directly or indirectly to the related technical fields, are included in the scope of the present invention.
Claims (10)
1. A bionic aircraft is characterized by comprising
A conductive filament;
the electric field inductor is used for acquiring the charge distribution and intensity of the atmosphere and/or cloud layer;
the winding and unwinding device is used for winding and unwinding the conductive wire;
the charging device controls the charge quantity of the conductive wire through the charge distribution and the intensity of the atmosphere and/or the cloud layer; and
and the power supply supplies power for the electric field inductor, the winding and unwinding device and the power supply device.
2. The bionic aircraft according to claim 1, further comprising a shell, wherein the winding and unwinding device, the power supply device and the power supply are arranged in the shell, a wire outlet is formed in the shell, and the conductive wire extends out of the bionic aircraft through the wire outlet;
the power-applying device controls the amount of electric charge of the case.
3. The biomimetic aircraft of claim 2, wherein the housing is streamlined, and a cross-sectional length of an upper surface of the housing is longer than a cross-sectional length of a lower surface of the housing.
4. The bionic aircraft according to claim 2, wherein the outer surface of the shell is black, and a thermoelectric generation film is arranged on the outer surface of the shell and is electrically connected with a power supply; the lower surface of the power supply is attached to the bottom of the inner wall of the shell, and heat insulation layers are arranged on the other outer surfaces of the power supply.
5. The bionic aircraft according to claim 1, wherein the conductive wires are a plurality of conductive fibers with diameters of 0.5-10.0 μm.
6. The bionic aircraft according to claim 1, wherein the retraction device comprises a motor and a containing box, a rotating shaft is arranged in the containing box, the motor drives the rotating shaft to rotate, an opening is arranged on the containing box, and one end of the conductive wire penetrates through the opening and is connected to the rotating shaft.
7. The biomimetic aerial vehicle of claim 1, wherein the energizing device is a piezoelectric crystal.
8. The biomimetic aircraft of claim 1, further comprising a positioning device, the positioning device being one or more of a GPS location and a beidou location.
9. A control method of the bionic aircraft according to any one of claims 1-8, characterized by comprising
Setting a destination;
acquiring the charge distribution and intensity of atmosphere and/or cloud layer through an electric field inductor to obtain an optimal flight route flying to a destination, and controlling a winding and unwinding device to release a conductive wire;
the electric charge quantity of the conductive wire is controlled by the electrification device in combination with the charge distribution and the strength of the atmosphere and/or cloud layer to fly in an optimal flying route.
10. The control method of the bionic aircraft according to claim 9, wherein the bionic aircraft obtains real-time data of charge distribution and intensity of surrounding atmosphere and/or cloud layer through an electric field sensor during flight to modify the optimal flight path in real time;
and controlling the power supply device and/or the winding and unwinding device to control the conductive wire according to the real-time correction result.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN202010944748.2A CN112027079A (en) | 2020-09-10 | 2020-09-10 | Bionic aircraft and control method |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010944748.2A CN112027079A (en) | 2020-09-10 | 2020-09-10 | Bionic aircraft and control method |
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| CN112027079A true CN112027079A (en) | 2020-12-04 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113619786A (en) * | 2021-08-26 | 2021-11-09 | 西安交通大学 | Miniature aircraft drive arrangement and unmanned aerial vehicle based on electrostatic force |
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| GB1061733A (en) * | 1963-02-15 | 1967-03-15 | Hans Werner Von Engel | A flying body |
| DE1581114A1 (en) * | 1962-12-27 | 1970-01-22 | Von Engel Hans Werner | Aircraft with electrostatic propulsion |
| US20070176050A1 (en) * | 2003-10-30 | 2007-08-02 | Dressler Gordon A | System and Method for an Ambient Atmosphere Ion Thruster |
| CN101395060A (en) * | 2006-03-02 | 2009-03-25 | 佩卡·扬胡宁 | Electric sail for producing spacecraft propulsion |
| US20100243816A1 (en) * | 2003-05-06 | 2010-09-30 | Gary Richard Gochnour | Aircraft also called a spacecraft, an aerospace craft, or a submersible craft |
| US20180281993A1 (en) * | 2017-03-31 | 2018-10-04 | Trustees Of Boston University | Propulsion and gas-moving systems using travelling-wave gas dielectrophoresis |
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2020
- 2020-09-10 CN CN202010944748.2A patent/CN112027079A/en not_active Withdrawn
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1581114A1 (en) * | 1962-12-27 | 1970-01-22 | Von Engel Hans Werner | Aircraft with electrostatic propulsion |
| GB1061733A (en) * | 1963-02-15 | 1967-03-15 | Hans Werner Von Engel | A flying body |
| US20100243816A1 (en) * | 2003-05-06 | 2010-09-30 | Gary Richard Gochnour | Aircraft also called a spacecraft, an aerospace craft, or a submersible craft |
| US20070176050A1 (en) * | 2003-10-30 | 2007-08-02 | Dressler Gordon A | System and Method for an Ambient Atmosphere Ion Thruster |
| CN101395060A (en) * | 2006-03-02 | 2009-03-25 | 佩卡·扬胡宁 | Electric sail for producing spacecraft propulsion |
| US20180281993A1 (en) * | 2017-03-31 | 2018-10-04 | Trustees Of Boston University | Propulsion and gas-moving systems using travelling-wave gas dielectrophoresis |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113619786A (en) * | 2021-08-26 | 2021-11-09 | 西安交通大学 | Miniature aircraft drive arrangement and unmanned aerial vehicle based on electrostatic force |
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