KR101128958B1 - Flying object - Google Patents

Abstract

The present invention relates to a vehicle.

The present invention, in the aircraft to obtain a driving force through the wing movement, alternately providing the attraction and repulsion through the change of the electromagnetic force on the surface of the left / right wings provided on both sides of the main body to generate mutually independent wing movement on the left / right wings It is characterized by obtaining a driving force.

The present invention can improve the flight efficiency by minimizing the total weight of the aircraft by simplifying and lightening the drive structure. In addition, the present invention can improve the propulsion by placing the drive structure on the wing to reduce the weight of the body and increase the weight acceleration in the wing movement. In addition, the present invention can improve the reversibility by enabling the vertical rise / fall, take off / landing, forward, turning, as well as backward.

Description

Aircraft {FLYING OBJECT}

The present invention relates to a vehicle, and more particularly to a vehicle having improved vertical rise, stationary flight, flight efficiency, propulsion and direction change.

In general, the aircraft may be an aeroplane, a flying saucer, an airship, a helicopter, or the like.

In the case of the plane is attached to the wings for generating a lift on both sides of the streamlined body, the tail portion of the body is attached to the tail wings for adjusting the direction.

At this time, the auxiliary wing is installed to adjust the angle within a predetermined range for the purpose of inducing takeoff / landing by adjusting the size of the lift on the rear of the wing generating the lift, the angle of the auxiliary wing using a motor, etc. Adjust

In such an airplane, the wing is simply a means for generating lift, and a propulsion device for a separate propulsion is required. Therefore, there is a problem that the structure is very complicated and heavy weight.

Recently, in order to solve this problem, a dragonfly-type aircraft that obtains propulsion through wing motion has been introduced. The dragonfly-type vehicle is a drive structure for transmitting the crank, the link and the tip of the link to the two wings woven by the "X" to the wing structure of the drive provided to the left and right symmetrical wing movement.

In the related art, a dragonfly-type aircraft having wing movements has a pair of left and right cranks and links converted into linear movements, respectively, and the link is connected to a wing connected by an "X" around an intermediate axis. Since the wing movement is made, there is a problem that the weight is heavy, and due to this, there is a problem that the flight distance is greatly shortened due to the lack of thrust.

In addition, conventionally, the dragonfly-type aircraft that performs the wing movement is not possible to turn only by the wing movement, so as to provide a separate rotor (ROTOR) in the tail portion, such as a helicopter, there is a complex structure problem.

In addition, the conventional dragonfly-type aircraft that performs the wing movement has a problem in turning direction that can not be turned backwards to turn like a conventional airplane when changing direction.

The present invention, in the aircraft to obtain a driving force through the wing movement, alternately providing the attraction and repulsion through the change of the electromagnetic force on the surface of the left / right wings provided on both sides of the main body to generate mutually independent wing movement on the left / right wings It is characterized by obtaining a driving force.

The present invention can improve the flight efficiency by minimizing the total weight of the vehicle by simplifying and lightening the drive structure.

In addition, the present invention can improve the propulsion by placing the drive structure on the wing to reduce the weight of the body and increase the weight acceleration in the wing movement.

In addition, the present invention can improve the reversibility by enabling the vertical rise / fall, take off / landing, forward, turning, as well as backward.

In addition, the present invention can change the speed of the blade movement in frequency can be easily adjusted freely.

In addition, the present invention can control the operation by manual operation, but according to the actual flight environment, that is, the program to adjust the resonant frequency to automatically find the resonant point according to the weight of the aircraft and the influence of the wind is stable and automatic You can also fly.

1 is a perspective view showing a configuration according to an embodiment of the present invention, Figure 2 shows a configuration according to an embodiment of the present invention in more detail before explaining the present invention One is a front cross-sectional view, Figure 3 is a partial front cross-sectional view showing the configuration of the left / right wing driving portion of the configuration according to an embodiment of the present invention, Figure 4 is a left / right wing driving portion of the configuration according to an embodiment of the present invention Figure 5 is a partial front cross-sectional view showing another configuration, Figure 5 is a side cross-sectional view of the wing portion showing the angle of the wing of another configuration according to an embodiment of the present invention, Figure 6 shows an embodiment according to the wing control of the present invention 7 is a front sectional view showing an operation according to an embodiment of the present invention, FIG. 8 is a perspective view showing a further configuration according to an embodiment of the present invention, and FIG. 9 according to an embodiment of the present invention. Propulsion blades during further configuration Partial side cross-sectional view showing the part, Figure 10 is a block diagram showing another embodiment according to the wing control of the present invention, Figure 11 shows the action of the propulsion wing portion of a further configuration according to an embodiment of the present invention. 12 is a perspective view showing another configuration according to an embodiment of the present invention, FIG. 13 is a plan view showing another configuration according to an embodiment of the present invention, and FIG. 14 is an embodiment of the present invention. Figure 15 is a side cross-sectional view showing a wing portion of another configuration according to, Figure 15 is a block diagram showing another embodiment according to the wing control of the present invention, Figures 16 and 17 of the other configuration according to an embodiment of the present invention 18 is a plan view showing another configuration according to an embodiment of the present invention, and FIGS. 19 and 20 are wing configuration states of another configuration according to an embodiment of the present invention. Wings FIG. 21 is a plan view showing another configuration according to an embodiment of the present invention, FIG. 22 is a partial cross-sectional view showing another configuration according to an embodiment of the present invention, and FIG. 23 is an embodiment of the present invention. A partial cross-sectional view showing still another configuration according to an example is shown.

The present invention will be described below with reference to the accompanying drawings presented as above.

First, the present invention, as shown in the accompanying drawings, Figures 1 to 3, in the aircraft to obtain a driving force through the wing movement, on the surface of the left and right wings (11, 12) provided on both sides of the main body (1) It is characterized in that the driving force is obtained by alternately providing the attraction force and the repulsive force through the change of the electromagnetic force to generate mutually independent wing movements on the left / right wings 11 and 12.

Here, in the present invention, the left wing 11 and the right wing 12 are main / driven wings having one end fixed to each other at intervals above and below the main body 1 (11a, 11b) 12a and 12b) may be provided symmetrically.

At this time, the main / driven wings (11a, 11b) (12a, 12b) may be hinged on one side to the main body 1, respectively, only the hinge (11a) (12a) hinge (H) coupling It can also be.

As described above, when the main / driven wings ((11a, 11b) (12a, 12b) are all hinged to the main body 1, when the manpower and repulsive action of the left and right wing drives 13, 14 to be described later Wing movement may occur while being attracted or repulsed to each other, thereby preventing fluctuations due to repulsive force in the opposite direction in which wing movement occurs.

On the other hand, as described above, when only the main blade (11a) 12a hinged to the main body 1, the main wing (11a) (12a) with respect to the driven wing (11b) (12b) while the force, the repulsive force acts on the wing You can exercise to increase your momentum. Of course, even if the driven blades 11b and 12b are fixed, a certain amount of vibration (wing movement) occurs, thereby reducing the fluctuation caused by the repulsion as described above.

In addition, the left wing 11a and the driven wing (11b) of the left wing (11) and the main wing (12a) and driven wing (12b) of the right wing 12, the left wing acting mutual attraction / repulsion by the electromagnetic force Left wing drive 13 including drive bodies 1, 2 (13a) and 13b, and right wing drive including right wing drives 1, 2 (14a) and 14b which are also attracted / repulsive by electromagnetic force. 14 may be provided.

The left wing actuators 1, 2 (13a) and 13b and the right wing drives 1, 2 (14a and 14b) are magnetically repulsive in response to the coils according to the direction of the coil and the current flowing through the coils, respectively. It can be configured to include a circuit.

At this time, if the left wing drive 1 (13a) and the right wing drive 1 (14a) is a magnetic circuit, the left wing drive 2 (13b) and the right wing drive 2 (14b) may be a coil, attached As shown in FIG. 4, if the left wing driver 1 (13a) and the right wing driver 1 (14a) are coils, the left wing driver 2 (13b) and the right wing driver 2 (14b) are magnetic circuits. Can be.

At this time, the magnetic circuit may be simply a magnet (satisfactory if the magnetic material), but the yoke protruding from the center; A magnet fixed to an outer side of the protruding surface of the yoke to form a gap with the central protruding portion; It may be configured to include; a top plate seated on the magnet.

As described above, the coil and the magnetic circuit interact with each other to achieve wing movement. That is, when an electric signal is applied to the coil, for example, when an electric current flows, an electromagnetic field is alternately formed according to the flowing direction, and the magnetic circuit vibrates while repulsing and sucking reaction, resulting in vane movement.

At this time, the left / right wings 11 and 12 are basically in a plane state without tilting with respect to the ground (in consideration of lift, but as shown in FIG. 5, the front of the main body (forward direction). The tilt angle may be inclined at about 10 degrees to about 20 degrees.

In this way, when wing motion occurs, forward movement is possible while pushing air backward.

In the above wing movement of the main blades (11a) (12a) may have a greater movement width downward than upward. Then, the force that pushes the air backwards during the wing movement can act to increase the propulsion.

Here, the left and right wing driving units 13 and 14 which move the left and right wings 11 and 12 are made of a direction signal and an acceleration / deceleration signal, which are digital signals for the position movement degree according to the operation of the rudder and the acceleration handle. When the direction signal and the acceleration / deceleration signal are input from the operation signal providing unit 20 and the operation signal providing unit 20 which are converted and provided to each other, the controller 30 converts and outputs a frequency according to the corresponding direction signal and the acceleration / deceleration signal. Can be controlled by

In this case, the operation signal providing unit 20 may be a conventional wire / wireless regulator using a separate high frequency, or may be a wire / wireless regulator (with a cockpit) provided in the main body (1).

In addition, the power signal providing unit 20 and the control unit 30 may be supplied with power through different power supply unit 40, may be supplied with power through one power supply unit 40. have.

In this case, when the acceleration handle of the operation signal providing unit 20 is raised in the acceleration direction, an acceleration signal is provided to the control unit 30, and the control unit 30 raises the frequency according to the input acceleration signal to increase the left / right. Transfer to the right wing drive (13) (14).

Then, the left and right wing drive (13, 14) acts with the attraction force and repulsive force in a state that the amplitude is narrowed by the corresponding frequency (when the amplitude is narrow, the blade movement is made fast, if the amplitude is wide the blade movement is made slow) Left / right wing (11, 12) is to move the blade, at this time, it is possible to control the speed by adjusting the strength of the blade movement by adjusting the level of power provided from the power supply unit 40.

In this way, according to the height of the frequency input to the left / right wing drive (13) 14 is adjusted quickly and slowly the blade movement is possible to take off / landing as well as speed control.

Hereinafter, the attraction force and the repulsive force of the left / right wing drive unit 13 and 14 of the present invention will be described in detail, but the left wing drive unit 1 (13a) and the left / right wing drive unit 13 and 14 are described. The right wing driver 1 (14a) is a magnetic circuit, the left wing driver 2 (13b) and the right wing driver 2 (14b) will be described through the embodiment of the coil, because both drive bodies are the same, it will be described as one Let's do it.

First, the magnets constituting the magnetic circuits of the left wing driver 1 (13a) and the right wing driver 1 (14a) forms a magnetic field in a state in which the N pole is magnetized so that the S pole is located below the N pole. In this state, the direction of the magnetic field is from the N pole to the S pole.

When a current flows clockwise in the coils constituting the left wing driver 2 (13b) and the right wing driver 2 (14b) in the state in which the magnetic field is formed, the magnet moves upwards, and the clock When current flows in the opposite direction, the magnet moves downward, and this state continuously vibrates with frequency.

The vibrations of the left and right wing drives 13 and 14 are transferred to the fixed left and right wings 11 and 12 while they are fully winged to obtain the vertical thrust / descent, propulsion of landing and forwarding. .

One of the important parts of the present invention is that the left wing 11 and the right wing 12 can each independently wing movement.

That is, when the frequency applied to the left and right wing driving units 13 and 14 for driving the left and right wings 11 and 12, respectively, the direction can be switched without a separate rotor such as a helicopter. Can be.

For example, if it wants to rotate to the left during flight, low frequency is not applied to the left wing driver 13 and high frequency is applied to the right wing driver 14.

Then, the left wing drive 13 is a slow wing motion by the action of the attraction and repulsive force acts slowly, the right wing drive 14 generates a quick wing motion by the action of attraction and repulsive action, rotates to the left Do it.

Left / right wing (11, 12) of the present invention as described above, the left / right wing driving portion (13), 14, the part is fixed to the seat is made of a panel, corresponding to the side of the wing in front of the panel It is made of a streamlined frame up to the edge portion, the wing fabric (C) made of thin synthetic resin or woven paper to the frame portion may be made by fixing by ultrasonic welding or bonding.

Then, the panel portion is firmly fixed to the left / right wing driving portion (13) (14), the wing fabric portion to make the wing movement while making the wings lighter, flapping.

In addition, the left / right wings 11, 12 may be made of the panel itself, the outer edge portion of the entire wing is made of a frame, the wing fabric (C) made of a thin synthetic resin or fabric paper therein It can be made fixed by ultrasonic welding or adhesion.

And, according to another embodiment of the present invention, as shown in the accompanying drawings Figures 8 and 9, to further include a propulsion wing 15 for generating a propulsion through the blade movement in the rear of the main body 1 Can also be.

At this time, the propulsion wing 15 may be made of a propulsion main / driven wing (15a, 15b) is fixed at one end of the main body 1 at intervals on the top / bottom.

At this time, the propulsion main / driven wings (15a, 15b) may be hinged to one end of the main body 1, respectively, may be hinged only the main blade (15a).

In addition, the propulsion wing blade (15a) and the propulsion driven wing (15b) is provided with a propulsion wing drive unit (16) including a propulsion wing driving body 1, 2 (16a) (16b) that mutual attraction / repulsive action by the electromagnetic force. Can be.

In this state, as shown in FIG. 10, the propulsion wing driving unit 16 may be controlled through the operation signal providing unit 20 and the control unit 30 described above.

That is, when the acceleration handle of the operation signal providing unit 20 is raised in the acceleration direction, an acceleration signal is provided to the control unit 30, and the control unit 30 increases the frequency according to the input acceleration signal and the propulsion wing driving unit 16. To pass).

Then, as shown in Figure 11, the propulsion wing drive unit 16 is to move the wing blades 15, while the repulsive force acting with the attraction force in the amplitude narrowed by the corresponding frequency, the power supply unit 40 You can also control the speed by adjusting the strength of the wing movement by adjusting the level of power provided by the.

And, according to another embodiment of the present invention, as shown in the accompanying drawings, Figures 12 to 14, a pair of first left wing drive 13 before and after each of the left wing 11 and the right wing 12, 13 -1) and the second left wing driving portion 13-2, and the first right wing driving portion 14-1 and the second right wing driving portion 14-2 may be provided.

In this case, the left / right wings 11 and 12 may be coupled to the main body 1 through a hinge H of a freely rotatable ball type provided at a middle portion of one side end.

In this case, the left / right wings 11 and 12 can be freely rotated up and down and left and right about the hinge H, so that a flexible wing movement can be made.

In addition, the first left wing driving unit 13-1 and the second left wing driving unit 13-2 are provided with two pairs of the left wing driver 1 (13a) and the left wing driver 2 (13b) spaced apart from each other. The first right wing drive 14-1 and the second right wing drive 14-2 may also be spaced apart from each other by the pair of the right wing drive 1 (14a) and the right wing drive 2 (14b). It may be prepared for.

In this state, as shown in FIG. 15, the first left wing driving unit 13-1 and the second left wing driving unit 13 are provided by the above-described operation signal providing unit 20 and the control unit 30. -2) and the first right wing driving unit 14-1 and the second right wing driving unit 14-2 can be controlled independently.

That is, when the acceleration handle of the operation signal providing unit 20 is raised in the acceleration direction, the acceleration signal is provided to the control unit 30, and the control unit 30 increases the frequency according to the input acceleration signal and the left / right wing ( 11) (12).

At this time, one of the important parts of the present invention can independently drive the first left wing drive 13-1 and the second left wing drive 13-2, the frequency applied from the control unit 30 Accordingly, the wing movement can be made by varying the width and speed of the wing movement, which is also true of the first right wing driving unit 14-1 and the second right wing driving unit 14-2.

In this case, as shown in FIG. 16, the wing motions of the first left wing drive 13-1 and the first right wing drive 14-1 of the left and right wings 11 and 12 are measured. When the width is widened and the width of the wing motion of the second left wing drive part 13-2 and the first right wing drive part 14-2 is relatively narrowed, the flow of air due to the wing motion is directed backward and is advanced. can do.

At this time, the drawing is shown to rotate the wing to the left and right about the hinge (H), but the wing movement to the left and right at the same time as the vertical wing movement, very similar to the wing of the birds occurs.

In this case, as shown in FIG. 17, the widths of the blade movements of the first left wing drive 13-1 and the first right wing drive 14-1 of the left and right wings 11 and 12 are determined. When the width is narrowed and the width of the wing motion of the second left wing drive part 13-2 and the first right wing drive part 14-2 is relatively widened, the air flow due to the wing motion is directed forward and can be reversed. have.

In addition, the present invention, as shown in Figure 18, the left wing 11 and the right wing 12, each of the front and rear pairs of the first left wing drive 13-1 and the second left wing drive ( 13-2) and the first right wing driving unit 14-1 and the second right wing driving unit 14-2, wherein the left and right wings 11 and 12 are provided at both sides of one end. It can be coupled to the main body 1 through a pair of ball type hinge (H ').

In this case, as shown in Figs. 19 and 20 of the accompanying drawings, in the state in which both sides of the front portion and the rear portion of the wing (H ') supports the wing movement in the state coupled to the main body 1, Width of the blade movement of the first left wing drive unit 13-1 and the first right wing drive unit 14-1 of the left and right wings 11 and 12, and the second left wing drive unit 13-2 and the first As described above, according to the width of the blade movement of the right wing drive unit 14-2, the direction of travel can be determined by switching the air flow direction.

At this time, the left / right wing (11) 12, as shown in the accompanying drawings, as shown in Figure 21, if the wing portion (C) made of synthetic resin or fabric paper, except for the edge portion of the wing, as described above During the wing movement, the flap of the wing fabric (C) is more and more wing movement similar to the wing of the bird occurs.

As described above, the present invention can improve flight efficiency by minimizing the total weight of the vehicle by simplifying and reducing the driving structure.

In addition, the present invention can improve the propulsion by placing the drive structure on the wing to reduce the weight of the body and increase the weight acceleration in the wing movement.

In addition, the present invention can improve the reversibility by enabling the vertical rise / fall, take off / landing, forward, turning, as well as backward.

In addition, the present invention, as shown in Figure 22, the outer circumferential surface or the outer circumferential surface and the inner circumferential surface of the coil which is one embodiment of the means constituting the left wing drive 13 and the right wing drive 14, the nonmagnetic material 51 ) To be accommodated in the housing 50 blocked by the magnetic panel 52 on the upper and lower surfaces of the coil, and fixed to the housing 50 by bonding or welding to the left and right wings 11 and 12. Can also be.

In this way, while protecting the coil from the outside, the magnetic force portion can be concentrated to maximize the efficiency.

In addition, the present invention may be configured by manufacturing the left wing drive unit 13 and the right wing drive unit 14 by insert injection when manufacturing the left / right wing (11) (12).

At this time, in the present invention, the terminal part of the coil (the part which is drawn out and connected to the electric circuit) may be protected by coating with a synthetic resin or other protector on the surface of the corresponding wing part to which the coil is fixed.

In addition, the present invention is provided with a spring in the hinged portion of the left / right wing (11) (12) or the position where the left / right wing driving portion (13) (14) is located, the left / right wing (11, 12) You can also add elasticity to the wing motion of the.

Finally, the present invention, as shown in the accompanying drawings, Figure 23, both wings (the figure shows the right wing 12 as an example), for example, the main wing 12a and the driven wing constituting the right wing 12 The inner / outer peripheral surfaces of the right wing actuator 1 (14a) and the right wing driver (2b) 14b respectively provided at 12b may be configured to be curved.

At this time, the degree of curvature of the left / right wing (11) 12 during the wing movement, the left wing drive 1 (13a) and the right wing drive 1 (14a) and the left wing drive 2 (13b) and the right wing It can be set according to the mutual flow path and angle of the drive body 2 (14b).

In this case, according to the degree of inclination of the right wing driving body 1 (14a) and the right wing driving body 2 (14b) in the wing movement process can be carried out without interference with each other, as well as the right wing driving Even if the inclination degree of the sieve 1 (14a) and the right wing driving body 2 (14b) is changed, it maintains a constant gap and wing movement, so that the action of a constant electromagnetic force is made.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is to be understood that the invention is not limited to the disclosed exemplary embodiments.

Rather, it will be apparent to those skilled in the art that many changes and modifications to the present invention are possible without departing from the spirit and scope of the appended claims.

Accordingly, all such suitable changes and modifications and equivalents should be considered to be within the scope of the present invention.

1 is a perspective view showing a configuration according to an embodiment of the present invention.

Figure 2 is a front cross-sectional view showing in more detail the configuration according to an embodiment of the present invention.

Figure 3 is a partial front cross-sectional view showing the configuration of the left / right wing drive of the configuration according to an embodiment of the present invention.

Figure 4 is a partial front cross-sectional view showing another configuration of the left / right wing driving portion of the configuration according to an embodiment of the present invention.

Figure 5 is a side cross-sectional view of the wing portion showing the angle of the wing of another configuration according to an embodiment of the present invention.

Figure 6 is a block diagram showing an embodiment according to the wing control of the present invention.

Figure 7 is a front sectional view showing the action according to an embodiment of the present invention.

8 is a perspective view showing a further configuration according to an embodiment of the present invention.

9 is a partial side cross-sectional view showing the propulsion wing portion of a further configuration according to an embodiment of the present invention.

10 is a block diagram showing another embodiment according to the wing control of the present invention.

Figure 11 is a partial side cross-sectional view showing the action of the propulsion wing portion of a further configuration according to an embodiment of the present invention.

12 is a perspective view showing another configuration according to an embodiment of the present invention.

13 is a plan view showing another configuration according to an embodiment of the present invention.

14 is a side cross-sectional view showing a wing portion of another configuration according to an embodiment of the present invention.

Figure 15 is a block diagram showing another embodiment according to the wing control of the present invention.

16 and 17 is a cross-sectional view of the wing portion showing the state of the wing motion of another configuration according to an embodiment of the present invention.

18 is a plan view showing another configuration according to an embodiment of the present invention.

19 and 20 is a sectional view of the wing portion showing a wing motion of another configuration according to an embodiment of the present invention.

21 is a plan view showing another configuration according to an embodiment of the present invention.

Fig. 22 is a partial sectional view showing yet another configuration according to an embodiment of the present invention.

Fig. 23 is a partial sectional view showing yet another configuration according to an embodiment of the present invention.

<Description of the symbols for the main parts of the drawings>

10: aircraft 11: left wing

11a, 11b: left main / follower wing 12: right wing

12a, 12b: right main / driven wing 13: left wing drive part

13-1: 1st left wing drive part 13-2: 2nd left wing drive part

13a, 13b: left wing drive 1,2, 14: right wing drive

14-1: 1st right wing drive part 14-2: 2nd right wing drive part

14a, 14b: Right wing drive 1,2, 15: Propulsion wing

15a, 15b: propulsion main / follower wing 16: propulsion wing driving part

16a, 16b: Propulsion wing drive 1,2 H, H ': Hinge

20: operation signal providing unit 30: control unit

40: power supply unit 50: housing

51: nonmagnetic material 52: magnetic material

1: main body

Claims (31)

In a vehicle that obtains a driving force through the wing movement, the attraction force and repulsion are alternately provided through the change of the electromagnetic force on the surfaces of the left and right wings 11 and 12 provided on both sides of the main body 1, respectively. 11) (12) A vehicle characterized by obtaining a driving force by generating mutually independent wing movement. According to claim 1, wherein the left wing (11) and the right wing (12) main / driven blades (11a, 11b) (12a, which one end is fixed at intervals above and below the main body 1, respectively) 12b)) is provided symmetrically characterized in that the aircraft. The main and driven blades (11a, 11b) (12a, 12b) of each of the left and right blades 11 and 12 are hingedly coupled to one end of the main body 1, respectively. Flying vehicle. The hinge main body (11a) (12a) of the main / driven blades (11a, 11b) (12a, 12b) of each of the left and right wings (11, 12) is hinged to the main body (H). A vehicle characterized by a combination. According to claim 2, wherein the left driving blade (11a), the left driven blade (11b) of the left wing (11) and the right driven blade (12a) and the right driven wing (12b) of the right wing (12), respectively, electromagnetic force The left wing drive 13 including the left wing drives 1, 2 (13a) and 13b which are mutually attracted / repulsed by the right wing and the right wing drive 1, 2 (14a) which are mutually attracted / repulsive by the electromagnetic force. Aircraft, characterized in that the right wing driving portion (14) comprising a 14b is provided. 6. The left wing actuators 1, 2 (13a) and 13b and the right wing actuators 1 and 2 (14a) and 14b respectively correspond to coils according to directions of coils and currents flowing through the coils. Aircraft characterized in that it comprises a magnetic circuit that acts as a repulsive force. 7. The left wing driver 1 (13a) and the right wing driver 1 (14a) are magnetic circuits, and the left wing driver 2 (13b) and the right wing driver 2 (14b) are coils. Air vehicle, characterized in that. 7. The left wing driver 1 (13a) and the right wing driver 1 (14a) are coils, and the left wing driver 2 (13b) and the right wing driver 2 (14b) are magnetic circuits. Air vehicle, characterized in that. 9. A vehicle according to any one of claims 6, 7, or 8, wherein the magnetic circuit includes a magnet. 2. The vehicle according to claim 1, wherein the left and right wings (11) (12) are planar without an inclination with respect to the ground. Aircraft according to claim 1, characterized in that the left / right wings (11) (12) are inclined forward of the main body (1). The vehicle of claim 11, wherein the inclination angle is 10 degrees to 20 degrees. 6. The flying vehicle according to claim 5, wherein the movement width of the left and right driving blades (11a) (12a) is greater than the upper direction when the attraction force and the repulsive force are applied. [6] The direction signal according to claim 5, wherein the left and right wing drives 13 and 14 for wing movement of the left and right wings 11 and 12 are digital signals indicating a position movement degree according to the operation of the rudder and the acceleration handle. When the direction signal and the acceleration / deceleration signal are input from the operation signal providing unit 20 and the operation signal providing unit 20 which are converted into and provided with the acceleration / deceleration signal, the frequency is converted and output according to the corresponding direction signal and the acceleration / deceleration signal. Air vehicle, characterized in that controlled by the control unit (30). 15. The vehicle according to claim 14, wherein the operation signal providing unit (20) is made of a wire / wireless controller using a separate high frequency wave. 15. The vehicle according to claim 14, wherein the operation signal providing unit (20) is made of a wire / wireless controller provided in the main body (1). According to claim 5, wherein the left / right wing (11, 12) is a portion in which the left / right wing driving portion (13, 14) is seated and fixed to the panel, the front of the panel on the side of the wing Aircraft characterized in that made of a streamlined frame up to the corresponding edge portion, the wing fabric made of thin synthetic resin or fabric paper is fixed by ultrasonic welding or bonding to the frame portion. Aircraft according to any one of the preceding claims, characterized in that the left / right wing (11) (12) consists of a panel. [6] The wing fabric according to any one of claims 1 to 5, wherein the left / right wings 11 and 12 are made of a frame of the entire outer rim, and made of a thin synthetic resin or fabric paper therein. Aircraft characterized in that the fixed by the ultrasonic welding or bonding. 2. The vehicle according to claim 1, further comprising a propulsion wing (15) which generates propulsion force through a blade movement at the rear of the main body (1). 21. The vehicle according to claim 20, wherein the propulsion wing (15) comprises propulsion main / driven wings (15a, 15b) fixed at one end at intervals above and below the rear end of the main body (1). 22. The vehicle according to claim 21, wherein the propulsion main / driven wing (15a, 15b) may be hinged to one end of the main body (1), respectively, and only the propulsion main wing (15a) is hinged. The propulsion wing drive unit according to claim 21, wherein the propulsion drive blade (15a) and the propulsion driven wing (15b) include propulsion wing drives (1, 2 (16a), 16b) for mutual attraction / repulsion by electromagnetic force ( 16) is provided, characterized in that the aircraft. According to claim 1, wherein the left wing (11) and the right wing (12), respectively, a pair of front and rear left wing drive 13-1 and second left wing drive (13-2), and the first right side The wing body (14-1) and the second right wing driving unit (14-2), characterized in that the aircraft is configured to provide. The aircraft according to claim 24, wherein the left and right wings (11) and (12) are coupled to the main body (1) through one freely rotatable ball type hinge (H) provided at an intermediate portion of one end. . According to claim 1, wherein the left wing (11) and the right wing (12), respectively, a pair of front and rear left wing drive 13-1 and second left wing drive (13-2), and the first right side A wing drive part 14-1 and a second right wing drive part 14-2 are provided, but the left and right wing parts 11 and 12 have a pair of ball type hinges H 'provided at both ends of one end. Air vehicle, characterized in that coupled to the main body (1) through. 27. The flying vehicle according to claim 26, wherein the left wing (11) and the right wing (12) except for the edge portion of the wing is made of synthetic resin or fabric paper. 6. The magnetic body panel 52 according to claim 5, wherein the outer circumferential surface of the coil, which is one of the means for constituting the left wing drive portion 13 and the right wing drive portion 14, is blocked by a nonmagnetic material 51, and the magnetic panel 52 is disposed on the upper and lower surfaces of the coil. It is accommodated in a housing (50) blocked by the air vehicle, characterized in that the housing (50) is fixed to the left / right wing (11) (12) by bonding or welding. The method of claim 5, wherein the outer circumferential surface and the inner circumferential surface of the coil, which is one of the means constituting the left wing drive portion 13 and the right wing drive portion 14, are blocked by a nonmagnetic material 51, and a magnetic panel (upper and lower surface of the coil) 52) is accommodated in a housing (50) blocked by the aircraft, characterized in that the housing (50) is fixed to the left / right wing (11) (12) by bonding or welding. The left wing actuator 1 (13a) and the right wing provided in the main blade (11a) (12a) and the driven wing (11b) (12b) constituting the left / right wing (11, 12), respectively. The wing body 1 (14a) and the left wing drive body 2 (13b) and the right wing drive body 2 (14b), characterized in that the inner and outer peripheral surfaces are configured to be curved, respectively. 31. The method of claim 30, wherein the degree of curvature is left wing drive 1 (13a) and right wing drive 1 (14a) and left wing drive 2 (13b) during the wing movement of the left and right wings (11, 12) And the right wing driving body 2 (14b) is set according to the mutual flow path and angle.

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