JP2007032551A - Reciprocating type propulsion moving body - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a method for propelling a moving body in an inertial space with propellant or centrifugal force not depending on ground friction reaction. <P>SOLUTION: When a pair of weights having mutually reverse rotation are located approximately overlapping each other backward or approaching each other, they are driven to be rotated in the direction of moving one apart from the other, whereby the moving body formed with the pair of weights having mutually reverse rotation is also eventually moved backward with reaction. When the pair of weights is mutually rotated and moved forward in the propelling direction, the pair of weights having mutually reverse rotation produces frontward centrifugal resultant force so that the backward movement of the moving body is stopped and changed into forward movement. When the pair of weights are mutually rotated and moved backward, they produces backward centrifugal resultant force so that forward movement of the moving body is decelerated and stopped and at the same time braking is given to the pair of weights approaching each other in the rotating direction to be slowed down or stopped. The backward rotation control of the pair of weights having mutually reverse rotation results in the moving body to be propelled and moved forward by a backward movement distance or longer. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

The present invention does not use a propellant for controlling the attitude of a flying object or satellite or changing orbits in outer space, and enables to travel without using reaction force due to tire friction propelled in a horizontal state on the ground And a reciprocating propulsion moving body for display.

The method of propelling in space or on the ground using the centrifugal force published in the past is in writing. In order to change the trajectory of flying objects in outer space, swing-by navigation using the reaction force of the propellant and the attraction of the stars and attitude control of the satellite, magnetic orbiters, propellants, ions, and microwaves are used to change the orbit. Are known.
On the ground, it is driven by friction between the ground and tires and relies on the external physical environment.

There is also a method of canceling the reaction caused by the moment of inertia at the driving and braking positions and propelling (see, for example, Patent Document 1).
There is also a method of propulsion by controlling the rotational speed that is not stopped in order to eliminate backward movement due to centrifugal force (see, for example, Patent Document 2).

JP 2000000427072 JP 62-103486 A

The solution of the problems of the propulsion device by the conventional inertia force and centrifugal force described above is the action of the third law of Newtonian motion. The reaction and inertia laws are important, but the vehicle is configured to rotate the weight by the reaction when the weight with the radius around the axis is rotated from the rear position to the front position. Although the mass including the weight is also related to the mass of the vehicle and the mass of the vehicle, the vehicle is considered to move backward.

On the ground, the backward movement due to the centrifugal force generated by the rotation that the weight does not stop is apparently stopped by the ground resistance of the ground and the tire and the rotational resistance of the multiple bearings used on the tire axle, and the inertial space In the outer space, the third law works even if it is gently pushed from an object of the same mass close to the mass with the mass. The reaction is considered to be separated from each other, and the friction that is mainly considered in the horizontal state on the ground is the ground resistance of the ground and the tire, the rotational resistance of the bearing that supports the axle of the tire, and the weights counteract each other in reverse rotation. By taking into account the increase in grounding resistance and rotational resistance due to the movement of the center of gravity by rotating forward and backward, the attitude of the flying object and satellite is changed and the orbit is changed by the reaction force due to the propellant in outer space, and tires on the ground It was made in order to solve these drawbacks.

In order to achieve the above object, the present invention is directed to a pair of shafts that are reversely rotated and driven by driving means, and to the upper end portions of the pair of shafts in a direction perpendicular to the axial direction of the shafts. A propulsion device comprising a pair of counterweights, each of which is fixed to one of the supporting members and having a weight fixed to the other of the pair of supporting members disposed above and below and configured to rotate counterclockwise. In the mobile body provided,
When the position of the pair of weights that rotate reversely to each other is at the rear, the moving body provided with the propulsion device is moved backward by controlling the rotation, and the moving body that pushes forward more than the backward moving distance Characteristic reciprocating propulsion mobile

The second problem solving means has a second feature of a reciprocating linear motion mechanism provided with the propulsion device and a movable body provided with the reciprocating linear motion mechanism.

Further, the third problem solving means is that the pair of weights that are reversely rotated in the reverse direction are located behind and the pair of weights in the rotational direction approaching each other are in cooperation with the driving means and the regeneration mechanism. A third feature is that the rotation directions are away from each other.

A fourth problem-solving means has a fourth feature of a pair of capacitors that are reversely rotated with each other and that are replaced with a capacitor instead of the weight.

A drive shaft of a reduction gear mounted on the electric motor of the drive means, a pair of shafts that are driven to rotate reversely to each other, the pair of shafts is a shaft, and an upper end of each shaft of a hollow shaft that is supported by the shaft A pair of support members oriented in a direction perpendicular to the axial direction of each axis is fixed to the part, and a weight is fixed to the other support material arranged vertically, and a pair of weights are fixed to each other. In the propulsion device configured with the weight and the moving body provided with the propulsion device,
When starting, the propulsion device is provided by rotating in the direction of rotation away from each other by driving when the position of a pair of weights that rotate in reverse to each other is at the rear, substantially overlapping, or close A vehicle moving on a horizontal ground is inevitably moved backward by reaction from the starting position, and when a pair of weights that rotate counterclockwise in front of the propulsion direction rotates, the pair of weights rotate counterclockwise. The backward movement of the vehicle provided with the propulsion device is stopped by the combined force of the forward centrifugal force generated by the operation, and this time the propulsion is moved and the momentum increases, the position of the vehicle provided with the propulsion device at this time Return to the starting position, and when the pair of weights are rotated and moved to each other on the rear side opposite to the propulsion direction side, the backward movement of the vehicle provided with the propulsion device is decelerated from the deceleration by the resultant force of centrifugal force. Rotation approaching each other at the same time as stopping By applying braking to the pair of weights at approximately the same position, or stopping nearby or slowing down, the vehicle is propelled forward by more than the distance the vehicle has moved backward, thus the position of the pair of weights By controlling the rotation at the rear, the vehicle is propelled forward by the electric energy alone beyond the distance the vehicle has moved backward, and the effect of running without using the reaction force due to tire friction in the horizontal state is produced. It is suitable for experiments for a mobile body in which the propulsion device is directly provided in the space of inertial space.

The vehicle provided with the propulsion device according to claim 2 is rotated in a rotational direction in which the pair of weights move away from each other by driving when the positions of the pair of weights are substantially overlapped or close to each other. Then, the vehicle provided with the propulsion device is moved backward due to the reaction, and in order to improve this, the propulsion device is installed in the operating part of the reciprocating linear motion mechanism, and the base of the reciprocating linear motion mechanism is moved in the inertial space or the ground. It is improved by being installed in the moving body, and when the position of the pair of weights that are reversely rotated with each other when they are first activated is substantially overlapped or close to the rear, When only the operating part of the reciprocating linear motion mechanism provided with the propulsion device is rotated backward in the direction of rotation and moved backward while sliding the base, and the pair of weights are rotated in reverse in the forward direction, Centrifugal force The operating portion of the reciprocating linear motion mechanism provided with the propulsion device is moved from the backward movement by the combined force, moved forward while sliding the base while being accelerated from the stop, and the reciprocating linear motion mechanism provided with the propulsion device. The momentum of the operating part increases, the momentum of the operating part of the reciprocating linear motion mechanism provided with the propulsion device is stopped by the elastic body to return to the starting position at the time of driving, and moves to the moving body in the stopped state, and The propulsion device is a combined momentum, and only the moving body is propelled forward, and when a pair of weights are rotated and moved to the rear opposite to the propulsion direction side, the propulsion device uses the resultant force of centrifugal force in the backward direction. At the same time as the forward movement of the moving body provided with deceleration is stopped from deceleration, a pair of weights in the rotating direction approaching each other is braked to substantially overlap, or stop at a nearby position, or control the rotation backward at a low speed By doing If the propulsion is applied to a flying object that combines the propulsion device and the linear motion mechanism in the space of inertial space, or to change the orbit of an artificial satellite, the propellant is not needed. In addition, since the linear motion mechanism is installed on the moving body that moves on the ground, the moving body is improved to propulsion movement only without the backward movement.

In claim 3, the moment of inertia of the pair of weights rotating in the opposite directions when the rotational speed by driving is applied to the pair of weights rotating in the reverse direction of the coaxial reversing mechanism and the braking is applied at the rotation speed. In order to reduce the drive system and supporting metal due to the load, a large current flows through the motor, and the spring-link mechanism of the regenerative mechanism is provided with a joint between the support materials, the support material on the shaft side and the weight side The pair of weights that are formed between the first and second support members, which are reversely rotated with respect to each other when they are first driven, are substantially overlapped in the rear, or when they are close to each other, they rotate in the direction of rotation away from each other. When a pair of shaft-side support members that are reversely rotated with each other by the driving means are braked and stopped in a rotating direction close to each other where the pair of weights are rotated one by one, the spring of the regeneration mechanism -Inertia of weight side support with link mechanism The energy of the moment is absorbed, and this time, the moment of inertia of the weight side support material is released in cooperation with the driving means in the opposite direction of rotation in the direction of rotation where the pair of weights move away from each other. By controlling the rotation in the rear, the efficiency of the electric motor of the driving means is also improved, and as described above, the motor moves in an inertial space or a ground where a pair of reciprocating weights provided with a regeneration mechanism are configured. The moving object also has the effect of being moved forward more than the backward movement distance,

Further, in claim 4, by replacing the pair of weights provided on the other of the upper and lower support members with a shape in which a capacitor installed in the moving body is installed, the artificial satellite and the flight By providing it on the body and the moving body of the vehicle, the mass is reduced, and the propulsion movement distance is also extended before, so that the space can be used effectively.

FIG.

Hereinafter, the best mode for carrying out the present invention will be described. FIG. 1 is a side view of a vehicle 1 provided with a propulsion device 2. A pair of shafts that rotate in reverse to each other includes a coaxial reversing mechanism and a biaxial parallel mechanism. Since the turning radius of each attached support member becomes large, the coaxial reversing mechanism will be described.

FIG.

FIG. 2 is a top view of the vehicle 1 provided with the propulsion device 2. In order to explain a simple structure using FIGS. 1 and 2, four hard tires 38 are provided in order to improve stability and reduce ground resistance. A vehicle 1 that is a moving body, a capacitor 5 that constitutes the propulsion device 2 in the vehicle 1, a coaxial reversing mechanism 7 that is driven by a speed reducer 4 that is mounted on an electric motor 3, and the coaxial reversing mechanism 7 rotate in reverse. A pair of shafts 8a. 9. Each support material 12.13 fixed on one side to 9 and a weight 14.15 fixed on the other of the support materials 12.13, and a propulsion device composed of these devices (hereinafter abbreviated as a propulsion device). 2), the main shaft 9 of the rotary shaft supported by the bearing of the flange 8b provided in 2, the lower driven bevel gear 11 fixed to the main shaft 9, and the upper driven bevel gear 10 are opposed to each other. The drive bevel gear 5 fixed to the drive shaft of the speed reducer 4 mounted on is engaged with the upper and lower driven bevel gears 10.11 having the same number of teeth facing each other, and the upper driven bevel gear 10 is provided with a bearing. Fixed to a flange 8a also serving as a hollow shaft, the flange 8a is pivotally supported by the main shaft 9, and a lower support oriented in a direction perpendicular to the axial direction of the flange 8a also serving as a hollow shaft at the upper end of the flange 8a. One side of the material 13 is fixed, and the upper end of the main shaft 9 One of the upper support members 12 oriented in the direction perpendicular to the axial direction of the main shaft 9 is fixed, the weight 14 is fixed to the other of the upper support members 12, and the other weight 15 is also a lower support member. The weight 15 of the lower support 13 fixed to the other of the upper support 12 and symmetrical to the weight 14 of the upper support 12 is formed so as not to be in contact with the receiver 17 of the remote control device manually by wire or wirelessly. The signal of the wireless receiver 17 is controlled via the control device (PWM control or the like) 16 to drive or brake the electric motor 3. The moving body directly provided with the propulsion device 2 for the inertial space is used for experiments, and the illustration and description are omitted.

FIG.

FIG. 3 is a correlation diagram showing the movement of the pair of weights 14.15 and the moving vehicle 1 that are reversely rotated with each other. The upper weight 14 is a white circle and the lower weight 15 is hatched in the circle. The dotted line indicates the reference position (1) of the vehicle 1 in a stopped state, and the propulsion side in which the dotted circle is divided in half around the main shaft 9 of the rotating shaft is indicated by diagonal lines. When the pair of weights 14.15 are substantially superposed (1) at the rear 40 or rotated from a nearby position, the vehicle 1 is shown. Is a schematic diagram showing the movement from (2) to (6),

The pair of weights 14.15 are substantially superposed (1) at the rear 40, or the position in the vicinity means that when the pair of weights 14.15 are driven for the first time, they are substantially superposed (1). However, if there is no mechanical or electrical braking device at the position detection device at the position where the rotation is stopped and stopped at the rear 40 in one continuous rotation, or at a low speed, the rotation of the motor is manually controlled by visual observation. It will shift greatly from the shifted position,

As shown in FIGS. 1 to 3, a moving object to be controlled on a horizontal ground or a toy vehicle 1 is manually wired or a signal of a wireless receiver 17 is controlled by a control device (PWM control). Etc.) When the electric motor 3 is rotated via 16, it is substantially superposed (1) at the position of the rear 40 shown in FIG. When the weight 14 and the weight 15 at the bottom of the black circle are rotated reversely to each other, the vehicle 1 shown in (2) is inevitably moved backward by reaction and further rotated (3). When it is rotated and moved to a position at an approximate angle of the front 39, the backward movement of the vehicle 1 is stopped by the combined force of the forward centrifugal force generated by the pair of weights 14.15 rotating in the reverse direction. This time, the vehicle 1 is propelled forward and the combined force of the forward centrifugal force When the amount of movement increases and the pair of weights 14.15 are rotationally moved to the position of the approximate angle of the front 39 indicated by (4), the vehicle 1 returns to the starting position, and the abbreviation (5) of the rear 40. When it is rotationally moved to the angular position, the propulsive movement is stopped in front of the vehicle 1 by the resultant force of the centrifugal force in the backward direction, and at the same time, each rotation of the pair of weights 14.15 at the rear 40 position is performed by the electric motor 3. The brake is applied and the pair of weights 14.15 are decelerated as they approach each other, and the pair of weights 14.15 are rearranged in the rear (40) (6), or stopped at a nearby position, or slow. By controlling the rotation at the rear 40, the vehicle 1 is propelled forward by more than the distance traveled backward.

FIG.

FIG. 4 shows a diagram in which a moving vehicle 1 is provided with a reciprocating linear motion mechanism. The reciprocating linear motion mechanism has an electrically driven linear motor 19 and a mechanical linear guide 20, and depends on the use environment and economics. In the case of the linear guide 20 which is provided and has a small friction coefficient of the reciprocating linear motion mechanism, the use on the ground is optimal and will be described. The propulsion device 2 configured with a pair of weights 14.15 that rotate in reverse to each other is fixed to the operating portion 22 of the linear guide 21, and the base 23 of the linear guide 21 is installed in the vehicle 1 and is operated on the vehicle side 1 or in operation. In order to prevent the operation unit 22 from colliding with the part 22 side, a shock absorber 25 for stopping from deceleration is installed, the shock absorber 25 is made of a low-repulsion coefficient that is difficult to deform, A stop holding device (such as an electromagnet) 24 for stopping the reaction of the stop from the deceleration accompanying the shock absorber 25 is installed, the propulsion device 2 configured as described above is installed in the operating portion 22 of the linear guide 21, and the linear guide By fixing the base 23 of the vehicle 21 to the vehicle 1,

FIG.

FIG. 5 is a correlation diagram showing the movement of the pair of weights 14.15 that reversely rotate with each other and the moving vehicle 1. The upper weight 14 is a white circle, and the lower weight 15 is a black circle. The dotted line indicates the reference position (1) of the vehicle 1 in a stopped state, and the front side 39 of the semicircle that represents the propulsion side that is divided in half with the dotted circle centered on the main shaft 9 of the rotating shaft When the opposite semi-circular rear 40 is shown and the pair of weights 14.15 are substantially superposed (1) at the rear 40 or rotated from a nearby position, the vehicle 1 is moved from (2) to (6) Schematic showing the movement up to

When the present invention is used in the above structure, the toy of the vehicle 1 that is optimal on a horizontal ground or the vehicle 1 in which the linear guide 21 is installed on the vehicle 1 for display is in a stopped state. When the position of the pair of weights 14.15 that are reversely rotated while maintaining the position is substantially overlapped (1) in the rear 40 or is in the vicinity, when the motor 3 is driven, the pair of weights 14 .15 are reversely rotated so as to move away from each other, only the operating part 22 of the propulsion device 2 reacts and inevitably only the operating part 22 of the propulsion device 2 slides the base 23 in the backward movement from the starting point (1). When the pair of weights 14.15 that are rotated in reverse to each other rotate and move to the front 39, the combined force of the forward centrifugal force generated by the pair of weights 14.15 being rotated in reverse from each other, The operating unit 22 of the propulsion device 2 slides backward. It is stopped (3), and this time it is propelled and moved forward from the stop, and the momentum of the operating part 22 of the linear guide 24 in which the propulsion device 2 is installed also increases, so that it returns to the starting point (4) during driving. A pair of weights 14.15 that are stopped by a body (low repulsion coefficient that is difficult to deform) 25, and that the movement of the operating portion 22 of the linear guide 21 is fixed by a stop holding device (electromagnet or the like) 24, and that rotate reversely to each other. The momentum of the configured propulsion device 2 moves to the vehicle 1 and becomes a combined momentum, and only the vehicle 1 is propelled forward, and the pair of weights 14.15 are positioned at a substantially angular position (5) in the rear 40. When it is rotationally moved, the propulsion movement of the vehicle 1 is stopped forward by the resultant centrifugal force of the centrifugal force, and at the same time, the rotation of the pair of weights 14.15 at the position of the rear 40 is braked by the electric motor 3. Give a pair of weights 14.15 to each other Then, it is decelerated and the rear 40 (6) is almost superposed, or it stops at a nearby position or becomes low speed, and the stop holding device (electromagnet etc.) 24 is released, so that the rear 40 rotates. By controlling, the vehicle 1 is propelled forward only.

FIG.

FIG. 6 is a perspective view in which a linear motor 18 is provided on an artificial satellite 26 that orbits the earth 31. The flying object basically has the same structure and is not shown in the figure. A linear motor 18 that is optimal in the propulsion axis direction is provided, which is used as an auxiliary in combination with the rocket engine of chemical fuel. The propulsion device 2 described above is provided in the operating part 19 of the linear motor, and the base 20 of the linear motor 18 is provided. Are provided on both ends of a support member 27 extending in both directions from the center of gravity of the artificial satellite 26 or the flying body, and a base 20 of the linear motor 18 is fixed to the two bases, and the two bases are fixed to the two bases. A pair of weights that reversely rotate the propulsion device 2 provided on both ends of the artificial satellite 26 and the flying object on a pedestal provided with the motor 29.30 of each axis that can change the propulsion device 2 into a two-dimensional direction axis. Propeller shaft direction of 4.15, is formed so as toward the center of gravity of the satellite 26 or flying object, a solar cell 28 is a schematic diagram provided in place have no influence on the rotation of the pair of weight 14.15. A position detection device such as a linear encoder omits the display in the figure.

When the present invention is used in the structure as described above, the power source is supplied by the battery 6 or the solar battery 28, and the controller 16 has two motors 29.30 and two linear motors 18 on two bases. Are supplied to two electric motors 3 that drive a pair of weights 14.15 that rotate reversely to each other, and drive a pair of weights 14.15 that rotate reversely to each other, such as an artificial satellite 26 or a flying object. By controlling the rotation position, driving and synchronization of the linear motor 18 and the signal for detecting the position of the pedestal that can change the propulsion device 2 in the two-dimensional direction by the electric motor 3 with a computer, there are two cases when changing the trajectory. By making the propulsion axis directions of the pair of weights 14.15 that rotate in reverse to each other in the same direction, the center of gravity of the artificial satellite 26 or the flying object is changed, and in the case of attitude control, a pair of opposing ones are mutually connected. Direction of propulsion axis of a pair of counterweights 14.15 rotating in reverse Once in the opposite direction to each other physician, it is rotated about the center of gravity of the satellite 26 and projectile, capable attitude control and orbit change of the satellite 26 and projectile in space only electrical energy,

Basically, the linear guide propulsion method provided in the vehicle 1 is the same as that of the pair of weights 14.15 of FIG. The method of trajectory change in the same propulsion axis direction is that the position of a pair of weights 14.15 that reversely rotate relative to each other upon first activation is substantially superposed (1) at or near the rear 40 of FIG. When the motor 3 is driven, the pair of weights 14.15 are rotated in a rotating direction away from each other, and only the operating part 19 of the linear motor 18 provided with the propulsion device 2 by reaction acts on the linear encoder 20. The moving unit 19 of the propulsion device 2 is slid and moved (2) from the starting point in synchronization with the retreating speed via a position detection device such as a der. The forward centrifugal The operating part 19 of the linear motor 18 provided with the propulsion device 2 is slid and moved in synchronism with the propulsion movement speed while being accelerated from the stop position (3), and the propulsion movement speed is synchronized with the combined force of The momentum of the operating part 19 of the linear motor 18 provided with the propulsion device 2 is also increased, braking is applied by the linear motor 18 to return to the starting position (4) during driving, and the propulsion device is held electrically. The momentum of the operating part 19 of the linear motor 18 provided with 2 is transferred to the artificial satellite 26 or the flying body in a constant direction state, and the combined momentum is changed to only the artificial satellite 26, the propulsion direction side and When the pair of weights 14.15 are rotated and moved in the opposite rear 40, the orbital change of the artificial satellite 28 provided with the propulsion device 2 or the flying object is made by the combined force of the backward centrifugal force. At the same time as stopping from speed, a pair of weights 14.15 in the direction of rotation (5) approaching each other is braked and substantially superposed (6), or stopped at a nearby position, or at low speed and backward By controlling the rotation, the orbit of the artificial satellite 26 and the flying object can be changed, and the attitude can be controlled by stopping one of the propulsion devices 2 at both ends of the artificial satellite 26. It can be done in the opposite direction.

FIG.

FIG. 7 is a schematic diagram in which a pair of weights 14.15 in the rotational direction approaching each other indicated by an arrow at the rear 40 is given in the rotational direction away from each other in cooperation with the driving means and the regeneration mechanism.

FIG.

FIG. 8 is a top view of the support member 12 provided with the spring-link mechanism of the regenerative mechanism. The weight on which the weight-side support member 41 is rotated by the shaft-side support member around the joint shaft 34 of the spring-link mechanism. A schematic diagram is shown in which the energy of 14 moments of inertia is absorbed and released by a spring 32.

FIG.

9 is a side view of the upper and lower support members 12.13 provided with the spring-link mechanism of the regenerative mechanism. The joint shaft 34 is provided between the support members, and one of the springs 32 is fixed to the shaft-side support member. 32 shows a schematic view of a spring-link mechanism of a regenerative mechanism in which the other 32 is fixed to the weight side support member 41 and each of the upper and lower weights 14.15 is rotated about the joint shaft 34. ,

When this is used, the position of the pair of weights 14.15 that rotate counterclockwise is substantially superposed at the rear 39, or the pair of weights 14.15 that are in the vicinity are rotated away from each other. When driving from a stopped state, the driving energy is once absorbed by the spring-link mechanism of the regenerative mechanism in cooperation with the electric motor 3 of the driving means, and is released and rotated one by one at a rotational speed. When the pair of weights 14.15 approaches each other, the pair of shaft-side support members rotating in the opposite directions by the motor 3 are braked and stopped by the spring link mechanism of the regenerative mechanism, and the inertia moment of the weight-side support material 41 This time, the rotation direction of the pair of weights 14.15 is set to the rotation direction away from each other in the opposite rotation direction. At the same time, the energy of the inertia moment of the weight side support member 41 is Released in cooperation By controlling the rotation at the same rear 40, the moving body including the pair of weights 14.15 having the regenerative mechanism and rotating reversely as described above is also more than the backward movement distance. Move forward.

FIG.

FIG. 10 shows a battery 6 installed in a moving body, instead of a pair of weights 14.15 provided on one side of a support material 12 fixed to a hollow shaft 33 provided with a hollow in the main shaft 9. In the installed top view, it is a schematic diagram in which at least two conductors 35 are led from each terminal of the capacitor 6 to the hollow shaft 33;

FIG.

FIG. 11 is a side view of the battery 6 of the support material 12.13. Instead of the weight 14.15, the shape of the battery 6 installed on the moving body is replaced with the shape of the upper and lower support materials 12.15. In the case of the storage battery 6 installed on the upper support member 12, the current collecting method from the respective storage batteries 6 installed in place of the weights 14 and 15 in FIG. A slip ring 36 is provided in the hollow shaft 33 at the lower part of the propulsion device 2 through the hollow of the hollow shaft 33, the conductive wire 35 is bonded to the slip ring 36 and collected by the brush 37, and the conductive wire 35 from the brush 37 is controlled. Sent to machine 17. The method of collecting current from the storage battery 6 fixed to the lower support member 13 is to provide a slip ring 36 on the flange 8a fixed to the upper bevel gear 10 with the conductive wire 35, and to fix the conductive wire 35 to the slip ring 36. The current is collected at 37 and the conductive wire 35 is sent to the controller 17.

When the present invention is used in the structure as described above, the propulsion device 2 in which the capacitor 6 is substituted for the pair of weights 14.15 which are not shown in the figure but rotate reversely to each other is connected to the linear of the reciprocating linear motion mechanism. It is installed in the motor 18 and linear guide 21, used in inertial space and on the ground moving body, and can be combined with the spring-link mechanism of the regenerative mechanism.

The reciprocating propulsion device of the present invention can be manufactured by conventional techniques, and can be used by installing a propulsion device and a reciprocating linear motion mechanism on a spacecraft in an inertial space or a moving body such as an artificial satellite. . Vehicles on the ground under gravity are considered to be effective for scientific development and education for toys and exhibits.

Side view of a reciprocating propulsion vehicle vehicle having a coaxial reversing mechanism Top view of a reciprocating propulsion vehicle with a coaxial reversing mechanism Correlation diagram showing (1) to (6) the movement of the vehicle of a pair of weights and a moving body that rotate reversely to each other Side view of vehicle with linear guide for reciprocating linear motion mechanism Correlation diagram showing the movement of the vehicle 1 provided with a pair of weights 14.15 and linear guides rotating in reverse with each other Perspective view of an artificial satellite with a linear motor with a reciprocating linear motion mechanism A diagram in which each pair of weights is rotated in the reverse direction. Top view of spring-link mechanism of regenerative mechanism Side view of spring-link mechanism of regenerative mechanism Top view with a storage capacitor instead of a weight on the support material Side view of the propulsion unit support with a capacitor instead of a pair of weights

Explanation of symbols

DESCRIPTION OF SYMBOLS 1 Vehicle 2 Propulsion device 3 Electric motor 4 Reduction gear 5 Drive bevel gear 6 Capacitor 7 Coaxial reversing mechanism 8a Upper flange 8b Lower flange 9 Main shaft 10 Upper bevel gear 11 Lower bevel gear 12 Upper support material 13 Lower support material 14 Upper weight 15 Lower Weight 16 Controller 17 Receiver 18 Linear motor 19 Linear motor operating part 20 Linear motor base 21 Linear guide 22 Linear guide operating part 23 Linear guide base 24 Stop holding device 25 Buffer 26 Artificial satellite or flying object 27 Support member 28 Solar cell 29 Electric motor 30 Electric motor 31 Earth 32 Spring 33 Hollow shaft 34 Joint shaft 35 Conductor wire 36 Slip ring 37 Brush 38 Hard tire 39 Front 40 Rear

Claims (4)

A pair of oppositely rotating shafts driven by driving means, and one of support members oriented in a direction perpendicular to the axial direction of each axis are fixed to the upper ends of the pair of axes, and vertically A propulsion device configured with a pair of counterweights that rotate counterclockwise each having a weight fixed to the other of the respective supporting members, and a pair of weights that rotate counterclockwise in a moving body provided with the propulsion device. A reciprocating propulsion moving main body characterized in that when the weight is in the rear, the moving body provided with the propulsion device is moved backward by controlling the rotation and propelled forward more than the retraction distance. 2. A reciprocating propulsion moving body according to claim 1, wherein the reciprocating linear motion mechanism is provided with the propulsion device, and the movable body is provided with the reciprocating linear motion mechanism. A pair of weights provided in a rotational direction moving away from each other by the cooperation of the driving means and the regenerative mechanism when the position of the pair of weights rotating in the reverse direction is behind and in the rotational direction approaching each other The reciprocating type propulsion moving body according to claim 1 characterized by the above-mentioned. 2. A reciprocating propulsion moving main body according to claim 1, wherein a pair of accumulators rotating in opposite directions are used instead of the weights.

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