KR20040081934A - An inner propulsion method and inner propulsion apparatus of a closed system using the coriolis force generating in the closed system of a doughnut shape - Google Patents

Abstract

The present invention relates to a method and apparatus for generating a Coriolis force by rotation of mass inside a closed system in the form of a donut and moving the closed system to the Coriolis force.

The internal propulsion method of the closed system by the Coriolis force according to the present invention

A body preparation step having an outer shape of a donut and providing a body in which a path is communicated in a closed state with a space formed therein; A core mass positioning step of placing a core mass having a constant radius on one side of the path of the body; RCM forming step of positioning the virtual RCM at a position eccentric distance from the geometric center of the body; Placing a core mass accelerating means on the outside of the body within a range of 180 degrees with respect to the vertical line passing through the center of the body to impart a constant acceleration to the core mass; Placing a core mass deceleration means on the outside of the body within a range of 180 degrees to 360 degrees with respect to the line segment passing through the center of the body to impart a constant acceleration to the core mass; And moving the core mass along a path of the body and increasing a radius from the RCM to generate a Coriolis force on the core mass.

An internal propulsion device for a closed system by a Coriolis force according to the present invention includes an outer shape of a donut and a body having a path connected to each other on an inner cross section; A core mass having a radius of a certain distance from a virtual RCM located at a distance from a geometric center of the body and positioned on a cross-sectional path of the body; Core mass acceleration means disposed outside the body to impart a constant acceleration to the core mass within a range of 180 degrees with respect to the vertical line passing through the center of the body; It includes; core mass reduction means disposed on the outside of the body to give a constant deceleration to the core mass in the range of 180 degrees to 360 degrees with respect to the vertical line passing through the center of the body.

According to the present invention, it is possible to generate a non-inertial Coriolis force inside the closed system without applying an external force to move the closed system.

Description

Internal propulsion method of the closed system by the Coriolis force generated inside the donut type closed system and the internal propulsion system }

The present invention relates to a method and apparatus for generating a Coriolis force by rotation of mass inside a closed system in the form of a donut and moving the closed system to the Coriolis force.

Where Coriolis force ( ) Refers to the total geometric center (TCM) of the mass on the inertial coordinate system as it rotates as the mass (M1, M2) is accelerated or decelerated by a certain distance (r) away from the geometric center (CM) as observed in the rotational coordinate system. Say the power to.

Applicant has disclosed Korean Patent Publication No. 2002-0090926 (Name: A method for generating a non-inertial Coriolis force in a closed system and an internal propulsion method using the Coriolis force) as a prior art related to an internal propulsion device of a closed system. It has been disclosed.

In the case of the patent invention, since the closed system has a spherical or cylindrical shape, there is a limit in generating a Coriolis force of a desired size, and there is a problem in that it is difficult to control the generated Coriolis force.

In addition, in the case of the patent invention, a power motor is used to rotate the core mass, and in order to increase the Coriolis force, the power motor must be rotated at an extremely high speed (for example, 200,000 rpm or more). There is a limitation in manufacturing such a high speed motor.

In addition, in the case of the patent invention, since the restraining means such as a string or a guide is required to allow the core mass to rotate along a constant track, the structure is complicated or mechanical friction or noise occurs.

In addition, in the case of the patent invention, the structure for changing the direction of the internal propulsion device is complicated or has to use a separate direction control motor.

An object of the present invention is to provide a desirable body shape for the core mass to move along a constant trajectory by generating a Coriolis force by causing the core mass to rotate along the inner passage of the body having a donut shape.

Another object of the present invention is to provide an acceleration and deceleration providing means of a structure most suitable for rotating at high speed while accelerating or decelerating a core mass along an inner passage of a body having a donut shape.

Still another object of the present invention is to provide a redirection device having a structure that can easily change the forward and backward direction of a closed system.

Still another object of the present invention is to provide an internal propulsion apparatus capable of generating a non-inertial Coriolis force inside the body to make the closed system non-inertial linear movement and to stop the closed system momentarily as needed.

Still another object of the present invention is to provide an internal propulsion device for a closed system that can operate without a wheel or without ejecting mass to the outside by generating a non-inertial Coriolis force inside the closed system.

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1 is a cross-sectional view of a structure modeling the internal propulsion system of the closed system according to the present invention.

Figure 2 is a plan view showing a schematic structure of a core mass according to the present invention.

3 is a cross-sectional view of the body according to the present invention taken along an imaginary line.

Figure 4 is a functional diagram showing the relationship between the rotation angle and Coriolis force of the core mass according to the present invention.

5 is a functional diagram showing the relationship between the rotation angle and the momentum of the core mass according to the present invention.

Figure 6 is a cross-sectional view showing an embodiment of the internal propulsion device of the closed system according to the present invention.

Figure 7 is a cross-sectional view showing an embodiment of the internal propulsion device of the closed system according to the present invention.

Figure 8 is a cross-sectional view showing an embodiment of the internal propulsion device of the closed system according to the present invention.

* Explanation of symbols for the main parts of the drawings

Reference Signs List 10 body 12 geometric center 14, 18 RCM (rotational mass center) 16 virtual line 20 center line 22 core mass acceleration means 24 core mass reduction means 26 initial velocity provision means 28 collision avoidance means 30 movement Path sensor

The internal propulsion method of the closed system by the Coriolis force according to the present invention

A body preparation step having an outer shape of a donut and providing a body in which a path is communicated in a closed state with a space formed therein; A core mass positioning step of placing a core mass having a constant radius on one side of the path of the body; RCM forming step of positioning the virtual RCM at a position eccentric distance from the geometric center of the body; Placing a core mass accelerating means on the outside of the body within a range of 180 degrees with respect to the vertical line passing through the center of the body to impart a constant acceleration to the core mass; Placing a core mass deceleration means on the outside of the body within a range of 180 degrees to 360 degrees with respect to the line segment passing through the center of the body to impart a constant acceleration to the core mass; And moving the core mass along a path of the body and increasing a radius from the RCM to generate a Coriolis force on the core mass.

The present invention preferably further comprises the step of rotating the core mass at a constant speed with respect to the geometric center of the body following the core mass positioning step.

An internal propulsion device for a closed system by a Coriolis force according to the present invention includes an outer shape of a donut and a body having a path connected to each other on an inner cross section; A core mass having a radius of a certain distance from the RCM located at a distance from the geometric center of the body and positioned on a cross-sectional path of the body; Core mass acceleration means disposed outside the body to impart a constant acceleration to the core mass within a range of 180 degrees with respect to the vertical line passing through the center of the body; It includes; core mass reduction means disposed on the outside of the body to give a constant deceleration to the core mass in the range of 180 degrees to 360 degrees with respect to the vertical line passing through the center of the body.

The core mass accelerating means is a coil wound in parallel to an imaginary line passing through the RCM.

The core mass reduction means is a coil wound in parallel to an imaginary line passing through the RCM.

The core mass accelerating means and the core mass reduction means are located outside the body, are disposed in parallel to the imaginary line passing through the RCM, the S pole on one side, the N pole on the other side is characterized in that the magnet is arranged.

The magnet is characterized in that the permanent magnet.

The magnet is characterized in that the electromagnet.

The core mass is characterized in that the magnetic body.

The core mass is characterized in that the rigid body.

The core mass has a sphere shape, an S pole is formed at the center of the sphere, and an N pole is formed at the surface of the sphere.

It is characterized by installing a plurality of core mass, core mass acceleration means and core mass reduction means within the range that can be installed evenly spaced at the same angle radially around the RCM.

In addition, the present invention preferably further comprises an initial speed imparting means disposed in the outer side of the body in parallel with the imaginary line passing through the geometric center of the body to rotate the core mass at a constant speed.

The initial speed imparting means is a coil wound in parallel to an imaginary line passing through the geometric center of the body.

In addition, the present invention preferably further comprises an anti-collision means arranged on the inner outer wall of the body so that the core mass does not collide with the inner wall surface of the body and moves on the space of the body.

The anti-collision means is characterized in that the electromagnet.

In addition, the present invention is disposed through the body, it is preferable to further include a movement path detection sensor installed in the width direction in the path of the body to detect the movement path of the core mass.

The movement path detecting sensor is an optical sensor.

In addition, the present invention is characterized in that the path of the body is a circle.

The path of the body is characterized in that the ellipse.

Hereinafter, with reference to the exemplary drawings will be described in detail a preferred embodiment of the present invention.

1 is a cross-sectional view of the structure modeling the internal propulsion system of the closed system according to the present invention, Figure 2 is a plan view showing a schematic structure of the core mass according to the present invention, Figure 3 is a body according to the present invention in a virtual line Figure 4 is a cross-sectional view taken along, Figure 4 is a functional diagram showing the relationship between the rotation angle of the core mass and the Coriolis force, Figure 5 is a functional diagram showing the relationship between the rotation angle and the momentum of the core mass according to the present invention 6 to 8 are cross-sectional views showing an embodiment of the internal propulsion device of the closed system according to the present invention.

Referring to Figure 1, the core mass ( To It is preferable to arrange a large number of) so that the Coriolis force generated can be increased, but the core mass is preferable for the convenience of analysis and explanation of the force acting on the core mass. Assume that they are only deployed.

The donut-shaped body 10 is provided, and when looking at the cross section of the body 10, a space is formed inside the core mass ( ) Has a path through which it can rotate.

The path is shown circularly in FIG. 1, but the core mass passing through the path ( ) Does not collide with the wall surface of the body 10, and in order to rotate smoothly, it is more preferable that the y-axis has an ellipse formed longer than the x-axis.

The geometric center 12 of the body 10 is in the center and passes through a rotational center of mass (RCM) 14 at a position eccentrically away from the geometric center 12 of the body 10 ( Assume 16).

Core mass in the vertical direction on the cross-sectional path of the body 10 through which the virtual line 16 passes ( ). Core mass at a predetermined distance from the geometric center 12 of the body 10 The core mass (RCM) by means of the core mass acceleration means 22 in a direction perpendicular to the imaginary line 16 passing through the RCM 14 so that the rotational center of mass (RCM; ) To give acceleration.

As shown in Figure 1, the core mass ( Core mass acceleration means 22 is installed outside the body 10 on the sectional path through which the imaginary line 16 passes in order for the c) to rotate on the path of the body 10 at a constant acceleration.

The core mass acceleration means 22 is preferably a coil wound in parallel to the imaginary line 16 passing through the RCM 14, and the symmetrical line of the imaginary line 16 is provided at one side of the S pole and the other side. It is arrange | positioned with the north pole. Of course, the angular velocity providing means may be a permanent magnet or an electromagnet.

The core mass ( As shown in Figs. 2 and 3, the shape of the sphere is S, the S pole is formed in the center of the sphere, and the N pole is formed on the surface of the sphere. Of course, the opposite can be done.

In addition, the core mass ( ) May be magnetic or rigid.

The core mass ( ) Is rotated at a constant angular velocity on the inner cross-sectional path of the body 10 by the core mass acceleration means 22 and the core mass reduction means 24 based on the RCM 14. Core mass ( Distance from the RCM 14 while rotating 1 < th > on the cross-sectional path of the body 10, 180 degrees to the right of the y-axis. Is increasing, so the above core mass ( Linear velocity Must continue to grow and accelerate, and conversely, the distance from the RCM 14 while rotating 180 degrees to the left of the y-axis. Continues to shrink, so the core mass ( Linear velocity Should continue to decrease and decelerate.

Therefore, the core mass ( Core mass deceleration means 24 outside the body 10 on the cross-sectional path through which the imaginary line 16 passes in order to rotate at a constant angular velocity with respect to the RCM 14 while rotating 180 degrees to the left of the y-axis. Should be installed.

As above, the core mass ( ) And RCM (14) alternately with Coriolis force ( ) Works, the Coriolis force ( ) Act in the opposite direction and cancel each other out, but due to parallax, the momentum appears, and the momentum appears and disappears every minute, and the core mass ( ) Will vary depending on the rotation angle.

The core mass, the core mass acceleration means and the core mass reduction means may be in various forms, unlike the structure described above.

For example, the core mass may be a fluid or powder, but may be a semiconductor, a conductor or an insulator among the fluids or powders, and the core mass of the fluid or powder is pumped with a pump to impart pressure and velocity. Acceleration and deceleration can also be given to them.

Moreover, the said core mass may be made into gas, and acceleration and deceleration may be given to a fan with respect to the said core mass made of gas.

In addition, the core mass may be made of particles such as electrons or protons, and acceleration and deceleration may be imparted to an electromagnetic field with respect to the core mass of the particles.

The Coriolis force ( The motion based on the amount of momentum generated by) can be defined as a closed motion, and the core mass ( Referring to the concept of the Coriolis force and the closed motion generated during the first rotation on the cross-sectional path of the body 10 as follows.

5 and 6, the core mass ( )this Is constant, Under these increasing conditions When rotated by an angle, its core mass ( Coriolis power appearing in) In this case, the Coriolis force acting in the + Y axis direction You can say that power If you integrate until

Become, Up to an angle Is generated, the core mass ( ) Rotates the path of the body 10 once Is generated,

Becomes

By expressing the Coriolis force again as a function of time, the Coriolis forces acting in opposite directions to each other , if,

Becomes In other words

= Becomes

In the above, the core mass ( ) Is described as rotating about the RCM 14, but there may be a problem that the starting load is too large initially.

Therefore, as shown in Fig. 6, first, the core mass ( ) The core mass () by the initial speed imparting means 26 relative to the geometric center 12 of the body 10 so as to rotate with sufficient speed in the storage. Rotate).

In this case, since the preservation field is formed and the centrifugal force and the centripetal force cancel each other, no force acts on the body 10, but the core mass ( ) Is ready to rotate with sufficient speed.

The initial speed providing means 26 is preferably disposed outside the body 10 and is a coil wound in parallel with an imaginary line passing through the geometric center 12 of the body 10.

Of course, the number of installation of the initial speed providing means 26 is not limited, it is preferable to select the enemy in consideration of the convenience of control within the range that can be installed in the internal propulsion device of the present invention.

In Figure 1 the core mass ( 6), but as shown in FIGS. 6 to 8, several core masses (3) are spaced at the same angle radially with respect to the RCM (14). ), The core mass acceleration means 22 and the core mass reduction means 24 can increase the generated Coriolis force by that much.

Of course, the core mass ( ) And the number of the core mass acceleration means 22 and the core mass reduction means 24 are not limited, and it is preferable to select the enemy in consideration of the convenience of control within the range that can be installed in the internal propulsion device of the present invention. Do.

In addition, as shown in Figure 7, the core mass ( It is preferable that the collision prevention means 28 is installed on the inner outer wall of the body 10 so that they do not collide with the inner wall of the body 10 and can smoothly move on the cross-sectional path.

Preferably, the collision preventing means 28 is a coil or an electromagnet, and the movement path detecting sensor 30 is disposed through the body 10 in a radial direction on the cross-sectional path of the body 10, thereby providing the core mass. Sensing the path in which they move from time to time to control the collision avoidance means 28 to always adjust the core mass to pass through the central path of the body (10).

The movement path detection sensor 30 may be used a variety of sensors, preferably an optical sensor.

Referring to FIG. 8, it is represented in FIG. 8 that there is another RCM 18 that was not present in the above embodiment.

Based on the RCM (18) the core mass ( ) The core mass at a position eccentrically away from the geometric center 12 of the body 10 to rotate with acceleration and deceleration. So that the center of rotational mass (RCM; 18) is

The core mass (by the core mass acceleration means 22 in the direction perpendicular to the imaginary line 16 passing through the RCM 18) When the acceleration force is given to the cores, the core mass ( Are rotated relative to the RCM 18, and the core mass acceleration means 22, the core mass reduction means 24, and the RCM are in the same shape as when the number 14 is used.

As described above, when the rotational center of mass of the RCM 14 is changed to the RCM 18, the body 10 moving in the + Y-axis direction moves by changing the moving direction in the -Y-axis direction.

Similarly, with respect to any one of the RCM (14) (18) the core mass ( While moving the body 10 while rotating the core mass ( ) Rotated around the geometric center 12, the closure system returns to the storage and immediately stops in place.

The present invention can be used in satellites, space ships, space stations, personal lifeboats in space, wheelless toys, wheelless conveyors and mobile devices in factories, and can be precisely moved in aircraft, ships, submarines and human bodies. It can be used as a propulsion device for moving capsules and has a wide range of applications, such as being applicable to brake systems in automobiles, aircrafts, and ships.

Although the embodiments of the present invention have been described in detail as described above, the scope of the present invention is not limited thereto, and common knowledge in the technical field to which the present invention pertains without departing from the gist of the present invention claimed in the claims. Those having a variety of modifications can be made, of course, such modifications are within the scope of the claims described as the core elements of the present invention, even those that are substantially equivalent to one embodiment of the present invention The scope of the design extends.

According to the present invention, since the core mass can be rotated along the inner path of the body having a donut shape, an effect of providing a body of a preferred shape for linearly moving the closed system by the Coriolis force is obtained.

In addition, according to the present invention, it is possible to efficiently increase the non-inertial Coriolis force while rotating at a very high speed while accelerating and decelerating the core mass, thereby providing a powerful internal propulsion device.

In addition, according to the present invention, since the RCM can be easily changed, an effect of providing an internal propulsion apparatus having a structure capable of easily changing the forward and backward direction of the closed system is obtained.

In addition, according to the present invention, the internal propulsion apparatus that can stop the closed system instantaneously because it can generate a non-inertial Coriolis force inside the body to make a non-inertial linear motion and change the storage system as needed, if necessary The effects that can be provided.

In addition, according to the present invention, by generating a non-inertial Coriolis force in the interior of the closed system, there is an effect that can provide an internal propulsion device of the closed system that can operate without the wheel or the injection of mass to the outside.

Claims (29)

A body preparation step having an outer shape of a donut and providing a body in which a path is communicated in a closed state with a space formed therein; A core mass positioning step of positioning a core mass having a constant radius from a geometric center of the body on one side of a path of the body; RCM forming step of positioning the virtual RCM at a position eccentric distance from the geometric center of the body; Placing a core mass accelerating means on the outside of the body within a range of 180 degrees with respect to the vertical line passing through the center of the body to impart a constant acceleration to the core mass; Placing a core mass deceleration means on the outside of the body within a range of 180 degrees to 360 degrees with respect to the line segment passing through the center of the body to impart a constant acceleration to the core mass; The core mass moves along the path of the body and the radius from the RCM is increased to generate a Coriolis force on the core mass; Internal propulsion method of the closed system by the Coriolis force generated in the closed system of the donut type including . The method of claim 1, And a step of rotating the core mass at a constant speed based on the geometric center of the body following the core mass position step. A body having an outer shape of a donut and having a path connected to each other on an inner cross section; A core mass having a radius of a certain distance from the RCM located at a distance from the geometric center of the body and positioned on a cross-sectional path of the body; Core mass acceleration means disposed outside the body to impart a constant acceleration to the core mass within a range of 180 degrees with respect to the vertical line passing through the center of the body; A donut-shaped donut type including a core mass deceleration means disposed outside the body to impart a constant deceleration to the core mass within a range of 180 degrees to 360 degrees with respect to a vertical line passing through the center of the body. Internal propulsion system of closed system by Coriolis force generated inside closed system. The method of claim 3, The core mass acceleration means is a coil wound in parallel to an imaginary line passing through the RCM internal propulsion device of the closed system by a Coriolis force generated inside the closed system of the donut type. The method of claim 3, The core mass reduction means is an internal propulsion device of the closed system by the Coriolis force generated inside the closed system of the donut type, characterized in that the coil wound in parallel to the virtual line passing through the RCM. The method of claim 3, The core mass acceleration means and the core mass reduction means are located on the outside of the body, disposed in parallel to the imaginary line passing through the RCM, the S pole on one side, the N pole on the other side is characterized in that the donut Internal propulsion system of closed system by Coriolis force generated inside closed system of type. The method of claim 6, The magnet is a permanent magnet, the internal propulsion system of the closed system by the Coriolis force generated in the closed system of the donut type, characterized in that the permanent magnet. The method of claim 6, The magnet is an electromagnet, the internal propulsion system of the closed system by the Coriolis force generated in the closed system of the donut type, characterized in that the electromagnet. The method of claim 3, The core mass is an internal propulsion device of the closed system by the Coriolis force generated inside the closed system of the donut type, characterized in that the magnetic body. The method of claim 9, The internal propulsion device of the closed system by the Coriolis force generated inside the closed system of the donut type, characterized in that the magnetic body is a fluid. The method of claim 9, The internal propulsion device of the closed system by the Coriolis force generated in the closed system of the donut type, characterized in that the magnetic material is powder. The method of claim 9, The internal propulsion device of the closed system by the Coriolis force generated inside the closed system of the donut type, characterized in that the magnetic body is a rigid body. The method of claim 12, The rigid body is in the form of a sphere, the S pole is formed in the center of the sphere, the N pole is formed on the surface of the sphere, the internal propulsion system of the closed system by the Coriolis force generated inside the donut-shaped closed system. The method of claim 3, Occurs in the donut-type closed system, characterized in that a plurality of core masses, core mass acceleration means and core mass reduction means are installed within the range that can be installed evenly with the same angle spaced radially around the RCM. Internal propulsion system of closed system by Coriolis force. The method of claim 3, The interior of the closed system by the Coriolis force generated in the closed system of the donut type further comprising an initial speed imparting means disposed on the outside of the body in parallel with the imaginary line passing through the geometric center of the body to rotate the core mass at a constant speed Propulsion system. The method of claim 15, The initial speed imparting means is an internal propulsion device of the closed system by the Coriolis force generated in the closed system of the donut type, characterized in that the coil wound in parallel to the imaginary line passing through the geometric center of the body. The method of claim 3, The core mass is disposed on an inner outer wall of the body, and the core mass does not collide with the inner wall surface of the body. Internal propulsion system of closed system. The method of claim 17, The anti-collision means is an internal propulsion device of the closed system by the Coriolis force generated inside the closed system of the donut type, characterized in that the electromagnet. The method of claim 3, It is disposed through the body, a plurality of installed in the width direction in the path of the body closed system by the Coriolis force generated in the closed system of the donut type further comprising a movement path sensor for sensing the movement path of the core mass Internal propulsion unit. The method of claim 19, The movement path sensor is an optical propulsion device of the closed system by the Coriolis force generated inside the closed system of the donut type, characterized in that the optical sensor The method of claim 3, Internal propulsion device of the closed system by the Coriolis force generated inside the closed system of the donut type, characterized in that the path of the body is a round The method of claim 3, The propulsion system of the closed system by the Coriolis force generated inside the closed system of the donut type, characterized in that the path of the body is an ellipse. The method of claim 3, The core mass is a semiconductor as a fluid, and the core mass acceleration means and the core mass reduction means are pumps installed inside the body, the internal propulsion system of the closed system by the Coriolis force generated in the closed system of the donut type. The method of claim 3, The core mass is a conductor as a fluid, the core mass acceleration means and the core mass reduction means is a pump installed inside the body of the propulsion system of the closed system by the Coriolis force generated in the closed system of the donut type. The method of claim 3, The core mass is a non-conductor as a fluid, and the core mass acceleration means and the core mass reduction means are pumps installed inside the body, the internal propulsion device of the closed system by the Coriolis force generated in the closed system of the donut type. The method of claim 3, The core mass is a semiconductor as a powder, and the core mass acceleration means and the core mass reduction means are pumps installed inside the body, the internal propulsion system of the closed system by the Coriolis force generated in the closed system of the donut type. The method of claim 3, The core mass is a gas, the core mass acceleration means and the core mass reduction means is an internal propulsion device of the closed system by the Coriolis force generated inside the donut-type closed system, characterized in that the fan installed inside the body. The method of claim 3, The core mass is electrons as particles, and the core mass acceleration means and the core mass reduction means are electromagnetic propulsion means installed on the outside of the body, and the internal propulsion of the closed system by the Coriolis force generated in the closed system of the donut type. Device. The method of claim 3, The core mass is a positron as particles, and the core mass acceleration means and the core mass reduction means are electromagnetic propulsion means installed on the outside of the body, the internal propulsion of the closed system by the Coriolis force generated in the closed system of the donut type Device.