JPS59577A - Inertia propelled engine and inertia motor - Google Patents

Abstract

PURPOSE:To produce a propelling force, by causing movement of a weight disposed in a radial space of a rotating system which produces such an inertial oscillation that the angular velocity is minimum at the central part of the rotating system and maximum at the outer side. CONSTITUTION:When a rotor 4 is turned with application of an input rotation omega0, an elliptic gear 2 and a bevel gear 8 attached to the rotor 4 are turned once together by a bevel gear 7 fixed to a stationary system 6. Resultantly, two elliptic gears 3 are turned once at unequal speed respectively in the directions shown by arrows in the drawing, and a weight 1 is made to cause circular motion also at an unequal speed by the rotation of the elliptic gears 3. At the position where all of the six focal points of the three elliptic gears are located straight, the angular velocity of the weight 1 becomes maximum (omega2) and minimum (omega1), and a propelling force is produced in the direction of omega2. In the above arrangement, the direction of the propelling force is changed by altering the phase of the bevel gear 7 fixed to the stationary system 6.

Description

DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an inertial propulsion engine that generates propulsive force based on the concept of deflecting centrifugal force, and an inertial motor that obtains rotational force thereby.

The purpose is also to obtain power.

First, to explain the principle of an inertial propulsion engine, Fig. 1 shows the mass m
A difference in centrifugal force is generated in the y-axis direction by a non-uniform circular motion in which the mass point P of The change in causes a reaction f, and this rotating system becomes dynamically balanced.

The basic concept of the present invention is to utilize centrifugal force again as a means to eliminate the reaction f at this time.

First, in Figure 1, the non-uniform circular motion of the mass point P in the χ-y coordinate is represented by
If we define inertial vibration as the vibration where the minimum angular velocity and maximum angular velocity are at both ends when viewed from the axial direction, the X-Y
A straight line 0-.centered on the coordinate origin 0. 31 is ω. When the mass point P rotates at the origin 0 on o-y, the minimum angular velocity ω
1, and when inertial vibration always has a maximum angular velocity ω2 at a fixed point Q on the Y-axis, the mass point P often draws a constant elliptical orbit as shown in the figure. In this case, it rotates at the period T of inertial vibration. Match the period of motion, ω. -2π/T.

Analyzing the change in momentum of mass point P on this orbit, we get
IJ in the figure = R, ω. Changes in momentum are canceled out after one revolution and become irrelevant, and the mass point has the maximum velocity mainly because it receives acceleration due to the centrifugal force mRxω: due to vl.

Therefore, since the momentum is maximized without any reaction, the centrifugal force is deflected in the direction from the origin O to the fixed point Q, and the propulsive force indicated by the arrow F can be generated.

In this way, the technical idea of the present invention is to rotate the inertial vibration of the mass point P at a fixed period so that the time when the angular velocity is the minimum is at the center, and when the angular velocity is the maximum, it always passes through a fixed point on the outside. It is.

Therefore, the inertial vibration is not only due to non-uniform circular motion in a plane perpendicular to the X-Y plane passing through the origin 0 as shown in Figure 2, but also due to non-uniform circular motion within the X-Y plane. O- due to exercise
Inertial vibration appearing on y is also within the scope of the technical idea of the present invention.

Furthermore, without worrying about the X-Y plane, by using a conversion mechanism that converts non-uniform circular motion into reciprocating linear motion, Kokichi, which moves the mass point P in reciprocating linear motion on o-y, is exactly inertial vibration itself,
It is the basis of technical thought.

Furthermore, the period of inertial vibration and the rotation period of the rotating system may be the same, and if there is a large difference in the angular velocity of inertial imaging, the rotating system may be rotated twice during one cycle. Also, ω2 passes through the fixed point Q.

The best mode for implementation is as shown in FIGS. 3 and 4, in which there is a rotor 4 supported by a stationary system 6 and its shaft 5,
Input rotation ω. When the rotor 4 rotates once with full force, the cap gear 7 fixed to the stationary system 6 activates the cap gear 8 on the rotor 4.
The structure is such that both the elliptical gear 2 and the elliptical gear 2 rotate once, and therefore, the two elliptical gears 3 each rotate once in the direction of the arrow at non-uniform speeds, and in conjunction with the elliptical gears 3, the weight 1 and each rotate non-uniformly. It is a mechanism that performs fast circular motion. Here, when the six focal points of each elliptical gear are all in series, the angular velocity of the weight l becomes maximum ω2 and minimum ω1, respectively, and the direction in which the maximum ω2 is achieved is the direction of the propulsive force. And the cap gear 7 fixed to the stationary system 6
It is natural that changing the 0 phase will change the direction of the propulsive force. The reason why two elliptical gears 3 are used in the rotor 4 and a plurality of weights 1 are used is to suppress vibration during rotation.

In reality, two or more of these inertial propulsion engines are arranged in parallel to cancel out unnecessary vibrations.

By the way, the non-uniform circular motion required for the present invention is made by meshing two or more elliptical gears of the same size. You can also do it. If there are three or more gears, reduce the weight of the gears and increase the final gear spacing.

Next, we will explain the principle of an inertial motor.

The above-mentioned inertial propulsion engines are usually two inertial propulsion engines, installed in the second rotation system, and arranged so that they are linked to generate a couple by the propulsive force, or have a complete structure that provides input rotation to the inertial propulsion engines. As long as the input rotation is applied, power can be obtained continuously.

The structure of the inertial propulsion engine capable of rotating 1lIi will be explained schematically in Figs. 5 to 8.
An inertial propulsion engine 12 is arranged on a disc 9 serving as a second rotating system in a direction that generates a couple by its propulsive force, and a gear IIi is rotated by a gear 10K coupled to a shaft 20, which inertial propulsion engine 12 (1) Fig. 5 shows a structure in which the electric motor 13 that drives the shaft 20 is fixed to the disk 9, and is supported by a stationary system so that it rotates as one. It is used to supply electricity. By controlling the rotation speed of the electric motor 130, the output rotational force can be adjusted.

(2) Figure 6 shows the above (moon electric motor 13 installed in a stationary system).

The structure is such that the rotation is given by gear 10 VC. Said (
1) Similarly, the rotational force of the inertial motor can be controlled by the rotational speed of the electric motor I3.

(3) In FIG. 7, the return gear consisting of the gear 16 and the gear 17 is in a stationary system by the shaft 19, and the gear 18, which is integral with the disk 9 and the gear 15, is connected to the shaft 20. The output rotation speed of the disc 9 can be increased or decreased and then directly returned to the gear 10. This inertial motor will stop by cutting off the communication via the return gear as shown by the arrow.

(4) Fig. 8 shows a structure in which the gear 10 for rotating the gear 11 is fixed to a stationary system by the entire shaft 20, and when the disk 9 rotates, the gear 11 automatically rotates.
Corresponds to the limit in the case of deceleration return in 3), and gear 10
is a stationary system and a feedback gear.

By keeping the gear 10 in a semi-fixed state, it is possible to fully control the output rotational force, and by releasing it freely, the inertia motor will stop.

(5) Fig. 9 has the same concept as (4) above, but the difference is that the gear 10 is an internal gear fixed to a stationary system, and the disc 9 rotates coupled to the shaft 20 Vc. Said (4
) has a similar effect.

The concept common to the above embodiments is that the gear 1 has no orientation with respect to the disk 9! As long as they rotate relative to each other in relation to each other, each inertial propulsion engine 12 (lj: works) and generates rotational force in the disk 9.

The best form of implementing an inertial motor is shown in Figures 10 to 1.
Shown in Figure 2.

The outline is that when the diameter of the moving circle is half the diameter of the fixed circle,
Embodied by combining an inertial propulsion engine with a mechanism that converts non-uniform circular motion into inertial vibration by utilizing the fact that the locus of the endocycloid becomes a straight line, and the embodiment shown in FIG. 9 in (5) above. This is what I did.

First, since it is the concept of (5) above, when the disc 9 rotates in the internal gear 10 fixed to a stationary system, the disc 24 is rotated by the gear 11, and the inertial propulsion engine is operated, and the disc 9 is rotated. Rotation is a self-replicating structure.

Next, an elliptical gear 23 is mounted on the disc 24 so that the elliptical gear 22 fixed to the disc 9 can be shifted with a radius R, and the focus of each elliptical gear is in series on line A-A in FIG. The gears are meshed in a phase in which the full propulsive force is generated in the direction of arrow F, and the internal gear 25 is fixed using a spacer 27 to secure the space occupied by the elliptical gear 22.

The gear 26, whose pitch circle has half the diameter of the internal gear 25, rotates on the elliptical gear 23 with the weight 21 attached eccentrically, and then rolls inside the internal gear 25. When it comes to line A-A, it is meshed so that it is in series with each oval gear including the weight 21 as shown in the figure.

When the disc 24 rotates by this mechanism and the elliptical gear 23 performs a non-uniform circular motion, the center of the weight 21 on the gear 26 moves approximately linearly in a reciprocating manner within the internal gear 25 while the disc 24 moves non-uniformly.
It will rotate with 4.

However, if the center of the weight 2I is on the pitch of the gear 26, it will be a complete linear motion and will be a complete inertial vibration. The reason why two sets of weights 21 and others are provided on the disc 24 is to completely suppress vibrations during rotation due to imbalance.

The output P of this inertial motor. Ignoring loss, P from the dimensions in the figure. -ωFD, where F is the propulsive force and the mass of the weight is fm, then F=KmRω:. Although the proportionality constant KU varies depending on various factors, it can be expected to be approximately 1.

Further, F can be adjusted by operating the control device 28 and adjusting the internal gear 10 to a semi-fixed state using the control input PC shown in FIG.

In the case of a high-output inertial motor, it is also possible to mount a small inertial motor and drive the inertial propulsion engine.

[Brief explanation of the drawing]

Figures 1 and 2 are diagrams explaining the principle of an inertial propulsion engine, Figure 3 is a front view of its embodiment, Figure 4 is a right side view of Figure 3, and Figures 5 to 9 are illustrations of an inertial motor. A schematic diagram illustrating the concept of the embodiment, FIG. 10 is a front view of the embodiment of the inertial motor, FIG. 11 is a sectional view taken along line A-A in FIG. 1O, and FIG. 12 is a right side view of FIG. Part of the BB cross section is enlarged. 21 Weight, 22.23 Oval gear, 24
Disc, 25 Internal gear, 26 Gear,
27 spacer 28 control device, 9
Disc, 10 Internal gear, 11 Gear, Y Figure 5 Figure 6

Claims (1)

[Claims] 1. When the non-uniform circular motion of an object whose minimum angular velocity reaches a maximum during half a revolution and returns to a minimum after another half revolution, the minimum angular velocity and the maximum angular velocity are determined when viewed from the direction of its rotating surface. If we define the vibrations at both ends as inertial vibrations, we can express inertial vibrations whose main axis is in the radial space of the rotating system, with the minimum angular velocity at the center of the rotating system and the maximum angular velocity at the outside. An inertial propulsion engine is a mechanism that rotates together with a rotating system with a writhing motion, and the period of inertial vibration is made to match an integral multiple of the rotational period of the rotating system. 2. The inertial propulsion engine according to claim 1, wherein the inertial vibration of the main body is due to non-uniform circular motion in a plane passing through the center of the rotating system and perpendicular to the rotating surface. 3. Claim 1 in which the inertial vibration of the main body becomes reciprocating linear motion on a straight line in the radial direction of the rotating system by using a conversion mechanism from non-uniform circular motion to reciprocating linear motion. Inertial propulsion engine as described in section. 4. Our inertial propulsion engine as set forth in claim 1, wherein the inertial vibration of the weight is due to non-uniform circular motion within the rotational plane of the rotating system. 5 When the non-uniform circular motion of an object whose minimum angular velocity reaches its maximum during half a revolution and returns to its minimum after another half revolution is viewed from the direction of its rotating surface, the vibrations with the minimum angular velocity and maximum angular velocity as both ends are particularly referred to as inertial vibrations. Defined as a mechanism in which a weight is located in the radial space of a rotating system and rotates with the rotating system with a movement that exhibits inertial vibration with the minimum angular velocity at the center of the rotating system and the maximum angular velocity at the outside. The structure is such that the inertial propulsion engine, which is an interlocking mechanism, is placed in the second rotating system to generate rotational force by matching the period of inertial vibration to an integral multiple of the rotational period of the rotating system, and the input to this inertial propulsion engine is An inertia motor with a structure that allows it to rotate. 6. The inertial motor according to claim 5, wherein the electric motor is fixed to the second rotating system and electric power is supplied from outside the system through a current collecting ring as a structure for providing input rotation to the inertial propulsion engine. 7. The inertial motor according to claim 5, wherein the electric motor is placed in a stationary system and a gear or other transmission mechanism is provided as a structure for providing input rotation to the inertial propulsion engine. 8. The inertial motor according to claim 5, wherein the inertial motor has a structure for providing input rotation to the inertial propulsion engine, and includes a feedback gear that converts output rotation of the second rotating system into input rotation again via a stationary system.