Anti-gravity propulsion device

JP2025051557A5Active Publication Date: 2025-07-04STUDIO SHION CO LTD
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Patent Information

Application Number
JP2023177116
Authority / Receiving Office
JP · JP
Patent Type
Applications
Current Assignee / Owner
Filing Date
2023-09-22
Publication Date
2025-07-04
Estimated Expiration
2043-09-22

AI Technical Summary

Technical Problem

Conventional propulsion devices interfere with the surrounding environment to generate recoil energy, making them unsuitable for noise-sensitive, heat-prone, or windy areas, and they are not ideal for attitude control in space.

Method used

An anti-gravity propulsion device that neutralizes part of the centrifugal gravity using homomorphous centrifugal bodies and ferromagnetic materials, allowing for quiet operation and minimal environmental influence, and can be used for attitude control in artificial satellites.

Benefits of technology

The device generates a strong upward thrust with minimal noise and environmental impact, enabling stable control of heavy objects from standstill to maximum output, suitable for various applications including space and rescue operations.

✦ Generated by Eureka AI based on patent content.

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Abstract

To provide an anti-gravity propulsion device which gets operation by invalidating a part of centrifugal gravity force.SOLUTION: An anti-gravity propulsion device is made by applying such a principle that proximity magnets which face each other with the same magnetic poles repel each other and push back. Therein, in order to provide a stable biased centrifugal force from a magnetic centrifugal body (3) group which circulates while pushing against a wall surface of an inner circumference, the orbit circle is turned to such a shape of short elliptic shape (R1, D3) that a lower half circle thereof is shortened a little and, further, by obscuring biased centrifugal gravity force proceeding upward generated by offsetting each other with a force of repulsion magnetic force (5) installed on the surrounding in order to make the strong centrifugal gravity force quantity toward the lower side which is generated on the magnetic centrifugal body ineffective.SELECTED DRAWING: Figure 10
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Description

[Technical field]

[0001] The present invention relates to a propulsion device and a propulsion engine. [Background technology]

[0002] All previous flying devices for propulsive flight in the air have relied on the use of lift or reaction forces from atmospheric pressure loads or space particles. Summary of the Invention [Problem to be solved by the invention]

[0003] To provide an antigravity propulsion device that operates by nullifying a part of centrifugal gravity and can be used in places vulnerable to the effects of noise, heat, wind, etc., and further as an attitude control device for artificial satellites in outer space, in contrast to conventional propulsion types that interfere with the surrounding environment to some extent in order to obtain reaction energy. [Means for solving the problem]

[0004] Any number of identical centrifugal bodies (3) with their centrifugal body bearings (3c) constrained by centrifugal body secondary pins (3b) are pin-connected by centrifugal body primary pins (3a) at the positions of pin holes drilled around the power plate (2) corresponding to the centrifugal body bearings, and they are housed in the housing (1) via the main shaft bearings (4). Therefore, when the power plate main shaft (2a) is rotated counterclockwise, the centrifugal body bearings fitted to the centrifugal bodies pinned at the end of the power plate strongly press against the inner circumferential surface (1a) of the housing all over the circumference according to the rotation speed (Figures 7 and 10).

[0005] The circular shape of the housing inner peripheral surface (1a) is a semicircular arc whose center (C) is the intersection point with the Y-axis, which has the X-axis as its lower chord, and three other arcs are tangent-connected to each other to make up the remaining part, and the centers of these arcs (C1, C2, C3) are separated by arbitrary distances from the center point (C) of the semicircular arc, which is the main axis point of the power plate, on the X-axis and the positive Y-axis, so that the centrifugal body revolves in a short elliptical orbit (R1, D3) of this shape rather than a perfect circle (R1, R2) (Fig. 11).

[0006] When the centrifugal body, which revolves around the main axis (C) of the power plate while pressing against the inner surface of the housing, moves along a circular orbit (D3) that is shorter than the perfect circular orbit (R1, R2). Since the rigidity of the housing absorbs the stress of the perfect circular orbit (R2), the main axis of the power plate at this point maintains a power balance at its center.

[0007] The centrifugal body that revolves around the inner circumference of the housing and the power source (5) that is arranged to interfere with it and can be braked above and below are both ferromagnetic and are set up so that their magnetic poles repel each other (Figure 12). Therefore, when the machine is stopped or goes into maintenance mode, the power source control box can be lowered to the bottom end (S2) of the provided power source control box to keep the magnetic forces away from each other (Figure 10).

[0008] To levitate the object in the air, the centrifugal bearing fitted to the rapidly rotating ferromagnetic centrifugal body presses against the inner circumferential surface of the housing. The centrifugal force of the power source is arranged to cancel out the downward centrifugal force to the extent that it lightly presses the circumferential wall surface (D3). This makes it possible to generate a powerful thrust on the rotating shaft (C) due to the upward biased centrifugal force. By optimizing the main shaft rotation speed of the power plate and the degree of magnetic interference with the power source, it becomes possible to stably control the anti-gravity propulsion of the target levitated heavy object from a stopped state to the maximum output range. Effect of the Invention

[0009] It is possible to quietly levitate heavy objects with almost no physical impact on the surrounding environment. [Brief description of the drawings]

[0010] [Figure 1] FIG. 2 is a front view of the present invention. [Diagram 2] FIG. 2 is a right side view of the present invention. [Diagram 3] FIG. [Figure 4] FIG. 2 is a front view of the present invention when stopped without the lid. [Diagram 5] FIG. 2 is a cross-sectional view taken along line AA' of the present invention. [Figure 6] FIG. 2 is a front view of the present invention when in operation without the lid. [Figure 7] FIG. 2 is an elevational view of the present invention without the lid. [Figure 8] FIG. 2 is a top view of the present invention. [Figure 9] FIG. [Figure 10] FIG. 3 is a cross-sectional view taken along the line BB' of the present invention. [Figure 11] FIG. 4 is an explanatory diagram of a circular shape of an inner peripheral surface of a housing according to the present invention. [Figure 12] FIG. 4 is a diagram showing the action of repulsive magnetic force when the present invention is stopped. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0011] The flying vehicle floats due to the upward thrust generated by the high-speed rotation of the multiple main shafts of this device attached to it and the connected rotary power source, and the forward and backward tilt created by the rotational movement angle of the main body around the axis of this device acts as a rudder for free movement through space, enabling quasi-level flight from takeoff to landing. EXAMPLES

[0012] When the prototype was actually tested, it was confirmed that the device was moved in the intended direction when subjected to the repulsive magnetic force of the fixed magnets. [Industrial Applicability]

[0013] Attitude control devices for levitating vehicles, sea and mountain rescue aircraft, space shuttle carriers, airborne stages, and artificial satellites, etc. [Explanation of symbols]

[0014] 1. Housing 1a Housing inner surface 2. Power Plate 2a Power Plate Axis 2b Power plate primary pin 3 Centrifugal body (ferromagnetic body) 3a Centrifugal body primary pin 3b Centrifugal body secondary pin 3c Centrifugal Bearing 4. Main shaft bearing 5 Power source (ferromagnetic material) 5a Power source support plate 5b Power source magnetic interference control rod 5c Power source magnetic interference adjustment moving space 6 Body mounting bolts 7 Lid 7a Lid mounting bolt holes 7b Lid mounting bolt C Center of rotation axis C1, C2, C3 Centers of three arbitrary arcs joined tangent to each other D3 Short elliptical orbit around R1 centered on the main axis of the Power Plate NN or S pole R1 A perfect circular orbit around R2, centered on the power plate's main axis R2 A perfect circular orbit around R1, centered on the power plate's main axis SN or S magnetic pole S1 Power source position at maximum output S2 Power source position during shutdown and maintenance

Claims

【Claim 1】 At a specific position around the power plate (2) having the main shaft (2a) at the center (C), a specific number of magnetic centrifugal bodies (3) with a centrifugal body bearing (3c) constrained by pins (3a) to spread outwards by the centrifugal force caused by the counterclockwise rotation of the main shaft are inscribed and orbiting. The shape of the inner peripheral surface (1a) of the housing is such that it can be set within the range up to a perfect circle where the arc ends of the upper half of the circle with the X-axis as the lower chord and the centers of three circles equally distant from the drive shaft (C) (C1, C2, C3) are all tangentially joined at four points. A powerful centrifugal force is exerted on the inner peripheral surface of the short elliptical orbit (D3) set in the deformed width (R2 - D3) region by the orbiting magnetic centrifugal bodies (3). The power source (5) has an arbitrary shape that functions to cancel out the weight of the centrifugal force by magnetism to the extent of lightly pressing on the bottom surface vicinity of the inner peripheral surface of the short elliptical orbit (D3). When the power source (5) is installed below or horizontally in the deformed width (R2 - D3) region, its magnetic polarity is a repulsive pole. When installed on the lid (7) side to attract the weight of the centrifugal force of the magnetic centrifugal body (3) pressing on the short elliptical orbit (D3) surface upwards to cancel out this gravity, the attracting pole is set as the effective magnetic pole. By this mechanism, which also operates with an alternating-pole electromagnet, the magnetic centrifugal bodies (3) orbiting on the surface set in the deformed width (R2 - D3) region of the housing invalidate the gravity caused by the magnetic centrifugal force received near their bottom surfaces by magnetism, and utilize the thrust generated when the centrifugal force that has lost its center of rotation pushes the inner peripheral (D3) surface of the housing from the inside in the opposite direction (R1) like a cut-string octopus. A propulsion device characterized by this.