Elliptical orbit thruster

Abstract

An elliptical orbit thruster, which relates to the technical field of aerospace engines. The elliptical orbit thruster effectively solves the problem of the prior art not being suitable for manufacturing engines of unidentified flying objects, and also provides another method and line of thought that differ from those regarding rocket engines. The magnitude differences of momentum and acting force in opposite directions are produced by means of the conversion of acceleration, deceleration, momentum and angular momentum inside an object, such that a spacecraft can be pushed to continuously fly in the universe without the need to discharge substances.

Description

Elliptical orbit thruster Technical Field

[0001] The present invention relates to the technical field of aerospace engines, in particular to an elliptical orbit thruster. Background Art

[0002] If flying saucers really exist, then the rocket propulsion method may be wrong and it is not suitable for building the engine of a flying saucer.

[0003] Many years ago, when I was young and ignorant, I had a chance idea and conceived a device that could generate differences in the magnitude of momentum and force in opposite directions inside an object through acceleration, deceleration, and conversion of momentum and angular momentum. It could propel a spacecraft to continue flying in the universe without the need to discharge matter. This invention is used to prove whether its methods and ideas are correct.

[0004] Summary of the Invention

[0005] The technical problem to be solved by the present invention is to provide an elliptical orbit thruster, which generates differences in the magnitude of momentum and force in opposite directions inside an object through acceleration, deceleration, and conversion of momentum and angular momentum, thereby enabling the spacecraft to continue flying in the universe without the need to discharge matter.

[0006] To achieve the above object, the present invention provides the following technical solutions:

[0007] An elliptical orbit thruster is characterized in that: the elliptical orbit thruster includes an object U (3) that is stationary in a vacuum weightlessness state, an elliptical orbit (8) is arranged inside the object U (3), the elliptical orbit (8) is an elliptical hollow orbit composed of a linear acceleration section (4), a lower U-shaped bend (5), a linear deceleration section (6), and an upper U-shaped bend (7) that are interconnected, the steel ball (1) circulates in the elliptical orbit (8), the flywheel (2) is located at both ends of the circular orbit (8) and is connected to the lower U-shaped bend (5) and the upper U-shaped bend (7), and an electromagnet is arranged on the flywheel (2).

[0008] In order to generate an upward force on the object U (3), the linear acceleration section (4) accelerates the downwardly moving steel ball (1) through an electromagnet.

[0009] In order to generate an upward force on the object U (3), the linear deceleration section (6) decelerates the upwardly moving steel ball (1) through an electromagnet.

[0010] In order to facilitate adjustment of the movement direction of the ball (1), the rotation direction of the flywheel (2) is the same as the movement direction of the ball (1).

[0011] In order to facilitate adjustment of the movement direction of the ball (1), the upper U-shaped bend (7) and the lower U-shaped bend (5) are U-shaped hollow tracks for accommodating the ball (1).

[0012] The beneficial effect of adopting the above technical solution is: the present invention provides another method and idea different from rocket engines, which generates thrust inside an object through acceleration, deceleration, and conversion of momentum and angular momentum. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] The specific embodiments of the present invention will be described in further detail below with reference to the accompanying drawings.

[0014] FIG1 is a schematic diagram of the first stage of the elliptical orbit thruster of the present invention;

[0015] FIG2 is a schematic diagram of the second stage of the elliptical orbit thruster of the present invention;

[0016] FIG3 is a schematic diagram of the third stage of the elliptical orbit thruster of the present invention;

[0017] FIG4 is a schematic diagram of the fourth stage of the elliptical orbit thruster of the present invention;

[0018] FIG5 is a schematic diagram of torque elimination of the elliptical orbit thruster of the present invention;

[0019] Among them, 1. small ball, 2. flywheel, 3. object U, 4. linear acceleration section, 5. lower end U-shaped bend, 6. linear deceleration section, 7. upper end U-shaped bend, 8. elliptical orbit. DETAILED DESCRIPTION

[0020] The specific implementation of the elliptical orbit thruster will be described in detail below with reference to the accompanying drawings.

[0021] Figures 1, 2, 3, 4 and 5 show the specific implementation and process of the elliptical orbit propulsor of the present invention:

[0022] In Figure 1, the steel ball (1) is accelerated downward by an electromagnet in the linear acceleration section (4), and at the same time, the object U (3) receives an upward force F1.

[0023] In Figure 2, the ball (1) is attracted by the electromagnet on the flywheel (2) at the end of the linear acceleration section (4). The ball (1) and the flywheel (2) rotate together through the lower U-shaped bend (5). When the ball (1) enters the linear deceleration section (6), the electromagnet is de-energized, and the ball (1) separates from the flywheel (2). At the same time, the object U (3) receives a downward force F2.

[0024] As shown in FIG3 , the steel ball (1) is decelerated by the electromagnet in the linear deceleration section (6), and the object U (3) receives an upward force F3.

[0025] In Figure 4, the ball (1) is attracted by the electromagnet on the flywheel (2) at the end of the linear deceleration section (6). The ball (1) and the flywheel (2) rotate together through the upper U-shaped bend (7). When the ball (1) enters the linear acceleration section (4), the electromagnet is de-energized, and the ball (1) separates from the flywheel (2). At the same time, the object U (3) receives an upward force F4, and then the ball (1) returns to the starting position and begins to accelerate into the next cycle.

[0026] Figure 5 shows that in order to solve the torque generated by the flywheel (2), the torque can be offset by arranging two sets of elliptical tracks (8) on the object U (3) and running them simultaneously.

[0027] The process and conclusion of the present invention are that the ball (1) continuously repeats the four cycles of Figures 1, 2, 3, and 4 in the elliptical track (8), which can continuously generate upward forces F1, F3, and F4, as well as a downward force F2. Moreover, the downward force F2 is less than the sum of the upward forces F1, F3, and F4. Therefore, the object U (3) will be subjected to the upward force and move upward. The idea of ​​the present invention is to use various motions or energy conversions within an object to make the momentum or force within the object have different magnitudes in the opposite direction. Then, a flying saucer is possible.

[0028] The above are only preferred embodiments of the present invention. It should be pointed out that those skilled in the art can make several modifications and improvements without departing from the inventive concept of the present invention, and these all fall within the scope of protection of the present invention.

Claims

1. An elliptical orbit thruster, characterized in that: The elliptical orbit thruster comprises an object U (3) which is stationary in a vacuum weightlessness state, wherein an elliptical orbit (8) is arranged inside the object U (3), wherein the elliptical orbit (8) is an elliptical hollow orbit composed of a linear acceleration section (4), a lower U-shaped bend (5), a linear deceleration section (6), and an upper U-shaped bend (7) which are interconnected, wherein the steel ball (1) circulates in the elliptical orbit (8), wherein the flywheel (2) is located at both ends of the circular orbit (8) and is connected to the lower U-shaped bend (5) and the upper U-shaped bend (7), and wherein an electromagnet is arranged on the flywheel (2).

2. The elliptical orbit thruster according to claim 1, characterized in that: The linear acceleration section (4) is a hollow track on which an electromagnet is installed, and the steel ball (1) is accelerated by electromagnetic force.

3. The elliptical orbit thruster according to claim 1, characterized in that: The linear deceleration section (6) is a hollow track equipped with an electromagnet, which decelerates the steel ball (1) through electromagnetic force.

4. The elliptical orbit thruster according to claim 1, characterized in that: The rotation direction of the flywheel (2) is the same as the movement direction of the ball (1).

5. The elliptical orbit thruster according to claim 1, characterized in that: The upper U-shaped bend (7) and the lower U-shaped bend (5) are U-shaped hollow tracks for accommodating the small ball (1) to adjust the movement direction.

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