CN118205726A

CN118205726A - Elliptical hollow track propeller

Info

Publication number: CN118205726A
Application number: CN202410225989.XA
Authority: CN
Inventors: 张敬
Original assignee: Individual
Current assignee: Individual
Priority date: 2024-02-29
Filing date: 2024-02-29
Publication date: 2024-06-18

Abstract

The invention discloses an elliptical hollow orbit propeller, and relates to the technical field of space engines. The elliptical hollow track propeller effectively solves the problems that the prior art is not suitable for manufacturing a flying saucer engine and is not suitable for continuous navigation in the universe. The idea of the invention is that under the condition that the resultant force is zero, the direction of one component force is changed, so that the included angle of the two component forces is changed, and the resultant force is not zero. The method adopted by the invention is that the direction of the linear momentum is adjusted through the acceleration, the deceleration, the mutual conversion of the linear momentum and the angular momentum of the pulley module in the object U, and the magnitude difference of the momentum and the acting force in the opposite direction is generated, so that the resultant force born by the object U in the object U is not zero, and the thrust generated in the object U pushes the spacecraft to continuously fly in the universe.

Description

Elliptical hollow track propeller

Technical Field

The invention relates to the technical field of space engines, in particular to an elliptical hollow orbit propeller.

Background

It is envisaged that a device may be used to determine its own ideas by accelerating, decelerating, interconverting linear and angular momentums, adjusting the direction of the linear momentums, generating a difference in magnitude between the momentums and the forces in opposite directions, generating thrust from the interior of the object to propel a spacecraft in the universe for a number of years later, seeing a science popularization video in which the angular momentum is converted into linear momentums to propel itself forward. The invention is used for proving whether the method and thought of the method are correct or not.

Disclosure of Invention

The invention aims to solve the technical problem of providing an elliptical hollow orbit propeller, which adjusts the direction of linear momentum through acceleration, deceleration, interconversion of linear momentum and angular momentum in an object to generate the magnitude difference of momentum and acting force in the opposite direction, and generates thrust from the interior of the object to push a spacecraft to continuously fly in the universe.

In order to achieve the above object, the present invention provides the following technical solutions:

Oval cavity track propeller, its characterized in that: the oval hollow track propeller comprises an object U (3) which is static under a vacuum weightlessness state, an oval hollow track (8) is arranged in the object U (3), the oval hollow track (8) is an oval track formed by mutually communicating a linear acceleration section (4), a lower end U-shaped bend (5), a linear deceleration section (6) and an upper end U-shaped bend (7), an electromagnet module (2) is positioned on two sides of the linear acceleration section (4) and the linear deceleration section (6), a vertical guide rail (10), a horizontal guide rail (12), an electromagnet module (2) and a Hall sensor (16) are arranged in the oval hollow track (8), and the pulley module (1) circularly moves in the oval hollow track (8), and is provided with a vertical guide wheel (9), a horizontal guide wheel (11), a magnet (13), a lead counterweight (14) and a positioning magnet (15).

In order to generate upward force on the object U (3), the linear acceleration section (4) accelerates the pulley module (1) in the track downwards through the electromagnet modules (2) at the two sides.

In order to enable the object U (3) to generate upward acting force, the linear deceleration section (6) decelerates the pulley module (1) in the track upwards through the electromagnet modules (2) at the two sides.

In order to change the movement direction of the pulley module (1), two ends of the lower U-shaped bend (5) are respectively connected with the linear acceleration section (4) and the linear deceleration section (6).

In order to change the movement direction of the pulley module (1), two ends of the upper U-shaped bend (7) are respectively connected with the linear deceleration section (6) and the linear acceleration section (4).

In order to facilitate the running of the pulley module (1) on the guide rail, collision with the oval hollow rail (8) is prevented, and a vertical guide rail (10) and a horizontal guide rail (12) are arranged inside the oval hollow rail (8).

In order to facilitate positioning of the pulley module (1), a plurality of Hall sensors (16) are arranged inside the elliptical hollow rail (8).

In order to facilitate acceleration and deceleration of the pulley module (1), the electromagnet module (2) is composed of a plurality of electromagnets, and the electromagnets are arranged on the inner walls of the linear deceleration section (6) and the linear acceleration section (4) in a straight line shape.

In order to facilitate the running of the pulley module (1) on the guide rail and prevent collision with the elliptical hollow rail (8), the pulley module (1) is externally provided with a vertical guide wheel (9) and a horizontal guide wheel (11).

In order to facilitate positioning of the pulley module (1), a positioning magnet (15) is arranged outside the pulley module (1).

In order to facilitate acceleration and deceleration of the pulley module (1), a magnet (13) is arranged outside the pulley module (1).

In order to obtain a larger reaction force, a lead counterweight (14) is arranged inside the pulley module (1), and the weight of the pulley module (1) is increased.

The beneficial effects of adopting above technical scheme are: the invention provides another method and thinking different from rocket engines, which is characterized in that thrust is generated in an object through acceleration, deceleration and interconversion of linear momentum and angular momentum, substances are not required to be discharged like a rocket, and the thrust can be continuously generated in the object only by electricity, so that a spacecraft is pushed to freely navigate in the universe.

Drawings

The following describes the embodiments of the present invention in further detail with reference to the accompanying drawings.

FIG. 1 is a schematic illustration of an elliptical hollow-rail propulsion of the present invention;

FIG. 2 is a schematic cross-sectional view of an elliptical hollow rail and sled module of the present invention;

FIG. 3 is a side view of a sled module of the elliptical hollow track pusher of the present invention;

the device comprises a pulley module 1, an electromagnet module 2, an object U, a linear acceleration section 4, a lower U-shaped bend 5, a linear deceleration section 6, an upper U-shaped bend 7, an elliptical hollow track 8, a vertical guide wheel 9, a vertical guide rail 10, a horizontal guide wheel 11, a horizontal guide rail 12, a magnet 13, a lead counterweight 14, a positioning magnet 15 and a Hall sensor 16.

Detailed Description

Embodiments of elliptical hollow-track propellers are described in detail below with reference to the figures.

Fig. 1, 2 and 3 show a specific embodiment and process of the elliptical hollow-rail propulsion of the present invention:

In fig. 1, the trolley module (1) accelerates downwards in the linear acceleration section (4) through the electromagnet module (2), while the object U (3) obtains an upward force F1. The pulley module (1) passes through the U-shaped bend (5) at the lower end and enters the linear deceleration section (6), and meanwhile, the object U (3) obtains a downward acting force F2. The pulley module (1) decelerates the pulley module (1) in the linear deceleration section (6) through the electromagnet module (2), and the object U (3) obtains an upward acting force F3. The trolley module (1) passes through the upper U-shaped bend (7) and enters the linear acceleration section (4), and simultaneously the object U (3) obtains an upward acting force F4, and then the trolley module (1) starts to accelerate into the next cycle.

The process and conclusion of the invention, according to the law of conservation of momentum, the trolley module (1) obtains a downward momentum equal to the upward F1 in the linear acceleration section (4), the resultant of which is zero. The direction of the pulley module (1) is changed after passing through the U-shaped bend (5) at the lower end, and simultaneously, the downward acting force F2 is generated, so long as the pulley module (1) still has kinetic energy when entering the linear deceleration section (6), and F2 is necessarily smaller than F1. The result is that the downward F2 is smaller than the sum of the upward F1 plus F3 plus F4, so that the object U (3) is moved upward by the upward force. The invention uses the acceleration and deceleration of the pulley module (1) in the object U (3), and uses the U-shaped bend (5) at the lower end to adjust the direction of the pulley module (1) so that the resultant force born by the object U (3) in the object U is not zero, thereby generating thrust in the object U (3) to push the spacecraft to continuously fly in the universe.

The foregoing is merely a preferred embodiment of the present invention, and it should be noted that modifications and improvements could be made by those skilled in the art without departing from the inventive concept, which fall within the scope of the present invention.

Claims

1. Oval cavity track propeller, its characterized in that: the oval hollow track propeller comprises an object U (3) which is static under a vacuum weightlessness state, an oval hollow track (8) is arranged in the object U (3), the oval hollow track (8) is an oval track formed by mutually communicating a linear acceleration section (4), a lower end U-shaped bend (5), a linear deceleration section (6) and an upper end U-shaped bend (7), an electromagnet module (2) is positioned on two sides of the linear acceleration section (4) and the linear deceleration section (6), a vertical guide rail (10), a horizontal guide rail (12), an electromagnet module (2) and a Hall sensor (16) are arranged in the oval hollow track (8), and the pulley module (1) circularly moves in the oval hollow track (8), and is provided with a vertical guide wheel (9), a horizontal guide wheel (11), a magnet (13), a lead counterweight (14) and a positioning magnet (15).

2. The elliptical hollow rail propulsion of claim 1, wherein: the linear acceleration section (4) accelerates the pulley modules (1) in the track downwards through the electromagnet modules (2) at two sides, so that the object U (3) obtains upward acting force.

3. The elliptical hollow rail propulsion of claim 1, wherein: the linear deceleration section (6) decelerates the pulley module (1) in the track upwards through the electromagnet modules (2) at two sides, so that the object U (3) obtains upward acting force.

4. The elliptical hollow rail propulsion of claim 1, wherein: the two ends of the lower U-shaped bend (5) are respectively connected with the linear acceleration section (4) and the linear deceleration section (6), the direction of the motion of the pulley module (1) after passing through the lower U-shaped bend (5) is changed, and meanwhile, the object U (3) obtains downward acting force.

5. The elliptical hollow rail propulsion of claim 1, wherein: the two ends of the upper U-shaped bend (7) are respectively connected with the linear deceleration section (6) and the linear acceleration section (4), the direction of the motion of the pulley module (1) after passing through the upper U-shaped bend (7) is changed, and meanwhile, the object U (3) obtains upward acting force.

6. The elliptical hollow rail propulsion of claim 1, wherein: the vertical guide rail (10) and the horizontal guide rail (12) which are arranged in the oval hollow rail (8) can enable the pulley module (1) to run on the guide rail, and the pulley module (1) and the oval hollow rail (8) are prevented from collision.

7. The elliptical hollow rail propulsion of claim 1, wherein: the interior of the elliptical hollow track (8) is provided with a plurality of Hall sensors (16) which can position the pulley module (1).

8. The elliptical hollow rail propulsion of claim 1, wherein: the electromagnet module (2) is composed of a plurality of electromagnets, the electromagnets are arranged on the inner walls of the linear deceleration section (6) and the linear acceleration section (4) in a straight line shape, and the magnetic field generated by the electromagnets is utilized to accelerate and decelerate the pulley module (1).

9. The elliptical hollow rail propulsion of claim 1, wherein: the outside of the pulley module (1) is provided with a vertical guide wheel (9) and a horizontal guide wheel (11) which can enable the pulley module (1) to run on the guide rail, so that the pulley module (1) and the oval hollow track (8) are prevented from collision.

10. The elliptical hollow rail propulsion of claim 1, wherein: the pulley module (1) is externally provided with a positioning magnet (15) which can be matched with a Hall sensor (16) to position the pulley module (1).

11. The elliptical hollow rail propulsion of claim 1, wherein: the outside of the pulley module (1) is provided with a magnet (13) which is matched with the electromagnet module (2) to accelerate and decelerate the pulley module (1).

12. The elliptical hollow rail propulsion of claim 1, wherein: the inside of the pulley module (1) is provided with a lead counterweight (14), so that the weight of the pulley module (1) is increased, and the reaction force obtained by the object U (3) is improved.