CN118618636A - Gyroscopic precession thrusters - Google Patents

Abstract

The present invention discloses a gyro precession thruster, and relates to the technical field of aerospace thrusters. The gyro precession thruster effectively solves the problem that existing rocket engines are not suitable for continuous navigation in the universe and fuel is exhausted. The idea and method of the present invention is that a combination of a U-shaped connecting rod and a gyro rotating disk inside the thruster body acts as an eccentric wheel, which can make the thruster body produce up and down displacement, and the stability and precession of the gyro module are activated by the high-speed rotation of the gyro rotating disk. The rotation direction of the flywheel is adjusted by the motor module, thereby adjusting the direction of the axial stage precession force, so that the up and down displacement of the thruster body has a difference in size, and the present invention can be used to propel the spacecraft to fly continuously in the universe.

Description

Gyroscopic precession thrusters

Technical Field

The present invention relates to the technical field of aerospace propulsion devices, and in particular to a gyroscopic precession propulsion device.

Background Art

Rocket engines consume fuel, and the limited fuel of a rocket will eventually run out when it is sailing in space. The stability and precession of a gyroscope can resist gravity. By adjusting the angle between the fulcrum and the rotation axis, the force direction of the gyroscope, and the direction of the flywheel rotation, the direction of the gyroscope precession can be adjusted to make the displacement of the object different in size, so that it can sail in space without fuel. Based on this idea, the present invention makes a gyro precession thruster that can sail in the vacuum environment of space without fuel.

Summary of the invention

The technical problem to be solved by the present invention is to provide a gyro precession thruster, which circulates through a U-shaped connecting rod and a gyroscope in a circular cavity. During the movement, the angle between the rotation axis of the gyroscope module and the U-shaped connecting rod, the force direction of the gyroscope, and the direction of rotation of the flywheel are adjusted, thereby adjusting the direction of the precession of the gyroscope, so that the displacement of the thruster body has a difference in size, and the thruster body can be used to propel the spacecraft to continue flying in the universe.

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

A gyro precession thruster, characterized in that: the gyro precession thruster comprises a thruster body (1) which is stationary in a vacuum weightless state, the thruster body (1) has two circular cavities (2) inside, the circular cavity (2) is divided into a right stage (7), a lower stage (8), a left stage (9), and an upper stage (10), a total of four stages forming a cycle, a U-shaped connecting rod (3) is inside the circular cavity (2), a rotating disk drive motor (4) and a gyroscope rotating disk (5) are installed at the end of the U-shaped connecting rod (3), the rotating disk drive motor (4) is connected to the gyroscope rotating disk (5) through gears, the gyroscope rotating disk (5) is divided into an axial stage (11), a lower adjustment stage (12), a parallel stage (13), and an upper adjustment stage (14), a total of four stages forming a cycle, and a plurality of gyroscope modules (1) are installed on the gyroscope rotating disk (5). 9) and a motor module (16), wherein the motor module (16) is connected to a gyroscope bracket (18) of a gyroscope module (19) through a gear, wherein the gyroscope module (19) is a gyroscope composed of a gyroscope bracket (18), a flywheel motor (17) and a flywheel (15), wherein the flywheel motor (17) is mounted on the gyroscope bracket (18), and flywheels (15) are mounted at both ends of an output shaft of the flywheel motor (17), wherein a main motor (6) is mounted at the rear of the propeller body (1), and conductive slip rings (20) are mounted on the output shafts of the main motor (6), a rotating disk drive motor (4) and the motor module (16), wherein the end of the output shaft of the main motor (6) is connected to a U-shaped connecting rod (3), and after passing through the conductive slip ring (20), the conductive wire (21) is connected to the rotating disk drive motor (4), the motor module (16) and the flywheel motor (17) to provide them with power and transmit control signals.

In order to eliminate air resistance and offset torque, the circular cavity (2) is in a vacuum state, and the U-shaped connecting rods (3) in the two circular cavities (2) rotate in opposite directions.

In order to facilitate the propeller body (1) to move upward a large distance in the right stage (7), the gyroscope rotating disk (5) rotates at a high speed to cause the gyroscope module (19) to precess upward in the axial stage (11) of the right stage (7). The direction of precession is opposite to the direction of movement of the U-shaped connecting rod (3). At this time, when the U-shaped connecting rod (3) moves from top to bottom, a large force is required to overcome the precession of the gyroscope, thereby generating a large upward reaction force on the propeller body (1).

In order to facilitate the propeller body (1) to move downward a small distance in the left stage (9), the gyroscope rotating disk (5) rotates at a high speed to cause the gyroscope module (19) to precess upward in the axial stage (11) of the left stage (9). The direction of the precession is the same as the direction of movement of the U-shaped connecting rod (3). At this time, when the U-shaped connecting rod (3) moves from bottom to top, a smaller force is required to overcome the precession of the gyroscope, thereby generating a smaller downward reaction force on the propeller body (1).

In order to generate a greater precession force, the gyroscope rotating disk (5) is equipped with a plurality of gyroscope modules (19). The plurality of gyroscope modules (19) on the gyroscope rotating disk (5) rotating at a high speed can generate a greater precession force.

In order to achieve the steering of the propeller body (1), there are four stages in total, namely the axial stage (11), the lower adjustment stage (12), the parallel stage (13), and the upper adjustment stage (14). By adjusting the proportion of the parallel stage (13) and the axial stage (11), the displacement distance on one side can be adjusted to achieve the steering of the propeller body (1).

In order to change the moving direction and steering of the propeller body (1), the axial stage (11) can be placed in the right stage (7), the lower stage (8), the left stage (9), and the upper stage (10) to adjust the thrust direction and steering of the propeller body (1).

In order to facilitate the flywheel (15) to switch between clockwise and counterclockwise, the motor module (16) is an integrated module consisting of a motor and a reducer, which is used to adjust the rotation direction of the flywheel (15) in the gyroscope module (19) and rotate the flywheel (15) 180 degrees.

In order to cause the propeller body (1) to be displaced, the U-shaped connecting rod (3) and the gyroscope rotating disk (5) are combined to act as an eccentric wheel.

In order to drive the U-shaped connecting rod (3) to move upward or downward, the high-speed rotation of the gyroscope rotating disk (5) can cause the gyroscope module (19) to produce an upward or downward precession in the axial stage (11).

The beneficial effect of adopting the above technical solution is: the present invention provides another method and idea different from the rocket engine. By circulating the U-shaped connecting rod and the gyroscope rotating disk in the circular cavity, the direction of the gyroscope module is adjusted during the movement to make the displacement of the thruster body have differences in size, so that the thruster body can push the spacecraft to continue flying in the universe.

BRIEF DESCRIPTION OF THE DRAWINGS

The specific implementation modes of the present invention are further described in detail below in conjunction with the accompanying drawings.

Fig. 1 is a side view of the basic principle of the present invention;

Fig. 2 is a top view of the basic principle of the present invention;

FIG3 is a schematic diagram of the force direction and precession direction of the gyroscope A according to the basic principle of the present invention;

FIG4 is a front view of the propeller body of the present invention;

FIG5 is a top view of the rotating disk of the gyroscope in the right stage of the present invention;

Fig. 6 is a side view of the force direction of the axial stage gyroscope of the right stage of the present invention;

FIG7 is a top view of the rotating disk of the gyroscope in the left stage of the present invention;

FIG8 is a side view of the axial stage gyroscope in the left stage of the present invention in the force direction;

FIG9 is a side view of the propeller body of the present invention;

Among them, 1. thruster body, 2. circular cavity, 3. U-shaped connecting rod, 4. rotating disk drive motor, 5. gyroscope rotating disk, 6. main motor, 7. right stage, 8. lower stage, 9. left stage, 10. upper stage, 11. axial stage, 12. lower adjustment stage, 13. parallel stage, 14. upper adjustment stage, 15. flywheel, 16. motor module, 17. flywheel motor, 18. gyroscope bracket, 19. gyroscope module, 20. conductive slip ring, 21. wire.

DETAILED DESCRIPTION

The specific implementation of the gyro precession thruster will be described in detail below with reference to the accompanying drawings.

Figures 1, 2, 3, 4, 5, 6, 7, 8 and 9 show the specific implementation and process of the gyro precession thruster of the present invention:

Figure 1, gyroscope A and gyroscope B are placed on a common fulcrum. The fulcrum of gyroscope B on the left is on the rotating surface. At this time, the stability of the gyroscope does not work. Gyroscope B will fall immediately due to the influence of gravity. The rotation axis of gyroscope A on the right is in the same line with the fulcrum. At this time, the stability and precession of the gyroscope work, which will overcome gravity and prevent it from falling. In order to make gyroscope A and gyroscope B fall at the same time, the downward force required is different in size.

Figure 2 shows that there is a certain angle between the fulcrum of gyroscope C and the rotation axis of gyroscope C. At this time, gyroscope C will not fall. Gyroscope C, like gyroscope A, has the stability and precession of a gyroscope.

Figure 3, when gyroscope A rotates clockwise, it is affected by the downward gravity F1 and will precess to the left in the direction of F2. When a force is applied to the left to accelerate the rotation in the direction of F2, gyroscope A will precess upward in the direction of F3. However, when gyroscope A rotates counterclockwise, it is affected by the downward gravity F1 and will precess to the right in the direction of F4. When a force is applied to the right to accelerate the rotation in the direction of F4, gyroscope A will precess upward in the direction of F3. The direction of gyroscope A's precession can be changed by adjusting the rotation direction of gyroscope A and the direction of the applied force.

FIG4 shows that the combination of the U-shaped connecting rod (3) and the gyroscope rotating disk (5) in the two circular cavities (2) acts as an eccentric wheel, which can cause the propeller body (1) to move up and down.

As shown in Figures 5 and 6, when the U-shaped connecting rod (3) and the gyroscope rotating disk (5) run to the axial stage (11) of the right stage (7), there is a certain angle between the rotating axis of the flywheel (15) in the gyroscope module (19) and the U-shaped connecting rod (3), which is the same as the gyroscope C in Figure 2. At this time, the stability and precession of the gyroscope still work. While the gyroscope rotates clockwise, it moves along the direction of F2 with the gyroscope rotating disk (5), generating a precession in the upward direction F3. The direction of the precession is exactly opposite to the direction of movement of the U-shaped connecting rod (3). At this time, when the U-shaped connecting rod (3) moves from top to bottom, a large force is required to overcome the precession of the gyroscope, thereby generating a large upward reaction force on the propeller body (1), causing the propeller body (1) to move upward a large distance in the right stage (7).

As shown in Figures 7 and 8, when the U-shaped connecting rod (3) and the gyroscope rotating disk (5) move to the axial stage (11) of the left stage (9), the stability and precession of the gyroscope come into play. At this time, the gyroscope rotates counterclockwise and moves along the direction of F4 along with the gyroscope rotating disk (5), generating a precession in the upward direction of F3. The direction of the precession is the same as the direction of movement of the U-shaped connecting rod (3). At this time, when the U-shaped connecting rod (3) moves from bottom to top, only a small force is required to overcome the stability of the gyroscope, thereby generating a small downward reaction force on the propeller body (1), causing the propeller body (1) to move downward a small distance in the left stage (9).

4, 5, 6, 7 and 8, in combination with these five figures, the distance of the upward displacement of the propeller body (1) is greater than the distance of the downward displacement, so that the propeller body (1) moves upward.

The process and conclusion of the present invention are as follows: the two main motors (6) of the propeller body (1) drive the U-shaped connecting rods (3) in the two circular cavities (2) to rotate in opposite directions; the rotating disk driving motor (4) drives the gyroscope rotating disk (5) to rotate at high speed; the motor module (16) drives the gyroscope module (19) to rotate to adjust the direction of the gyroscope; and the flywheel motor (17) drives the flywheel (15) to rotate at high speed. In FIG4 , the combination of the U-shaped connecting rods (3) in the two circular cavities (2) and the gyroscope rotating disk (5) acts as an eccentric wheel, causing the propeller body (1) to move up and down. When the U-shaped connecting rod (3) and the gyroscope rotating disk (5) run to the axial stage (11) of the right stage (7), as shown in Figures 5 and 6, the stability of the gyroscope takes effect and precesses upward. At this time, when the U-shaped connecting rod (3) moves from top to bottom, a large force is required to overcome the precession of the gyroscope, thereby generating a large upward reaction force on the propeller body (1), causing the propeller body (1) to move upward a large distance in the right stage (7). When the U-shaped connecting rod (3) and the gyroscope rotating disk (5) run to the axial stage (11) of the left stage (9), as shown in Figures 7 and 8, the stability of the gyroscope takes effect and precesses upward. At this time, when the U-shaped connecting rod (3) moves from bottom to top, only a small force is required to overcome the stability of the gyroscope, thereby generating a small downward reaction force on the propeller body (1), causing the propeller body (1) to move downward a small distance in the left stage (9). In conjunction with Figures 4, 5, 6, 7 and 8, the distance that the propeller body (1) is displaced upward is greater than the distance that it is displaced downward, so that the propeller body (1) moves upward.

When the direction of movement and steering of the propeller body (1) need to be adjusted, in conjunction with Figures 4 and 5, the gyroscope modules (19) on the gyroscope rotating disk (5) in the left circular cavity (2) are all adjusted to the parallel stage (13). At this time, the left side will not produce upward displacement, and the right side will produce it normally, so the propeller body (1) will turn left. In conjunction with Figures 4, 5, and 7, the propeller body (1) moves upward because the axial stage (11) appears in the right stage (7) and the left stage (9). By adjusting the position where the axial stage (11) of the two gyroscope rotating disks (5) appears, the direction of displacement of the propeller body (1) can be adjusted. By adjusting the position where the axial stage (11) of one of the gyroscope rotating disks (5) appears, the propeller body (1) can be turned.

The above are only preferred embodiments of the present invention. It should be pointed out that a person 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 protection scope of the present invention.

Claims (10)

1. Gyro precession propeller, its characterized in that: the gyroscope precession propeller comprises a propeller body (1) which is static under the vacuum weightlessness state, 2 circular cavities (2) are arranged in the propeller body (1), the circular cavities (2) are divided into 4 stages including a right side stage (7), a lower side stage (8), a left side stage (9) and an upper side stage (10) to form a cycle, a U-shaped connecting rod (3) is arranged in the circular cavities (2), a rotary disk driving motor (4) and a gyroscope rotary disk (5) are arranged at the tail end of the U-shaped connecting rod (3), the rotary disk driving motor (4) is connected with the gyroscope rotary disk (5) through gears, the gyroscope rotary disk (5) is divided into an axial stage (11), a lower side regulating stage (12), a parallel stage (13) and an upper side regulating stage (14) to form a cycle, a plurality of gyroscope modules (19) and motor modules (16) are arranged on the gyroscope rotary disk (5), the motor modules (16) are connected with a gyroscope bracket (18) of the gyroscope module (19) through gears, the gyroscope modules (19) and the gyroscope module (18) are arranged on the gyroscope bracket (17), flywheel (15) are equipped with at flywheel motor (17) output shaft both ends, main motor (6) are equipped with at propeller body (1) rear portion, all be equipped with on the output shaft of main motor (6), rotary disk driving motor (4) and motor module (16) and lead electrical slip ring (20), main motor (6) output shaft end is connected with U-shaped connecting rod (3), behind wire (21) through lead electrical slip ring (20), intercommunication rotary disk driving motor (4), motor module (16) and flywheel motor (17) provide power supply and transmission control signal for it.

2. The cylindrical cavity (2) according to claim 1, characterized in that: the circular cavities (2) are in a vacuum state, and the U-shaped connecting rods (3) in the 2 circular cavities (2) rotate oppositely to eliminate air resistance and offset torque.

3. The right-hand stage (7) according to claim 1, characterized in that: the gyroscope rotating disc (5) rotates at a high speed to enable the gyroscope module (19) to upwards precess in an axial stage (11) of the right stage (7), the precession direction is opposite to the movement direction of the U-shaped connecting rod (3), and when the U-shaped connecting rod (3) moves from top to bottom, a large force is required to overcome the precession of the gyroscope, so that a large upward reaction force is generated on the propeller body (1), and the propeller body (1) is upwards displaced by a large distance in the right stage (7).

4. The left-hand stage (9) according to claim 1, characterized in that: the gyroscope rotating disc (5) rotates at a high speed to enable the gyroscope module (19) to advance upwards in an axial stage (11) of the left stage (9), the advancing direction is the same as the moving direction of the U-shaped connecting rod (3), and when the U-shaped connecting rod (3) moves from bottom to top, smaller force is needed to overcome the gyroscope advancing property, so that smaller downward reaction force is generated on the propeller body (1), and the propeller body (1) is displaced downwards by a smaller distance in the left stage (9).

5. The gyroscope rotating disk (5) according to claim 1, characterized in that: the gyroscope rotating disc (5) is provided with a plurality of sets of gyroscope modules (19), and the plurality of sets of gyroscope modules (19) on the gyroscope rotating disc (5) rotating at high speed can generate larger precession force upwards in the axial stage (11) of the right side stage (7) and also generate larger precession force upwards in the axial stage (11) of the left side stage (9).

6. The axial phase (11), the lower adjustment phase (12), the parallel phase (13), the upper adjustment phase (14) according to claim 1, characterized in that: the axial stage (11), the lower adjusting stage (12), the parallel stage (13) and the upper adjusting stage (14) are 4 stages in total, and the displacement distance of one side can be adjusted by adjusting the proportion of the parallel stage (13) to the axial stage (11), so that the steering of the propeller body (1) is realized.

7. The axial phase (11) according to claim 1, characterized in that: the axial stage (11) can be arranged at the positions of the 4 stages of the right stage (7), the lower stage (8), the left stage (9) and the upper stage (10) through the axial stage (11), so that the direction of thrust of the propeller body (1) can be adjusted, and the moving direction and the steering of the propeller body (1) can be changed.

8. The electric machine module (16) of claim 1, wherein: the motor module (16) is an integrated module formed by a motor and a speed reducer, and is used for adjusting the rotation direction of the flywheel (15) in the gyroscope module (19), and the flywheel (15) can be converted between clockwise and anticlockwise by rotating the flywheel (15) by 180 degrees.

9. The U-shaped link (3) and gyroscope rotating disk (5) according to claim 1, characterized in that: the combination of the U-shaped connecting rod (3) and the gyroscope rotating disc (5) plays a role of an eccentric wheel and is used for enabling the propeller body (1) to generate displacement.

10. The gyroscope rotating disk (5) and the gyroscope module (19) according to claim 1, characterized in that: the gyroscope rotating disc (5) rotates at a high speed, so that the gyroscope module (19) can precess upwards or downwards in the axial stage (11) to drive the U-shaped connecting rod (3) to move upwards or downwards.