Civil mobile spaceflight launcher

Abstract

The invention relates to a civil mobile spaceflight launcher, which is invented for coping with sudden accidents, has a flight function, can take off and land vertically, has multiple flight modes, is not limited by airport runways, can take off and land under various regional environment conditions, can flexibly select a launching area, and is convenient to use. The rocket can be brought to the stratosphere to be launched, the spacecraft can be flexibly selected to be launched in the stratosphere above areas such as unmanned areas, desert areas, waste parks and seas when passing through the earth, pollution to the ground is reduced, damage to human caused by flying fragments is reduced, and disasters caused by rocket falling due to unsuccessful launching in accidents are reduced. Ground facility construction is reduced, configuration of ground crew is reduced, and flight personnel can be received back from the outer space or needed materials can be conveyed at any time.

Description

Technical Field

[0001] The present invention belongs to the technical field of space launchers, and in particular relates to a civilian mobile space launcher. Background Art

[0002] The dream of mankind to fly in the blue sky has been realized, but in the process of mankind moving from the earth to the blue sky, the traditional fixed mode is still used to use the space launch site to launch spacecraft to send mankind from the earth to space. Although this is successful, it also has limitations. Once an unpredictable event occurs at the launch site, it will directly affect the expected launch, or when an accident occurs to the pilots flying in space and they need to return to the earth temporarily individually or collectively, they cannot return to the earth, resulting in adverse consequences. The present invention is a civilian mobile space launcher invented to deal with the above-mentioned sudden accidents. Summary of the invention

[0003] The civilian mobile space launcher of the present invention has a flight function, can take off and land vertically and has multiple flight modes, is not restricted by airport runways, can take off and land under various geographical environmental conditions, can flexibly select a launch area, can bring a rocket to the stratosphere for launch, and can flexibly select to launch over uninhabited areas, desert areas, wasteland areas, the sea and other areas when the spacecraft passes over the earth, thereby reducing pollution to the earth, reducing damage to humans caused by flying debris, reducing disasters to humans caused by the falling of the rocket body due to launch failures, reducing ground facility construction, reducing the configuration of ground crew, and can flexibly select multiple time periods to pick up flight personnel from space or transport required materials.

[0004] The technical solution of the present invention is: a civilian mobile space launcher, including 1. an overall structure of the space launcher, 2. a space launcher frame, 3. a space launcher landing gear, 4. a space launcher hatch, 5. a space launcher chord ladder, 6. a space launcher metal mesh cover, 7. a space launcher light tube, 8. an external display screen of the space launcher, 9. a space launcher cockpit fixed frame, 10. a space launcher cockpit gyro balancer, 11. a space launcher cockpit gyro balancer sliding ball, 12. a space launcher cockpit, 13. a space launcher cockpit guide rail, 14 a space launcher cockpit hatch, 15. a space launcher control system operation keyboard, 16. a space launcher control system display screen, 17. a space launcher engine rotation angle adjustment electric drive shaft, 18. a space launcher engine rotation angle adjustment electric drive turntable, 19. a space launcher engine.

[0005] The overall structure of the aerospace launcher described in the technical solution of the present invention is a circular disk shape.

[0006] The space launcher frame described in the technical solution of the present invention is a special frame for the space launcher, the space launcher landing gear is arranged and installed at the bottom of the space launcher, the space launcher hatch is arranged and installed on the left side of the bottom of the space launcher, the space launcher chord ladder is arranged and installed at the lower part of the space launcher hatch, the space launcher metal mesh cover is arranged and installed on the outside of the space launcher, the space launcher light tube is arranged and installed around the space launcher, and the space launcher external display screen is arranged and installed at the bottom of the space launcher.

[0007] The space launcher cockpit fixing frame described in the technical solution of the present invention is in the shape of a round sphere.

[0008] The space launcher cockpit gyro balancer described in the technical solution of the present invention is symmetrically distributed up, down, front, back, left and right and is installed on the inner wall of the space launcher cockpit fixed frame; the space launcher cockpit gyro balancer sliding ball is installed on the space launcher cockpit gyro balancer; the space launcher cockpit is in the shape of a round sphere; a space launcher cockpit guide rail is installed around the outer side of the space launcher cockpit; the space launcher cockpit gyro balancer sliding ball is connected to the space launcher cockpit guide rail installed around the outer side of the space launcher cockpit; the space launcher cockpit gyro balancer sliding ball is buckled in the guide groove of the space launcher cockpit guide rail around the outer side of the space launcher cockpit, and can realize reciprocating sliding up, down, front, back, left and right.

[0009] The space launcher cockpit door described in the technical solution of the present invention is arranged and installed on the front lower left side of the space launcher cockpit.

[0010] The space launcher control system operation keyboard and the space launcher control system display screen described in the technical solution of the present invention are arranged and installed in the space launcher cockpit.

[0011] The electric drive shaft for adjusting the engine rotation angle of the space launcher described in the technical solution of the present invention is driven by a motor to rotate forward 360 degrees and backward 360 degrees. The electric drive turntable for adjusting the engine rotation angle of the space launcher is fixed on the electric drive shaft for adjusting the engine rotation angle of the space launcher. The electric drive turntable for adjusting the engine rotation angle of the space launcher is driven by a motor to rotate forward 360 degrees and backward 360 degrees. The electric drive shaft for adjusting the engine rotation angle of the space launcher and the electric drive turntable for adjusting the engine rotation angle of the space launcher constitute a space launcher engine rotation angle adjustment device. The space launcher engine rotation angle adjustment device has four units of the space launcher engine rotation angle adjustment device which are symmetrically arranged and installed on the space launcher frame. The space launcher engine rotation angle adjustment device can adjust the space launcher engine rotation angle arbitrarily up, down, front, back, left and right.

[0012] The space launcher engine described in the technical solution of the present invention is installed on the space launcher engine rotation angle adjustment electric drive turntable. The space launcher of the present invention is equipped with four engines of equal power, and the engines are respectively installed at four symmetrical positions of the space launcher through the space launcher engine rotation angle adjustment device.

[0013] The space launcher of the present invention upgrades and improves the existing space launcher technology, so that the space launcher can show its superiority, flexibility and safety in executing the launch mission. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 Schematic diagram of the overall external structure of the space launcher

[0015] Figure 2 Schematic cutaway view of a space launch vehicle

[0016] Figure 3 Schematic diagram of the space launch vehicle engine being adjusted to vertical take-off and landing state

[0017] Figure 4 Schematic diagram of the space launch vehicle engine being adjusted to parallel flight in the air

[0018] Figure 5 Schematic diagram of the space launch vehicle engine being adjusted to fly sideways in the air

[0019] Figure 6 Schematic diagram of the space launcher engine being adjusted to the air suspension state

[0020] Figure 7 Schematic diagram of a space launcher carrying a rocket launcher when manned

[0021] Figure 8 Schematic diagram of a space launcher carrying a rocket launcher when unmanned

[0022] In the figure: 1. The schematic diagram of the overall structure of the space launcher is to show the unique image of the space launcher from the appearance. 2. The frame of the space launcher is used to carry and connect all the components of the space launcher. 3. The landing gear of the space launcher is used to support the overall weight of the space launcher when the space launcher is parked, moved, or landed on the ground. 4. The hatch of the space launcher is used to provide space launcher pilots and related personnel performing flight launch missions to enter and exit the space launcher. 5. The string ladder of the space launcher is used to provide space launcher pilots and related personnel performing flight launch missions to get on and off the space launcher. 6. The metal mesh cover of the space launcher is used to prevent birds and air debris from entering the space launcher when the space launcher is performing flight launch missions in the air. 7. The light tube of the space launcher is used for lighting and sending signals for the space launcher. 8. The external display screen of the space launcher is used to display videos, pictures, and texts when the space launcher is flying in the air.

[0023] In the technical solution of the present invention: 9. The fixed frame of the cockpit of the space launcher is in the shape of a circular sphere, and 10. The gyro balancer of the cockpit of the space launcher and 11. The sliding ball of the gyro balancer of the cockpit of the space launcher are symmetrically arranged and installed on the upper, lower, front, rear, left and right inner side walls of the circular sphere as a whole, wherein 11. The sliding ball of the gyro balancer of the cockpit of the space launcher is buckled with 12. The guide rail of the cockpit of the space launcher is arranged and installed around the outer side of the cockpit of the space launcher, so that 11. The sliding ball of the gyro balancer of the cockpit of the space launcher is buckled in the guide groove of the guide rail of the cockpit of the space launcher 13.

[0024] In the technical solution of the present invention: 14. The cockpit door of the space launcher is arranged and installed on the lower left side of the front of the cockpit of the space launcher. 15. The keyboard of the space launcher operating system and 16. The display screen of the space launcher operating system are arranged and installed in 12. The cockpit of the space launcher.

[0025] In the technical solution of the present invention: 17. The space launcher adjusts the engine rotation angle and electrically drives the rotating shaft, 18. The space launcher adjusts the engine rotation angle and electrically drives the rotating disk, 19. The space launcher adjusts the engine rotation angle and electrically drives the rotating shaft bearing bracket, 20. The space launcher adjusts the engine rotation angle and electrically drives the rotating shaft motor, 21. The space launcher adjusts the engine rotation angle and electrically drives the rotating shaft motor wiring harness, 22. The space launcher adjusts the engine rotation angle and electrically drives the rotating disk, 23. The space launcher adjusts the engine rotation angle and electrically drives the rotating disk gear, 24. The space launcher adjusts the engine rotation angle and electrically drives the rotating disk motor, 25. The space launcher adjusts the engine rotation angle and electrically drives the rotating disk motor wiring harness, 26. The space launcher adjusts the engine rotation angle and electrically drives the rotating disk motor gear. The space launcher can adjust the space launcher engine 27 to rotate upward, downward, forward, backward, leftward, and rightward without angle restrictions according to the instructions issued by the space launcher driver operating the space launcher operating system keyboard 15 during the flight launch mission, so that the space launcher can change a variety of flight postures.

[0026] In the technical solution of the present invention: 27. The space launch vehicle engine has four equal power divisions installed in symmetrical positions on the aircraft. DETAILED DESCRIPTION

[0027] The present invention will be further described below in conjunction with the accompanying drawings.

[0028] like Figures 1 to 8 As shown, a civil mobile space launcher of the present invention is an implementation example, including a schematic diagram of the overall external structure of the space launcher Figure 1 , space launcher frame 2, space launcher landing gear 3, space launcher hatch 4, space launcher string ladder 5, space launcher metal mesh cover 6, space launcher light tube 7, space launcher external display screen 8. The overall appearance of the space launcher Figure 1A space launcher frame 2 is installed inside, and its function is to carry and connect all the components of the space launcher. The space launcher landing gear 3 is installed at the bottom of the space launcher, and there are three of them, which are divided into three supporting points in a triangle. Its function is to bear the weight of the space launcher when the space launcher is parked, moved, or landed on the ground. The space launcher hatch is installed on the left side of the lower part of the space launcher, and is used to provide the space launcher driver or the related personnel who perform the flight launch mission to enter and exit the space launcher. The space launcher string ladder 5 is installed below the space launcher hatch 4, and is used to provide the space launcher driver or the related personnel who perform the flight launch mission to get on and off the space launcher. The space launcher metal mesh cover 6 is installed around the space launcher, and is used to prevent birds and air garbage from entering the space launcher when the space launcher is flying in the air. The space launcher light tube 7 is installed at multiple points on the surface around the space launcher, and is used for lighting and sending signals for the space launcher. The external display screen 8 of the space launcher is arranged and installed at the lower part of the space launcher, and is used for displaying video, pictures and text when the space launcher performs a flight launch mission in the air.

[0029] The space launcher cockpit fixing frame 9 of the present invention is arranged and installed at the center of the space launcher, and is in the shape of a round sphere. The space launcher cockpit gyro balancer 10 is arranged and installed at the symmetrical positions of the upper, lower, front, rear, left and right parts of the inner side wall of the round sphere. The space launcher cockpit gyro balancer sliding ball 11 is arranged and installed on the space launcher cockpit gyro balancer 10. The space launcher cockpit 12 is made of special materials such as bulletproof, explosion-proof and fireproof, and is a space launcher that can be used in any space launcher regardless of whether the space launcher is launched in the air. In case of any accident, the cockpit 12 of the space launcher can be guaranteed to be intact. The cockpit guide rails 13 of the space launcher are arranged around the outer side of the cockpit. The sliding ball 11 of the cockpit gyro balancer of the space launcher is buckled and connected with the guide groove of the cockpit guide rail 13 of the space launcher. When the space launcher performs the flight launch mission, no matter what kind of flight tumbling action or flight attitude change the space launcher makes in the air, the cockpit 12 of the space launcher will remain parallel under the action of the cockpit gyro balancer 10. When the space launcher is not allowed to tumble and change its attitude, the pilot of the space launcher also rolls horizontally, vertically, upside down, and upright with the space launcher, causing the pilot of the space launcher to have high blood pressure, panic, and dizziness. This prevents the pilot of the space launcher from mistaking the sea for the blue sky in an emergency and manipulating the space launcher to continue to descend and fall into the sea, causing tragedy.

[0030] The space launcher cockpit door 14 is installed on the lower left side of the space launcher cockpit. It is a special door for the space launcher driver to enter and exit the cockpit. No other irrelevant personnel are allowed to enter. The space launcher control system operation keyboard 15 and the space launcher operating system display screen 16 are installed in the space launcher cockpit 12. The space launcher control system described in the space launcher technical solution of the present invention is composed of a space launcher external multi-directional camera and a space launcher cockpit external multi-directional camera to collect information. After the information is displayed on the space launcher operating system display screen 16, the space launcher driver controls the space launcher operating system keyboard 15 to perform the flight launch mission.

[0031] The present invention discloses a civilian mobile space launcher, which has an electric drive shaft 17 for adjusting the rotation angle of an engine, an electric drive shaft bearing 18 for adjusting the rotation angle of an engine, an electric drive shaft bearing bracket 19 for adjusting the rotation angle of an engine, an electric drive shaft motor 20 for adjusting the rotation angle of an engine, a wire harness 21 for the electric drive shaft motor for adjusting the rotation angle of an engine, an electric drive turntable 22 for adjusting the rotation angle of an engine, a gear 23 for the electric drive turntable for adjusting the rotation angle of an engine, an electric drive turntable motor 24 for adjusting the rotation angle of an engine, a wire harness 25 for the electric drive turntable motor for adjusting the rotation angle of an engine, and an electric drive turntable motor gear 26 for adjusting the rotation angle of an engine. The space launcher can adjust the rotation of the space launcher engine 27 upward, downward, forward, backward, leftward, and rightward without angle restriction according to the instructions issued by the space launcher driver operating the space launcher operating system keyboard 15 during the execution of the flight launch mission, so that the space launcher can change numerous flight postures.

Claims

1. A civilian mobile space launcher, comprising 1. an overall structure of the space launcher, 2. a space launcher frame, 3 a space launcher landing gear, 4. a space launcher hatch, 5. a space launcher chord ladder, 6. a space launcher metal mesh cover, 7. a space launcher light tube, 8. an external display screen of the space launcher, 9. a space launcher cockpit fixed frame, 10. a space launcher cockpit gyro balancer, 11. a space launcher cockpit gyro balancer sliding ball, 12. a space launcher cockpit, 13. a space launcher cockpit guide rail, 14. a space launcher cockpit hatch, 15. a space launcher control system operation keyboard, 16 a space launcher control system display screen, 17. a space launcher engine rotation angle adjustment electric drive shaft, a space launcher engine rotation angle adjustment electric drive turntable, and a space launcher engine.

2. According to the civilian mobile space launcher described in claim 1, the frame is a special frame for the space launcher, the space launcher landing gear is arranged and installed at the bottom of the space launcher, the space launcher hatch is arranged and installed on the left side of the bottom of the space launcher, the space launcher chord is arranged and installed at the lower part of the space launcher hatch, the space launcher metal mesh cover is arranged and installed on the outside of the space launcher, the space launcher light tube is arranged and installed around the space launcher, and the space launcher external display screen is arranged and installed at the bottom of the space launcher.

3. According to the civil mobile space launcher described in claim 2, the cockpit gyro balancer is symmetrically distributed up, down, front, back, left and right and is installed on the inner wall of the fixed frame of the space launcher cockpit, the sliding ball of the gyro balancer of the space launcher cockpit is installed on the gyro balancer of the space launcher cockpit, the space launcher cockpit is in the shape of a round sphere, and the space launcher cockpit guide rail is installed around the outer side of the space launcher cockpit, the sliding ball of the gyro balancer of the space launcher cockpit is connected to the space launcher cockpit guide rail installed around the outer side of the space launcher cockpit, and the sliding ball of the gyro balancer of the space launcher cockpit is buckled in the guide groove of the space launcher cockpit guide rail around the outer side of the space launcher cockpit, and can realize reciprocating sliding up, down, front, back, left and right. The space launcher cockpit door described in the technical solution of the present invention is arranged and installed on the front lower left side of the space launcher cockpit.

4. According to the civilian mobile space launcher described in claim 3, the control system operation keyboard and the space launcher control system display screen are arranged and installed in the space launcher cockpit.

5. According to a civilian mobile space launcher as described in claim 4, the electric drive shaft for adjusting the engine rotation angle is driven by a motor and can rotate forward 360 degrees and backward 360 degrees. The electric drive turntable for adjusting the engine rotation angle of the space launcher is fixed on the electric drive shaft for adjusting the engine rotation angle of the space launcher. The electric drive turntable for adjusting the engine rotation angle of the space launcher is driven by a motor and can rotate forward 360 degrees and backward 360 degrees. The electric drive shaft for adjusting the engine rotation angle of the space launcher and the electric drive turntable for adjusting the engine rotation angle of the space launcher constitute a space launcher engine rotation angle adjustment device. The space launcher engine rotation angle adjustment device has a total of four units of the space launcher engine rotation angle adjustment device which are symmetrically arranged and installed on the space launcher frame. The space launcher engine rotation angle adjustment device can adjust the space launcher engine rotation angle arbitrarily up, down, front, back, left, and right.

6. According to the civilian mobile space launcher of claim 5, the engine is installed on the electric drive turntable for adjusting the engine rotation angle of the space launcher. The space launcher of the present invention is equipped with four engines of equal power, and the engines are respectively installed at four symmetrical positions of the space launcher through the space launcher engine rotation angle adjustment device. The space launcher of the present invention upgrades and improves the existing space launcher technology, so that the space launcher can show its superiority, flexibility and safety in executing the launch mission.

Images