CN110775074A - Lunar-based constant-temperature layer underground vacuum flight track traffic system - Google Patents

Lunar-based constant-temperature layer underground vacuum flight track traffic system Download PDF

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Publication number
CN110775074A
CN110775074A CN201911237646.0A CN201911237646A CN110775074A CN 110775074 A CN110775074 A CN 110775074A CN 201911237646 A CN201911237646 A CN 201911237646A CN 110775074 A CN110775074 A CN 110775074A
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China
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station
electromagnetic
car
carriage
electromagnetic device
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CN201911237646.0A
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张国庆
谢和平
高明忠
李存宝
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Shenzhen University
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Shenzhen University
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Priority to CN201911237646.0A priority Critical patent/CN110775074A/en
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Pending legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
    • B61B1/00—General arrangement of stations, platforms, or sidings; Railway networks; Rail vehicle marshalling systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L13/00—Electric propulsion for monorail vehicles, suspension vehicles or rack railways; Magnetic suspension or levitation for vehicles
    • B60L13/04—Magnetic suspension or levitation for vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
    • B61B13/00—Other railway systems
    • B61B13/10—Tunnel systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/16—Extraterrestrial cars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G4/00—Tools specially adapted for use in space

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  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • Control Of Vehicles With Linear Motors And Vehicles That Are Magnetically Levitated (AREA)

Abstract

The invention provides a lunar-based constant temperature layer underground vacuum flying track traffic system, which is arranged at a constant temperature layer of a moon, and comprises a first station, a second station, a tunnel, a first electromagnetic device, a second electromagnetic device, a magnetic suspension device and a carriage, wherein the tunnel is connected with the first station and the second station, the tunnel is in a vacuum environment, the first electromagnetic device is arranged at the first station, the second electromagnetic device is arranged at the second station, the magnetic suspension device is arranged on the inner wall of the tunnel, and the magnetic suspension device applies magnetic suspension force overcoming gravity to the carriage so as to enable the carriage to be in a suspension state; the first electromagnetic device applies electromagnetic force to the carriage to enable the carriage to move from the first station to the second station; the second electromagnetic device applies electromagnetic force to the car to stop the car at the second station. Through the arrangement, the vacuum flying rail transit system is favorable for carrying out high-efficiency traffic transportation, and meanwhile, the suitable temperature is favorable for people to take.

Description

Lunar-based constant-temperature layer underground vacuum flight track traffic system
Technical Field
The invention belongs to the field of traffic, and particularly relates to a lunar-based constant-temperature-layer underground vacuum flying rail traffic system.
Background
The moon is the only satellite of the earth and is the sentinel for deep space exploration of human beings, and the development of intelligent utilization of the underground space of the moon is an important measure for establishing a moon base and bringing the moon into the human activity range. However, due to the extreme environments of microgravity, near vacuum, extremely large temperature difference (-183-127 ℃), ultralow thermal conductivity and the like of the lunar surface, a good living environment cannot be provided for human beings.
How to build a vacuum flying rail transit system under the extreme environment of the moon becomes a key for establishing the traffic connection between human bases.
Disclosure of Invention
The invention aims to provide a lunar-base constant-temperature layer underground vacuum flying rail transit system which can carry out traffic and transportation in an extreme environment.
In order to realize the purpose of the invention, the invention provides the following technical scheme:
the invention provides a vacuum flying track traffic system in a vacuum environment, which is arranged at a constant temperature layer of a moon, the temperature of the constant temperature layer is kept constant, the distance between the constant temperature layer and the moon surface of the moon is at least 1 m, the vacuum flying track traffic system comprises a first station, a second station, a tunnel, a first electromagnetic device, a second electromagnetic device, a magnetic suspension device and a carriage, the tunnel is connected with the first station and the second station, the tunnel is in a vacuum environment, the first electromagnetic device is arranged at the first station, the second electromagnetic device is arranged at the second station, the magnetic suspension device is arranged on the inner wall of the tunnel, the carriage is used for bearing passengers and moves in the tunnel, the magnetic suspension device applies magnetic suspension force which overcomes gravity to the carriage, so that the carriage is in a suspension state; the first electromagnetic device exerts electromagnetic force on the carriage to enable the carriage to move from the first station to the second station; the second electromagnetic device exerts electromagnetic force on the carriage to stop the carriage at the second station.
In one embodiment, the vacuum flying rail transit system further includes a third electromagnetic device, the third electromagnetic device is disposed at the second station, the third electromagnetic device is disposed between the second electromagnetic device and the first electromagnetic device, the third electromagnetic device and the second electromagnetic device are disposed at an interval to form a first interval space, and the position of the carriage when the carriage stops is located in the first interval space.
In one embodiment, the first compartment is provided with a coil assembly that applies an electromagnetic force to the vehicle compartment to accelerate or decelerate the vehicle compartment.
In one embodiment, the first electromagnetic device includes a first electromagnetic baffle, the second electromagnetic device includes a second electromagnetic baffle, the extending direction of the tunnel is a first direction, the first electromagnetic baffle and the second electromagnetic baffle are perpendicular to the first direction, the first electromagnetic baffle applies electromagnetic force to a first end face of the carriage to drive the carriage from the first station to the second station, and when the carriage moves to the second station, the second electromagnetic baffle applies electromagnetic force to a second end face of the carriage opposite to the first end face.
In one embodiment, the third electromagnetic device includes a third electromagnetic shield, the third electromagnetic shield is opposite to the second electromagnetic shield, the first separation space is formed between the third electromagnetic shield and the second electromagnetic shield, and when the car moves from the first station to the second station, the third electromagnetic shield applies an electromagnetic force to the first end surface of the car, so that the car reciprocally decelerates and displaces to a stop in the first separation space in the first direction.
In one embodiment, the third electromagnetic device further includes a first displacement mechanism, the first displacement mechanism is connected to the third electromagnetic baffle, and the first displacement mechanism is configured to control displacement of the third electromagnetic baffle, so as to enable the second separated space to communicate with or close the tunnel.
In one embodiment, the first end surface and the second end surface are planar and parallel to each other, the car further includes a plurality of side surfaces connected to the first end surface and the second end surface, the plurality of side surfaces, the first end surface and the second end surface enclose a car space for bearing passengers, and the cross section of the car in the first direction is rectangular.
In one embodiment, the number of the side faces is 3, and in a second direction perpendicular to the first direction, the cross section of the carriage is a first triangle, the cross section of the tunnel is a second triangle, and the first triangle corresponds to the second triangle.
In one embodiment, the inner wall of the tunnel comprises a bottom wall and two side walls, and the magnetic suspension devices are arranged on the bottom wall and the side walls.
In one embodiment, the first station and the second station are provided with a lifting system, one end of the lifting system is connected with the first station or the second station, and the other end of the lifting system protrudes out of a lunar surface.
Through the arrangement, the vacuum tunnel enables the carriage to run without air resistance, the magnetic suspension device provides a running condition without friction for the carriage, the carriage can run at a high speed without a power device, the vacuum flight track traffic system is favorable for carrying out high-efficiency traffic transportation from the first station to the second station, and meanwhile, the constant-temperature layer provides suitable temperature for the vacuum flight track traffic system and is favorable for people to ride.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and other drawings can be obtained by those skilled in the art without creative efforts.
FIG. 1 is a schematic representation of the geological structure of a planet;
FIG. 2 is a schematic structural diagram of a vacuum flight rail transit system provided by the present invention;
fig. 3 is a schematic structural diagram of the vacuum flying rail transit system of fig. 2 in a second direction.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is apparent that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention.
Referring to fig. 1, from a geological perspective, a planet (e.g., the earth or an alien planet) includes an outer surface 11, and the outer surface 11 is exposed to radiation from stars (e.g., the sun). From surface 11 to the inside of planet, include first geological stratification 10, second geological stratification 20 and third geological stratification 30 in proper order, first geological stratification 10 is the soil horizon, and second geological stratification 20 is the mixed layer that soil and rock mix, and third geological stratification 30 is the rock stratum. The thickness H1 of the first geological layer 10, the thickness H2 of the second geological layer 20 and the thickness H3 of the third geological layer 30 are different at different positions on the planet. In some regions on the planet, the geological conditions are uniformly distributed in the radial direction of the planet, the thickness of the second geological layer 20 is 0, the thickness of the first geological layer 10 is uniform, and the position of the original second geological layer 20 is filled with the first geological layer 10 and/or the third geological layer 30. In addition, the thicknesses of the temperature changing layer, the constant temperature layer 40 and the temperature increasing layer of the planet are different at different latitudes. There are many possibilities for the correspondence of the constant temperature layer 40 with the first, second and third geological layers 10, 20, 30. For example, the constant temperature layer 40 is located at a position of the first geological layer 10 close to the second geological layer 20; the constant temperature layer 40 is positioned on the first geological layer 10 and part of the second geological layer 20; the constant temperature layer 40 is positioned on the first geological layer 10 and all the second geological layers 20; the constant temperature layers 40 are located in the first geological formation 10, the second geological formation 20 and the third geological formation 30. Taking the moon as an example, the moon comprises a moon land and a moon sea, the first geological layer 10 is generally 10-20 m deep in the moon sea, the first geological layer 10 is generally 5-10 m deep in the moon land, and the constant temperature layer 40 of the moon is positioned in an area below 1 m deep on the surface of the moon, that is, the constant temperature layer 40 at least comprises an area below 1 m deep of the first geological layer 10.
The extreme environments of microgravity, near vacuum, extremely large temperature difference (-183-127 ℃), ultralow thermal conductivity and the like of the lunar surface make the construction of a traffic system on the lunar surface extremely difficult and difficult to realize.
Referring to fig. 2, on the moon, due to the low thermal conductivity of lunar soil, a constant temperature layer 40 exists below 1 m depth of the moon table, the temperature is kept at about 250K (-20 ℃), and a good temperature environment can be provided for human activities, so that a human activity base on the moon is basically built in the constant temperature layer 40.
Based on the research on the constant temperature layer 40, the embodiment of the invention provides a lunar-based constant temperature layer underground vacuum flying rail transit system, and the vacuum flying rail transit system is arranged at the constant temperature layer 40 of the moon. The vacuum flight track traffic system can be built on the moon and also can be built on the foreign planet, and can provide a relatively livable environment for human beings. Particularly, with the implementation of moon exploration engineering in China, the construction on the moon can be realized in a short time. The detection of Mars also has substantial progress, and the construction of Mars can be realized in the near future.
Referring to fig. 2 and 3, the vacuum flight track traffic system under the lunar-based constant temperature layer provided by the embodiment of the invention is arranged at the constant temperature layer 40, so that the vacuum flight track traffic system has a relatively constant suitable temperature environment. The vacuum flight rail transit system comprises a first station 100, a second station 200, a tunnel 300, a first electromagnetic device 11, a second electromagnetic device 12, a magnetic suspension device 15 and a carriage 400. The tunnel 300 connects the first station 100 and the second station 200, and the tunnel 300 is a vacuum environment. The first electromagnetic device 11 is disposed at the first station 100, and the second electromagnetic device 12 is disposed at the second station 200. The magnetic levitation device 15 is provided on the inner wall of the tunnel 300, and the car 400 is used for carrying passengers and moving in the tunnel 300. The magnetic levitation device 15 applies a magnetic levitation force against the gravity to the car 400 so that the car 400 is in a levitated state.
The first electromagnetic device 11 applies electromagnetic force to the railway car 400 to move the railway car 400 from the first stop 100 to the second stop 200. In addition, when the car 400 departs from the second station to the first station 100, the first electromagnetic device 1 may stop the car 400 at the first station 100.
The second electromagnetic device 12 applies electromagnetic force to the car 400 to stop the car 400 at the second station 200. In addition, when the car 400 is driven from the second station to the first station 100, the first electromagnetic device 1 may drive the car 400 from the second station 200 to the first station 100.
Specifically, the inner wall of the tunnel 300 may be consolidated by spraying special cement mortar through an anchor-spray support technique, so that the tunnel 300 does not collapse under a vacuum condition. The car 400 may carry not only passengers but also cargo. In one embodiment, the interior of the cabin 400 may be filled with air so that a human being may move freely within the cabin 400, and the cabin 400 may be provided with a plurality of doors at the doors of the vehicle to isolate the air-filled cabin 400 from the vacuum environment. In one embodiment, the interior of the cabin 400 may be a vacuum environment, so that the air pressure inside and outside the cabin 400 is balanced. The electromagnetic force generated by the first electromagnetic device 11 and the second electromagnetic device 12 may be a repulsive force or an attractive force.
It can be understood that the vacuum flying rail transit system of the moon needs to be disposed in a space having a small temperature change, such as the constant temperature layer 40 of the moon, since the day and night temperature difference of the moon is large and each device of the vacuum flying rail transit system is easily out of order. And the constant temperature layer 40 of the moon is only 1 meter away from the lunar surface, and the amount of work required for arranging the vacuum flying rail transit system in the constant temperature layer 40 of the moon is small. In addition, due to the environment of micro gravity of the moon, the carriage 400 is more easily levitated by the magnetic levitation device 15, and the power requirement of the magnetic levitation device 15 is more easily satisfied. Meanwhile, the tunnel 300 has a natural vacuum environment due to the environment of the lunar vacuum, and thus the vehicle compartment 400 has no air resistance in the tunnel 300. The material of the tunnel 300 may be lunar soil or lunar rock, and the depth of the tunnel 300 from the lunar surface of the moon is at least 1 meter, so as to ensure that the whole tunnel 300 is located in the constant temperature layer 40. The high vacuum environment of the moon is more suitable for the operation of the vacuum flying rail transit system provided by the invention. Under the vacuum and suspension environment, the kinetic energy of the carriage 400 is basically not lost, the carriage 400 does not need to be provided with a power device, only the first electromagnetic device 11 needs to provide an initial speed, and the carriage 400 can obtain and maintain a faster speed to drive to the next station. Through the arrangement, the vacuum flying rail transit system can overcome the extreme environment of the moon, and is beneficial to the development and civilization of human beings on the moon.
Through the arrangement, the vacuum tunnel 300 enables the carriage 400 to run without air resistance, meanwhile, the magnetic suspension device 15 provides a running condition without friction for the carriage 400, the carriage 400 does not need to be provided with a power device and can run at a high speed, the vacuum flying rail transit system is favorable for carrying out high-efficiency traffic transportation from the first station 100 to the second station 200, and meanwhile, the constant temperature layer 40 provides a proper temperature for the vacuum flying rail transit system, and the vacuum flying rail transit system is favorable for people to ride.
In one embodiment, referring to fig. 2, the vacuum flight rail transit system further includes a third electromagnetic device 13, the third electromagnetic device 13 is disposed at the second station 200, and a fourth electromagnetic device 14 may be further disposed at the first station 100. The third electromagnetic device 13 is disposed between the second electromagnetic device 12 and the fourth electromagnetic device 14, and the fourth electromagnetic device 14 is disposed between the first electromagnetic device 11 and the third electromagnetic device 13. The third electromagnetic device 13 applies electromagnetic force to the car 400 to stop the car 400 at the second station 200, and the fourth electromagnetic device 14 applies electromagnetic force to the car 400 to stop the car 400 at the first station 100.
Specifically, by providing the third electromagnetic device 13 and the fourth electromagnetic device 14, the carriage 400 is stopped at the first station 100 under the electromagnetic force of the first electromagnetic device 11 and the fourth electromagnetic device 14; the cage 400 is stopped at the second station 200 by the electromagnetic force of the second electromagnetic device 12 and the third electromagnetic device 13. In addition, if there is a third station on the side of the second station 200 remote from the first station 100, a driving force can be applied to the train 400 by the third electromagnetic device 13 so that the train 400 can travel to the third station, and similarly, the layout of the third station can refer to the layout of the second station 200. Through the above arrangement, the car 400 can smoothly stop at the first station 100 or the second station 200, and the stability of the vacuum flight rail transit system is improved.
In one embodiment, referring to fig. 2, the first electromagnetic device 11 and the fourth electromagnetic device 14 are disposed at an interval to form a second space 101. The third electromagnetic device 13 is spaced apart from the second electromagnetic device 12 to form a first spacing space 201. The position of the vehicle compartment 400 when it stops is located in the second compartment 101 or the first compartment 201, the second compartment 101 and the first compartment 201 are provided with the coil assembly 21, and the electromagnetic damping device applies electromagnetic force to the vehicle compartment 400 to accelerate or decelerate the vehicle compartment 400. Specifically, the coil block 21 is disposed on the inner wall of the tunnel 300 in the second compartment 101 and the first compartment 201. Through the arrangement, the coil assembly 21 can assist the carriage 400 to stop or start, and is beneficial to shortening the stop time and the start time of the carriage 400, so that the operation cycle of the vacuum flight rail transit system is shorter and the efficiency is higher.
In one embodiment, referring to fig. 2, the first electromagnetic device 11 includes a first electromagnetic shield 111, and the second electromagnetic device 12 includes a second electromagnetic shield 121. The first electromagnetic shield 111 applies an electromagnetic force to a first end surface 401 of the vehicle compartment 400, and the second electromagnetic shield 121 applies an electromagnetic force to a second end surface 402 of the vehicle compartment 400 that is opposite to the first end surface 401. Specifically, the first end surface 401 and the second end surface 402 may be perpendicular to the first direction 91, so that the electromagnetic forces of the first electromagnetic device 11 and the second electromagnetic device 12 are the same as the movement of the car 400, and the car 400 is sufficiently driven, or the electromagnetic forces of the first electromagnetic device 11 and the second electromagnetic device 12 are opposite to the movement of the car 400, and the car 400 is sufficiently stopped. Through the above arrangement, the electromagnetic forces of the first electromagnetic device 11 and the second electromagnetic device 12 can be sufficiently converted into the kinetic energy of the car 400, so that the starting time of the car 400 is further shortened, or the kinetic energy of the car 400 is sufficiently consumed, so that the stopping time of the car 400 is further shortened.
In one embodiment, referring to fig. 2, the third electromagnetic device 13 includes a third electromagnetic shield 131. The third electromagnetic shield 131 is opposed to the second electromagnetic shield 121, and the third electromagnetic shield 131, the second electromagnetic shield 121, and the tunnel 300 form a first spacing space 201. The third electromagnetic shield 131 applies electromagnetic force to the first end surface 401 of the car 400, so that the car 400 performs reciprocating deceleration displacement in the first compartment 201 to stop in the first direction 91, wherein the first direction 91 is the extending direction of the tunnel 300;
the fourth electromagnetic device 14 includes a fourth electromagnetic shield 141, the fourth electromagnetic shield 141 is opposite to the first electromagnetic shield 111, the fourth electromagnetic shield 141, the first electromagnetic shield 111 and the tunnel 300 form the second partitioned space 101, and the fourth electromagnetic shield 141 applies an electromagnetic force to the second end face 402 of the vehicle compartment 400 so that the vehicle compartment 400 is reciprocally decelerated and displaced in the second partitioned space 101 to a stop in the first direction 91.
It is understood that, taking the car 400 parked at the first station 100 as an example, when the car 400 arrives at the first station 100, the first electromagnetic shield 111 first exerts a repulsive force on the car 400, so that the car 400 decelerates. However, since the car 400 is in a vacuum environment and in a floating state, there are no friction and air resistance, and as long as the speed of the car 400 is greater than 0, the car 400 can move all the time, so that it is difficult for the first electromagnetic device 11 to just stop the car 400. The first electromagnetic shield 111 continues to apply the electromagnetic force so that the vehicle compartment 400 decelerates to turn around, and at this time, the fourth electromagnetic shield 141 applies an electromagnetic force to the vehicle compartment 400 opposite to the electromagnetic force applied by the first electromagnetic shield 111 so that the vehicle compartment 400 reciprocates in the second partitioned space 101. The magnitude of the electromagnetic force of the first electromagnetic shield 111 and the electromagnetic force of the fourth electromagnetic shield 141 are adjusted so that the car 400 is stopped in the second partitioned space 101 of the first station 100.
Through the arrangement, the stable parking of the carriage 400 on the first station 100 or the second station 200 is facilitated, and the safety of the vacuum flight rail transit system is improved.
In one embodiment, referring to fig. 2, the third electromagnetic device 13 further includes a first displacement mechanism (not shown). The first displacement mechanism is connected with the third electromagnetic baffle 131, and is used for controlling the displacement of the third electromagnetic baffle 131 so as to open or close the second compartment 101 towards the second station 200;
specifically, the fourth electromagnetic device 14 further includes a second displacement mechanism (not shown). The second displacement mechanism is connected to the fourth electromagnetic barrier 141, and the second displacement mechanism is configured to control the fourth electromagnetic barrier 141 to displace, so that the first partitioned space 201 is opened or closed toward the first station 100. The first displacement mechanism and the second displacement mechanism can be of a push-pull structure, a turnover structure and the like, and can be of a hydraulic mode, a mechanical mode and the like.
It is understood that when the first station 100 of the car 400 is activated, the fourth electromagnetic panel 141 needs to be evacuated so that the car 400 can move away from the second bay space 101 toward the second station 200, and likewise, when the second station 200 of the car 400 is activated, the third electromagnetic panel 131 needs to be evacuated so that the car 400 can move away from the first bay space 201 toward the first station 100. When the vehicle compartment 400 enters the second compartment 101, the fourth electromagnetic shield 141 closes the second compartment 101 to cooperate with the first electromagnetic shield 111 to stop the vehicle compartment 400 in the second compartment 101, and similarly, when the vehicle compartment 400 enters the first compartment 201, the third electromagnetic shield 131 closes the first compartment 201 to cooperate with the second electromagnetic shield 121 to stop the vehicle compartment 400 in the first compartment 201.
In one embodiment, referring to fig. 2, the first end surface 401 and the second end surface 402 are planar and parallel to each other. The car 400 further includes a plurality of side surfaces connected to the first end surface 401 and the second end surface 402, and the plurality of side surfaces, the first end surface 401 and the second end surface 402 enclose a car space for carrying passengers. The tunnel 300 extends in a first direction 91, and the cross section of the car 400 in the first direction 91 is rectangular. Through the above arrangement, the mass distribution of the carriage 400 in the first direction 91 is uniform, which is advantageous for the carriage 400 to be able to run smoothly.
In one embodiment, referring to fig. 2 and 3, the number of sides is 3. In a second direction 92 perpendicular to the first direction 91, the cross section of the car 400 is a first triangle, and the cross section of the tunnel 300 is a second triangle, the first triangle corresponding to the second triangle. Specifically, the first triangle and the second triangle are isosceles triangles, the first triangle and the second triangle have a corresponding relation similar to a triangle, and the corresponding edges are parallel to each other. Through the arrangement, the rolling of the carriage 400 during high-speed operation is avoided, and the safety of the vacuum flight rail transit system is further improved.
In one embodiment, referring to fig. 2 and 3, the inner wall of the tunnel 300 includes a bottom wall 301 and two side walls 302, and the magnetic suspension device 15 is disposed on both the bottom wall 301 and the side walls 302. Specifically, the magnetic levitation devices 15 respectively provided on the two side walls 302 generate the same magnitude of magnetic force to the vehicle body 400. Through the above arrangement, the electromagnetic force received by the carriage 400 is further balanced, which is beneficial to the smooth operation of the carriage 400.
In one embodiment, referring to fig. 2, the first station 100 and the second station 200 are provided with a lifting system (not shown), one end of the lifting system is connected to the first station 100 or the second station 200, and the other end of the lifting system protrudes from the lunar surface. In particular, the lift system may lead to a human base deeper in the moon. By providing the lifting system, it is convenient for passengers to get on the lifting system at the first station 100 or the second station 200 to arrive at the lunar surface.
In an embodiment, referring to fig. 2, the vacuum flying rail transit system may be built in a lunar simulation environment of the earth, and the vacuum flying rail transit system is used as a simulation experiment system for testing the vacuum flying rail transit system, such as the material of the carriage 400 in the vacuum flying rail transit system and the distance between the carriage 400 and the tunnel 300, so as to facilitate the vacuum flying rail transit system to be built on the moon.
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.

Claims (10)

1. The vacuum flying track traffic system is characterized by being arranged at a constant temperature layer of a moon, the temperature of the constant temperature layer is kept constant, the distance between the constant temperature layer and the moon surface of the moon is not less than 1 m, the vacuum flying track traffic system comprises a first station, a second station, a tunnel, a first electromagnetic device, a second electromagnetic device, a magnetic suspension device and a carriage, the tunnel is connected with the first station and the second station, the tunnel is in a vacuum environment, the first electromagnetic device is arranged at the first station, the second electromagnetic device is arranged at the second station, the magnetic suspension device is arranged on the inner wall of the tunnel, the carriage is used for bearing passengers, the tunnel moves in the carriage, and the magnetic suspension device exerts magnetic suspension force overcoming gravity on the carriage, so that the carriage is in a suspension state; the first electromagnetic device exerts electromagnetic force on the carriage to enable the carriage to move from the first station to the second station; the second electromagnetic device exerts electromagnetic force on the carriage to stop the carriage at the second station.
2. The vacuum flying rail transit system of claim 1, further comprising a third electromagnetic device, wherein the third electromagnetic device is disposed at the second station, the third electromagnetic device is disposed between the second electromagnetic device and the first electromagnetic device, the third electromagnetic device and the second electromagnetic device are disposed at a distance to form a first separation space, and the position of the car when the car stops is located in the first separation space.
3. The vacuum flying rail transit system of claim 2, wherein the first compartment is provided with a coil assembly which applies electromagnetic force to the car to accelerate or decelerate the car.
4. The vacuum flying rail transit system of claim 2, wherein the first electromagnetic device comprises a first electromagnetic shield, the second electromagnetic device comprises a second electromagnetic shield, the tunnel extends in a first direction, the first electromagnetic shield and the second electromagnetic shield are perpendicular to the first direction, the first electromagnetic shield applies an electromagnetic force to a first end surface of the car to drive the car to move from the first station to the second station, and the second electromagnetic shield applies an electromagnetic force to a second end surface of the car opposite to the first end surface when the car moves to the second station.
5. The vacuum flying rail transit system of claim 4, wherein the third electromagnetic device comprises a third electromagnetic shield, the third electromagnetic shield being opposite to the second electromagnetic shield, the third electromagnetic shield and the second electromagnetic shield forming the first compartment space therebetween, the third electromagnetic shield applying an electromagnetic force to the first end surface of the car when the car moves from the first station to the second station, so that the car reciprocally decelerates and displaces to a stop in the first compartment space in the first direction.
6. The vacuum flying rail transit system of claim 5, wherein the third electromagnetic device further comprises a first displacement mechanism, the first displacement mechanism is connected with the third electromagnetic shield, and the first displacement mechanism is used for controlling the displacement of the third electromagnetic shield so as to enable the second separated space to be communicated with or closed off the tunnel.
7. The vacuum flying rail transit system of claim 4, wherein the first end surface and the second end surface are planar and parallel to each other, the car further comprises a plurality of side surfaces connected to the first end surface and the second end surface, the plurality of side surfaces, the first end surface and the second end surface enclose a car space for carrying passengers, and the cross section of the car in the first direction is rectangular.
8. The vacuum flying rail transit system of claim 7, wherein the number of the sides is 3, and in a second direction perpendicular to the first direction, the cross section of the car is a first triangle, and the cross section of the tunnel is a second triangle, and the first triangle corresponds to the second triangle.
9. The vacuum flying rail transit system of claim 8, wherein the inner wall of the tunnel comprises a bottom wall and two side walls, and the magnetic levitation device is disposed on both the bottom wall and the side walls.
10. The vacuum flying rail transit system of claim 1, wherein the first station and the second station are provided with a lifting system, one end of the lifting system is connected with the first station or the second station, and the other end of the lifting system protrudes from a moon list.
CN201911237646.0A 2019-12-05 2019-12-05 Lunar-based constant-temperature layer underground vacuum flight track traffic system Pending CN110775074A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114765977A (en) * 2019-09-11 2022-07-19 阿纳托利·爱德华多维奇·尤尼茨基 Method for manufacturing and arranging Eunitz-based ultra-high-speed transportation complex

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114765977A (en) * 2019-09-11 2022-07-19 阿纳托利·爱德华多维奇·尤尼茨基 Method for manufacturing and arranging Eunitz-based ultra-high-speed transportation complex

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Application publication date: 20200211