WO2018184519A1 - 用山体做支架、尽自然本力为动力的发射器及运输装置 - Google Patents

用山体做支架、尽自然本力为动力的发射器及运输装置 Download PDF

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Publication number
WO2018184519A1
WO2018184519A1 PCT/CN2018/081700 CN2018081700W WO2018184519A1 WO 2018184519 A1 WO2018184519 A1 WO 2018184519A1 CN 2018081700 W CN2018081700 W CN 2018081700W WO 2018184519 A1 WO2018184519 A1 WO 2018184519A1
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Prior art keywords
tray
pipe
sealing
piston
sealed
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PCT/CN2018/081700
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English (en)
French (fr)
Inventor
程建评
Original Assignee
程建评
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Publication date
Application filed by 程建评 filed Critical 程建评
Priority to CN201880004106.5A priority Critical patent/CN110198892A/zh
Publication of WO2018184519A1 publication Critical patent/WO2018184519A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
    • B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G5/00—Ground equipment for vehicles, e.g. starting towers, fuelling arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/052—Means for securing the rocket in the launching apparatus
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F7/00—Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots

Definitions

  • the invention relates to the field of aerospace and the field of transportation technology, in particular to an emitter and a transport device powered by a mountain body and powered by natural forces.
  • the existing aeronautical launching device is a rocket launcher, which enables the rocket (aircraft) to be stabilized on the launching frame before launching. It simply uses the reaction force of the burning material injected by the rocket to ignite the aircraft and overcomes the gravity and air friction of the aircraft. .
  • the disadvantage is that the power booster cannot be generated and cannot be made very large.
  • the dense atmosphere at six or seven kilometers above sea level also generates huge friction for high-speed aircraft.
  • the cost of the aircraft is expensive, and the launch is greatly affected by meteorological conditions. The operation is extremely unstable and prone to accidents. It consumes its own prematurely. Conquering the cosmic combustion of the reaction, eventually making the aircraft fly fast and not far.
  • the technical problem to be solved by the present invention is to provide a launcher and a transport device that use a mountain as a support and a natural force as a power, which can effectively utilize atmospheric pressure as a power, improve the stability of the launch of the aircraft, and reduce the difficulty of transportation.
  • a transmitter that uses a mountain as a support and a natural force as a power, and includes a sealed pipe with a smooth inner wall of the mountain body, the sealed pipe is from the bottom of the mountain to the mountain
  • the mountain peak extends in the direction of the mountain
  • the bottom end of the sealing pipe is closed
  • the inner wall of the sealing pipe is provided with a guide rail extending along the length of the sealing pipe
  • the piston pipe assembly is arranged in the sealing pipe.
  • the piston tray assembly being disposed on a side of the pressure pusher away from a bottom end of the sealing pipe, a periphery of the piston tray assembly and a periphery of the pressure pusher and the sealed pipe
  • the inner wall seal is movably connected, and the piston tray assembly and the pressure pusher are both slidably connected to the guide rail;
  • the top end of the sealing duct is open and provided with a top valve for opening and closing the top end opening of the sealed pipe;
  • the tube wall of the sealed pipe is provided with a plurality of drums for feeding outside air into the sealed pipe or sending air from the sealed pipe.
  • a wind device a plurality of the air blowing devices are spaced apart along a length direction of the sealing pipe; an electric current conductor is fixed on the piston type tray assembly, and an outer wall of the sealing pipe is provided for applying the electric current conductor
  • An electromagnetic generating device for electromagnetic force of the bottom end of the sealing pipe toward the top end of the sealing pipe, the top valve, the air blowing device, the energizing conductor, and the electromagnetic generating device are all controlledly connected to the controller, The controller controls opening and closing of the top valve, the air blowing device, the energizing conductor, the electromagnetic generating device, and adjusting an air blowing direction of the air blowing device.
  • a traction device for securing and releasing the aircraft, the periphery of the traction device being slidably coupled to the rail, the traction device being provided with the energization conductor.
  • the advantageous effect of using the above further solution is that the arrangement of the traction device can ensure the stability of the aircraft during the movement in the sealed duct, and the electromagnetic force received by the aircraft is increased due to the energizing conductor on the traction device. More conducive to the launch of the aircraft.
  • the invention has the beneficial effects that the invention utilizes the mountain body as a natural support, uses atmospheric pressure difference and electromagnetic force as power, utilizes the atmospheric pressure difference between the low altitude area and the high altitude area (or even the quasi-vacuum), and the pressure difference generated by the air blown by the air blower.
  • the sealed pipe is discharged to realize the launch of the aircraft.
  • the sealing pipe is built from the bottom of the mountain to the mountain, and the mountain base is fully utilized to ensure that the sealed pipe is stably gripped inside the mountain or on the cliff, and the bottom end of the sealed pipe is from the relatively low altitude to the high altitude.
  • the atmospheric pressure difference between the low-altitude area and the high-altitude area (or even the quasi-vacuum) and the air pressure difference generated by the air blown by the air blowing device pushing the aircraft running along the inside of the sealed pipe to help the aircraft overcome its own gravity when it rises, and in the aircraft There is a certain initial velocity when leaving the upper end of the pipe.
  • the number of the guide rails is two or more, and two or more of the guide rails are disposed in parallel with each other.
  • the guide rail and the piston-type tray assembly are connected by magnetic levitation.
  • the electromagnetic generating device is a set of two first electric wire sets extending along a length direction of the sealing pipe, and two sets of the first electric wire sets are arranged in parallel, and two sets of the first electric wire sets are located at On the opposite outer wall of the sealed pipe, and the currents on the first electric wire sets of the two groups are direct current and the current directions are opposite; the energizing conductor is a vertical setting of the wires connecting the two sets of the first electric wire sets Two electric wire sets. According to Ampere's law and right-hand rule, a magnetic field is generated between the two sets of first electrical conductor sets.
  • the current direction of the second electrical conductor set When the current direction of the second electrical conductor set is perpendicular to the direction of the magnetic field, the current direction of the two sets of first-point conductor sets can be adjusted.
  • the second set of electrical conductors is subjected to an upward force to urge the piston tray assembly and the pressure pusher to move toward the upper end of the sealed conduit along the length of the sealed conduit.
  • the air blowing device located under the piston tray assembly and the pressure pushing device supplies air into the sealed pipe. Increasing the air pressure of the piston tray assembly and the pressure pipe of the pressure pusher.
  • the air blowing device located above the piston tray assembly and the pressure pusher draws air into the sealed pipe to reduce the piston tray assembly and the upper end of the pressure pusher. Air pressure provides power to push the piston tray assembly and the pressure pusher.
  • the present invention can also be improved as follows:
  • the aircraft is placed on the piston-type pallet assembly, and then the upper end of the aircraft is fixedly supported by the traction device, and the piston-type pallet assembly drives the aircraft to closely slide along the inner guide rail of the pipe.
  • the pressure pusher is provided with a pusher valve for communicating the upper and lower spaces of the pressure pusher;
  • the piston tray assembly is provided with a tray valve for communicating the upper and lower spaces of the piston tray assembly;
  • the valve and the tray valve are both in controllable connection with the controller, the controller controlling the opening and closing of the pusher valve and the tray valve.
  • the beneficial effect of using the above further solution is that the setting of the pusher valve and the tray valve enables adjustment of the air pressure at both ends of the sealed pipe.
  • the piston type tray assembly includes a tray A and a tray B, and the tray A and the tray B are respectively provided with the energization conductor, and the periphery of the tray A and the tray B are respectively sealed with the sealed pipe
  • the inner wall is sealingly connected and is slidably connected to the rail, the tray A is disposed between the tray B and the pressure pusher, and the tray valve is disposed on the tray A and the tray B .
  • the piston tray assembly includes a tray A and a tray B, which facilitates the provision of an explosion pushing device between the two.
  • an explosion pushing device for generating an instantaneous impact force on the tray B after the explosion is provided between the tray A and the tray B, and the explosion pushing device is connected to the controller, and the controller controls the The opening of the explosion pushing device.
  • the beneficial effect of using the above further solution is that the setting of the explosion pushing device can instantly increase the impact force on the tray B at the time of starting, so that the aircraft on the tray B can generate greater acceleration, which is advantageous for the launch of the aircraft.
  • each of the air blowing devices being provided with the sensor, the sensor being connected to the controller data, the sensor Information about whether the detected aircraft passed is transmitted to the controller.
  • the advantage of using the above further solution is that the setting of the sensor monitors whether the aircraft passes in real time, thereby facilitating the controller to control the air blowing device to achieve the adjustment of the air pressure.
  • the upper end of the sealed pipe is vertically disposed.
  • the advantage of using the above further solution is that the vertical arrangement of the upper end of the sealing duct enables the aircraft to have a greater centrifugal force after it has disengaged from the sealed duct, facilitating the escape of the aircraft from the earth.
  • the air blowing device at the upper portion of the closed duct and the air blowing device at the lowest end are provided with a water switch for injecting or pumping water into the closed duct, and the controller is connected to the water switch control The controller controls the opening and closing of the water switch. Specifically, a total of four water switches are arranged side by side at the top three and the lowest one of the airtight devices of the closed pipe, controlled by the controller, and water is supplied and pumped between the piston tray assemblies.
  • the above-mentioned further solution has the beneficial effects of: melting the rich ice and snow on the mountain and adding it between the piston tray assemblies, so that the lifting device, the pressure pusher and the piston tray assembly after the completion of the launch are removed, except for their own weight.
  • the air in the closed pipe can be skillfully removed by the weight of the snow water melted on the mountain to become a quasi-vacuum, and the molten snow water is discharged at the lowest altitude at the beginning of the previous launch.
  • the blasting port for the air blowing device for air supply and air exhausting disposed outside the closed pipe adopts an elongated shape, and the valve for switching the blast port is also controlled by the controller along the elongated blast port. Open and close along the length of the closed pipe.
  • the beneficial effect of adopting the above further solution is that because the aircraft is running forward at a high speed in a closed pipe, the long air vent and the valve that opens and closes in the longitudinal direction can feed the wind relatively evenly or Take out.
  • the technical problem to be solved by the present invention is to provide a transportation device that realizes the transportation of goods at a high altitude, and uses the pressure difference between the atmospheric pressure and the electromagnetic force to realize the carriage of the goods with the mountain body as a support and the natural force as the power.
  • a transport device that uses a mountain body as a support and a natural force as a power, and includes a smooth sealed pipe with a mountain body as a support, and the bottom end of the sealed pipe is closed.
  • a guide rail extending along a length of the sealing pipe is disposed on an inner wall of the sealing pipe, and a piston tray assembly and a pressure pusher are disposed in the sealing pipe, and the piston tray assembly is disposed on the pressure pusher a side of the piston tray assembly and a periphery of the pressure pusher are sealingly movably connected to an inner wall of the sealing duct, the piston tray assembly and the pressure pusher, away from a side of the bottom end of the sealing pipe Slidingly connected to the guide rail;
  • the top end of the sealing pipe is open and provided with a top valve for opening and closing the top opening of the sealing pipe;
  • the sealing pipe is provided with a plurality of holes for the outside air a blower device fed into the sealed duct or sending air out of the sealed duct, a plurality of the blower devices along the length of the sealed duct Separatingly disposed;
  • the piston tray assembly is fixed with an energizing conductor, and an outer wall of the sealing duct is provided with an electromagnetic force
  • the advantage of using the above further solution is that the push of the piston tray assembly and the pressure pusher is achieved by the atmospheric pressure difference and the electromagnetic force, thereby realizing the conveyance of the cargo on the piston tray assembly and the pressure pusher.
  • the sealing pipe is provided with a plurality of pick-up ports for opening the side wall of the sealing pipe, and the pick-up port is provided with a pick-up door for opening or closing the pick-up port.
  • the beneficial effect of using the above further solution is that the setting of the pick-up door facilitates the extraction of the conveyed goods at the set location.
  • FIG. 1 is a schematic structural view of a transmitter using a mountain as a support and a natural force as a power;
  • FIG. 2 is a schematic view showing the inside of a transmitter using a mountain as a support and a natural force as a power;
  • FIG. 3 is a schematic structural view of a transport device using a mountain as a support and a natural force as a power;
  • FIG. 4 is a schematic structural view of another embodiment of a transmitter using a mountain body as a support and a natural force as a power;
  • FIG. 5 is a schematic structural view of another embodiment of a transport device using a mountain as a support and a natural force as a power;
  • G 1 , G 2 , G 3 , . . . , G m , G m+1 in the drawing indicate the position at which the air blowing device is mounted on the sealed pipe;
  • Gm+1, Gm, Gm-1 and G1 are arranged at four places in parallel with the air blowing device to set a water switch that opens into the inside of the closed pipe;
  • V 1 is the initial stage of launching flight
  • V 2 is the flying phase of the launching aircraft
  • M is the starting point of the aircraft entering the flying phase. Specifically, M is located between G m and G m+1 .
  • the transmitter that uses the mountain body as a support and the natural force as the power includes a sealed pipe 1 with a smooth inner wall of the mountain body, in this
  • the altitude of the mountain body exceeds 3,000 meters, and the mountain body to which the sealed pipe 1 is attached cannot be a steep cliff, which would otherwise affect the support of the sealed pipe 1.
  • the sealed pipe 1 is an arc-shaped pipe structure; the bottom end to the top end of the sealed pipe 1 extends from a relatively low altitude to a high altitude region, preferably from the bottom of the mountain to the mountain peak, and the mountain base is fully utilized.
  • the supporting action is such that the sealing pipe 1 is stably gripped inside the mountain or on the cliff, and the bottom end of the sealing pipe 1 is closed;
  • the inner wall of the sealing pipe 1 is provided with a guide rail 2 extending along the longitudinal direction of the sealing pipe 1, and the guide rail 2 extends from the bottom end of the sealing pipe 1 to the top end of the sealing pipe 1, the guide rail 2
  • the number of the guide rails 2 is two or more, and the two of the sealed pipes 1 are provided with a piston tray assembly 3 and a pressure pusher 4, which can be the mechanical force generated by the motor, but Preferably, it is electromagnetically driven, the piston tray assembly 3 is disposed on a side of the pressure pusher 4 away from the bottom end of the sealing duct 1, the periphery of the piston tray assembly 3 and the pressure pusher 4
  • the periphery is sealed and movably connected to the inner wall of the sealing pipe 1, and the piston tray assembly 3 and the pressure pusher 4 are slidably coupled to the guide rail 2, preferably, the piston tray assembly 3 and the The pressure pushers 4 are all magnetically connected to the guide rail 2, and the piston tray assembly 3 and the pressure pusher 4 are movable back and forth along
  • the top of the sealing pipe 1 is provided with a top valve 5 for opening and closing the top opening of the sealing pipe 1; the pipe wall of the sealing pipe 1 is provided with a plurality of holes for feeding outside air into the sealing pipe 1 Or the air blowing device 6 that sends out the air in the sealing pipe 1, and the air blowing device 6 can also seal the outer wall of the sealing pipe 1 where the air blowing device 6 is located, and the air blowing device 6 is increased when it is opened.
  • the air pressure in the sealed pipe 1 is reversed to reduce the air pressure in the sealed pipe 1, and the plurality of air blowing devices 6 are arranged along the length direction of the sealing pipe 1; the piston tray assembly 3 is fixed There is an energization conductor 7, and an electromagnetic generating device 8 for applying an electromagnetic force from the bottom end of the sealing duct 1 to the tip end of the sealing duct 1 to the energizing conductor 7 is provided on an outer wall of the sealing duct 1
  • the top valve 5, the air blowing device 6, the energizing conductor 7, the electromagnetic generating device 8, the water switch 19, and the positioner 20 are all connected to a controller (not shown in the drawing).
  • the controller controls the top valve 5, the blast The device 6, the energization conductor 7, the opening and closing of the electromagnetic generating device 8, and the blast direction of the air blowing device 6. Utilizing the atmospheric pressure difference between low altitude and high altitude, the aircraft running along the inside of the sealed pipe 1 is pushed to help the aircraft overcome its own gravity when it rises, and there is an initial velocity when the aircraft leaves the upper end of the sealed pipe 1.
  • a traction device 10 for securing and releasing the aircraft, the periphery of the traction device 10 being slidably coupled to the guide rail 2, the traction device 10 being provided with the energization conductor 7.
  • the traction device 10 enables traction fixation of the aircraft to prevent bump instability when the aircraft is moved by the piston tray assembly 3.
  • the positioner 20 is a set of means for respectively securing the piston tray assembly 3 and the pressure pusher 4 at the take-off position of the aircraft 9.
  • the pressure pusher 4 is provided with a pusher valve 11 for communicating the upper and lower spaces of the pressure pusher 4; the piston tray assembly 3 is provided with a tray valve 12 for communicating the upper and lower spaces of the piston tray assembly 3
  • the pusher valve 11 and the tray valve 12 are both in control connection with the controller, the controller controls opening and closing of the pusher valve 11 and the tray valve 12, the pusher valve 11 and the tray
  • the arrangement of the valve 12 enables adjustment of the air pressure across the sealed conduit 1.
  • the piston tray assembly 3 includes a tray A3-1 and a tray B3-2, and the tray A3-1 and the tray B3-2 are respectively provided with the energization conductor 7, the tray A3-1 and the
  • the periphery of the tray B3-2 is sealingly connected to the inner wall of the sealing pipe 1, and is slidably connected to the guide rail 2, and the tray A3-1 is disposed on the tray B3-2 and the pressure pusher 4.
  • the tray valve 12 is disposed on both the tray A3-1 and the tray B3-2.
  • An explosion pushing device 13 is disposed between the tray A3-1 and the tray B3-2.
  • the explosion pushing device 13 is an explosive
  • the controller controls the connection, and the controller controls the opening of the explosion pushing device 13.
  • the setting of the explosion pushing device 13 can instantaneously increase the impact force on the tray B3-2 at the time of starting, so that the aircraft on the tray B3-2 can generate greater acceleration, which is advantageous for the launch of the aircraft.
  • a bottom portion of the sealed duct 1 is provided with an aircraft (object) port 18 communicating with the inner cavity of the sealed duct 1, in which the aircraft is installed ( At the mouth 18 is provided an aircraft door 17 for closing and opening the aircraft port 18.
  • the electromagnetic generating device 8 is a set of two sets of first electric wires extending along the longitudinal direction of the sealed pipe 1, and two sets of the first electric wire sets are arranged in parallel, and the two sets of the first electric wire sets are Located on the opposite outer wall of the sealed pipe 1, and the current directions on the two sets of the first electric wire sets are opposite; the energizing conductor 7 is a vertical arrangement of the two sets of the first electric wire sets. Two electric wire sets. According to Ampere's law and right-hand rule, a magnetic field is generated between the two sets of first electrical conductor sets. When the current direction of the second electrical conductor set is perpendicular to the direction of the magnetic field, the current direction of the two sets of first-point conductor sets can be adjusted.
  • the second electrical lead set is subjected to an upward force to urge the piston tray assembly 3 to move toward the upper end of the sealed duct 1 along the length of the sealed duct 1.
  • the guide rail 2 is a conductive rail 2
  • the rail 2 is electrically connected thereto
  • the second electric conductor group is connected to the guide rail 2 to realize the second electric conductor group.
  • Conductive Two sets of said direct currents of opposite current directions are applied to the first electric wire set, and the piston type pallet assembly 3 and the energizing conductor 7 on the traction device 10 (the second electric wire group having the same current direction) are worked.
  • An upward power is generated perpendicular to the inner wall of the sealing duct 1 to drive the piston tray assembly 3, the pressure pusher 4, the traction device 10, and the aircraft to operate.
  • a sensor 14 mounted at the blower device 6 for detecting whether an aircraft has passed, the sensor 14 being in data communication with the controller, the sensor 14 transmitting information of whether the detected aircraft passed or not Controller.
  • the sealed pipe 1 is a vertically disposed structure.
  • the sealed pipe 1 is a combined pipe composed of a plurality of arcs.
  • the present invention also discloses a transport device that uses a mountain body as a support and is powered by natural forces, and includes a sealed pipe 1 having a smooth inner wall with a mountain body as a support, and the bottom end of the sealed pipe 1 is closed.
  • the inner wall of the sealing pipe 1 is provided with a guide rail 2 extending along the longitudinal direction of the sealing pipe 1, and the sealing pipe 1 is provided with a piston tray assembly 3 and a pressure pusher 4, and the piston tray assembly 3 is disposed on a side of the pressure pusher 4 away from the bottom end of the sealing pipe 1, the periphery of the piston tray assembly 3 and the periphery of the pressure pusher 4 are sealingly connected with the inner wall of the sealing pipe 1
  • the piston tray assembly 3 and the pressure pusher 4 are both slidably connected to the guide rail 2;
  • the top of the sealing duct 1 is provided with a top valve 5 for opening and closing the top opening of the sealed duct 1;
  • the pipe wall of the sealing pipe 1 is provided with a plurality of air blowing devices 6 for feeding outside air into the sealing pipe 1 or sending air in the sealing pipe 1, and the plurality of the air blowing devices 6 are along Length interval of sealed pipe 1
  • the piston tray assembly 3 is fixed with an energizing conductor 7 on the outer
  • the pushing of the piston tray assembly 3 and the pressure pusher 4 is effected by the atmospheric pressure difference and the electromagnetic force, thereby realizing the conveyance of the cargo on the piston tray assembly 3 and the pressure pusher 4.
  • the sealing pipe 1 is provided with a plurality of pick-up ports 15 for opening the side wall of the sealing pipe 1, and the pick-up port 15 is provided with a pick-up door for opening or closing the pick-up port 15. 16.
  • the setting of the pick-up door 16 facilitates the extraction of the conveyed goods at the set location.
  • the modified launching aircraft is a transport device for transporting goods, and it is not necessary to provide an explosive device, and a piston type pallet can be separately constructed, or the electromagnetic generating device 8 and the energizing conductor 7 need not be provided, and the ordinary motor is replaced. Traction, or the need for the magnetic levitation rail 2 as the ordinary guide rail 2, mainly using the atmospheric pressure difference, can generate the driving force to transport the goods from the low altitude to the high altitude area, that is, the goods are transported to the take-out port 15 of the sealed pipe 1 And take it out.
  • the aircraft is stationary and ready to fly
  • the stationary of the aircraft the current on the first electrical conductor set is turned off, the aircraft door 17 is opened, and the prepared aircraft is placed from the loading aircraft port 18 onto the tray B3-2 resting at the bottom end of the sealed pipe 1 through the traction.
  • the device 10 is fixed, and the tray B3-2, the tray A3-1 and the pressure pusher 4 are positioned by the positioner 20, the pressure pusher 4 is disposed at the bottom end of the sealed pipe 1, and the aircraft door 17 is closed; interval between the tray 4 and the pressure pusher A3-1, A3-1 of the tray between the pusher 4 is provided with a pressure air column connected to the outside by blowing means 6 is located at position G 1
  • the air blowing device 6 that communicates with the air column is in a closed state, so that the tray A3-1, the tray B3-2, and the flying device fixed to the tray B3-2 are stationary.
  • the tray A3-1 and the tray B3-2 can drive the aircraft to open, the current switch on the traction conductor 10, the tray A3-1 and the energized conductor 7 on the tray B3-2 (ie the second electrical conductor group) is opened.
  • the electromagnetic force generated by the electromagnetic generating device 8 ie, the first electrical conductor set
  • the aircraft enters the initial flight phase V 1 , and the positions of the specific V 1 and V 2 are as shown in FIG.
  • the tray and the tray A3-1 B3-2 run up past the blowing means located at the G 2 6, 14 receives information from the sensor at the blowing means 6 located at the G 2, and transmits the information to the controller, control system
  • the air blowing device 6 at the control G 2 is opened to increase the air pressure in the space of the sealed pipe 1 below the tray A3-1.
  • the tray A3-1 and the tray B3-2 are run upwards, they are sequentially located at the G 3 .
  • the air blowing device 6 is at G 4 , ⁇ , G m
  • the sensor 14 corresponding to the position transmits a signal
  • the controller controls the opening of the air blowing device 6 at the corresponding position, continuously communicates with the outside, and replenishes the air. Thereby supplementing the air pressure.
  • the top valve 5, the tray A3-1 and the tray valve 12 of the tray B3-2 are closed, located at G 1 , G 2 , G 3 , G 4 , ⁇ , G m ,
  • the air blowing device 6 at G m+1 is opened, and the trays B3-2 and A3-1 are respectively operated up and down at Gm+1 under electromagnetic force, and are arranged side by side with the air blowing device at Gm+1.
  • Water switch 19 injects water between the trays B3-2 and A3-1, the traction device 10, the tray A3-1 and the tray B3-2, the pressure pusher 4 and the water under their gravity, they are along the guide rail 2 slowly descend to the bottom end of the sealed pipe 1, while discharging the air in the closed pipe through the air blowing device 6 at Gm, Gm-1, Gm-2 ⁇ ; when the pallet A3-1 runs to Gm+1 At the end of the Gm+1, the air blowing device 6 is closed; similarly, the air blowing device 6 at the Gm, Gm-1, ..., G3, and G2 is sequentially closed, and the water switch 19 disposed at the Gm and Gm-1 is respectively placed on the tray. Water is added between A3-1 and B3-2.
  • the positioner 20 is opened, the tray A3-1 and the pressure pusher 4 are positioned, and the water switch at the G1 is set. 19 withdraw the water between the trays A3-1 and B3-2, Finally, the tray B3-2 is positioned, and during the entire lowering process, the discharge of air in the closed duct is realized, and a vacuum is drawn.
  • the launching device of the present invention subverts the function of the launching frame of the current rocket launching device, and the biggest feature is that it dares to use the high-altitude mountain peak as the launching frame and the atmospheric pressure as the power.
  • the mountain is steep and the air is thin.
  • the theoretical calculation of Mount Everest is only about 300 hectopascals.
  • the depth of the mountain gully is deep; the lowest Turpan basin in the west is 154 meters below sea level, and the atmospheric pressure is much larger than 1 Standard atmospheric pressure. If it is built on the mountain, it will use the Everest as a support for the use of the Everest.
  • the aeronautical launcher with a radius of more than 7 meters will be converted into a kiloton of lift only by the atmospheric pressure of nature.
  • an aeronautical launcher with a radius of more than 10 meters is built (only 2,198 tons of atmospheric lift), hundreds of thousands of tons of aircraft will be easily transported to Earth orbit, the moon, and even Mars.
  • the invention also discloses a transport device which uses a mountain body as a support and uses natural force as a power.
  • the launch aircraft is a transport cargo device, because no ultra-high speed is required, the flight device can be omitted.
  • This cargo transport device can provide a new method for transporting goods in mountainous areas with extremely long distances and steep slopes. In the process of building in the mountains, the sealed pipes 1 that pass through the mountains can be built more gently.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
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  • Mechanical Engineering (AREA)
  • Non-Mechanical Conveyors (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
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Abstract

一种用山体做支架、尽自然本力为动力的发射器，包括以山体为支架的内壁光滑的密封管道(1)，密封管道(1)内设有活塞式托盘组件(3)和压力推动器(4)，顶端开口并设有顶部阀门(5)；管壁上设有鼓风装置(6)，活塞式托盘组件(3)上固定有通电导体(7)，密封管道(1)的外壁上设有电磁发生装置(8)。该发射器利用山体作为自然支架，采用大气压强差和电磁力作为动力，利用低海拔地区与高海拔地区的大气压强差以及鼓风机抽送空气产生的压强差，推动飞行器进行移动，将飞行器推送至密封管道的上端，并且赋予飞行器一定的初速度。

Description

用山体做支架、尽自然本力为动力的发射器及运输装置 技术领域
本发明涉及航天航空领域以及运载技术领域，尤其涉及一种用山体做支架、尽自然本力为动力的发射器及运输装置。
背景技术
现有的航空发射装置是火箭发射架，使火箭(飞行器)在发射前，稳定在发射架上，单纯利用火箭点火后喷射的燃烧物质的反作用力，克服飞行器的重力和空气摩擦力而升空。缺点是不能产生动力助推飞行器且不能造得很高大。海拔六、七千米下稠密的大气层也对高速的飞行器产生巨大的摩擦力，飞行器造价昂贵，且发射受气象条件影响大，运行极不平稳且易出事故，过早地消耗了自身携带的征服宇宙的产生反作用力的燃烧物质，最终使飞行器飞不快、飞不远。
现有技术中对于高海拔山体上的货物的运输存在困难，尤其是将物品运输到未开设公路的高山上，当车辆和飞机无法达到时，则难以运输，对高海拔地区的建设以及科研造成困扰。
发明内容
本发明所要解决的技术问题是提供一种用山体做支架、尽自然本力为动力的发射器及运输装置，能有效利用大气压力作为动力，提高飞行器发射的稳定性，并且能降低运输难度。
本发明解决上述技术问题的技术方案如下：一种用山体做支架、尽自然本力为动力的发射器，包括以山体为支架的内壁光滑的密封管道，所述密封管道从山体的山底向山体的山峰方向延伸设置，所述密封管道的底端封闭， 所述密封管道的内壁上设有沿所述密封管道的长度方向延伸设置的导轨，所述密封管道内设有活塞式托盘组件和压力推动器，所述活塞式托盘组件设在所述压力推动器远离所述密封管道底端的一侧，所述活塞式托盘组件的周边以及所述压力推动器的周边均与所述密封管道的内壁密封活动连接，所述活塞式托盘组件和所述压力推动器均与所述导轨滑动连接；所述密封管道的顶端开口并设有用于开启和封盖所述密封管道顶端开口的顶部阀门；所述密封管道的管壁上设有多个用于将外部空气送入密封管道内或将密封管道内的空气送出的鼓风装置，多个所述鼓风装置沿所述密封管道的长度方向间隔设置；所述活塞式托盘组件上固定有通电导体，所述密封管道的外壁上设有用于对所述通电导体施加由所述密封管道的底端向所述密封管道的顶端的电磁力的电磁发生装置，所述顶部阀门、所述鼓风装置、所述通电导体、所述电磁发生装置均与控制器控制连接，所述控制器控制所述顶部阀门、所述鼓风装置、所述通电导体、所述电磁发生装置的开启和关闭，以及调节所述鼓风装置的鼓风方向。
还包括用于固定和松开所述飞行器的牵引装置，所述牵引装置的周边与所述导轨滑动连接，所述牵引装置上设有所述通电导体。
采用上述进一步方案的有益效果是：牵引装置的设置能确保飞行器在密封管道内移动的过程中能保持自身的稳定性，并且由于牵引装置上设有通电导体，增大飞行器所受到的电磁力，更加有利于飞行器的发射。
本发明的有益效果是：本发明利用山体作为自然支架，采用大气压强差和电磁力作为动力，利用低海拔地区与高海拔地区(乃至准真空)的大气压强差以及鼓风机抽送空气产生的压强差，推动密封管道内的活塞式托盘组件沿密封管道的长度方向进行移动，将飞行器推送至密封管道的上端，并且赋予飞行器一定的初速度，然后在飞行器自身动力的作用下以较高的速度冲出密封管道，实现飞行器的发射。
本发明中的密封管道山底到山峰依山建设，充分利用山体基托作用，使密封管道稳定地抓紧在山体内部或峭壁上，密封管道的底端至顶端由相对低海拔到高海拔的地区，利用低海拔地区与高海拔地区(乃至准真空)的大气压力差以及鼓风装置抽送气体产生的气压差，推动沿密封管道内部运行的飞行器，帮助飞行器上升时克服其自身重力，并在飞行器离开管道上端时有一定的初速度。
所述导轨的数量为两个以上，两个以上所述导轨均相互平行设置，优选的，所述导轨与所述活塞式托盘组件通过磁悬浮连接。
所述电磁发生装置为两组沿所述密封管道的长度方向延伸设置的第一电导线组，且两组所述第一电导线组的平行设置，两组所述第一电导线组位于所述密封管道相对的外壁上，且两组所述第一电导线组上的电流为直流电且电流方向相反；所述通电导体为与两组所述第一电导线组的连线垂直设置的第二电导线组。根据安培定律及右手定则，两组第一电导线组之间产生磁场，当第二电导线组的电流方向与磁场方向垂直时，通过调节两组第一点导线组的电流方向，可以使得第二电导线组会受到向上的作用力，从而推动活塞式托盘组件以及所述压力推动器向沿密封管道的长度方向向密封管道的上端移动。
由于密封管道上沿其长度方向设有多个鼓风装置，在活塞式托盘组件以及压力推动器通过鼓风装置后，位于活塞式托盘组件以及压力推动器下方的鼓风装置向密封管道内送气，增大活塞式托盘组件以及压力推动器的密封管道的气压，位于活塞式托盘组件以及压力推动器上方的鼓风装置向密封管道内抽气，减小活塞式托盘组件以及压力推动器上端的气压，提供推动活塞式托盘组件以及压力推动器的动力。
在上述技术方案的基础上，本发明还可以做如下改进：
在所述密封管道内部，将飞行器置于活塞式托盘组件上，然后通过牵引 装置固定套住飞行器的上端，活塞式托盘组件带动飞行器沿管道内部导轨紧密滑动移动。
进一步，所述压力推动器上设有用于连通所述压力推动器上下空间的推动器阀门；所述活塞式托盘组件上设有用于连通所述活塞式托盘组件上下空间的托盘阀门；所述推动器阀门和所述托盘阀门均与所述控制器控制连接，所述控制器控制所述推动器阀门和所述托盘阀门的开启和关闭。
采用上述进一步方案的有益效果是：推动器阀门和托盘阀门的设置能实现对密封管道两端气压的调节。
进一步，所述活塞式托盘组件包括托盘A和托盘B，所述托盘A和所述托盘B上均设有所述通电导体，所述托盘A和所述托盘B的周边均与所述密封管道的内壁密封连接，且均与所述导轨滑动连接，所述托盘A设在所述托盘B与所述压力推动器之间，所述托盘A和所述托盘B上均设有所述托盘阀门。
采用上述进一步方案的有益效果是：活塞式托盘组件包括托盘A和托盘B，能方便在两者之间设置***推动装置。
进一步，所述托盘A和所述托盘B之间设有用于在***后对托盘B产生瞬间冲击力的***推动装置，所述***推动装置与所述控制器控制连接，所述控制器控制所述***推动装置的开启。
采用上述进一步方案的有益效果是：***推动装置的设置能在启动时瞬间增大对托盘B的冲击力，使得托盘B上的飞行器能产生更大的加速度，利于飞行器的发射。
***推动装置启动后产生对托盘B向上的冲击力，使得托盘B3-2带动飞行器更快地运行。
进一步，还包括安装在所述鼓风装置处用于检测飞行器是否经过的传感器，每个所述鼓风装置处均设有所述传感器，所述传感器与所述控制器数据 连接，所述传感器将检测到的飞行器是否经过的信息传输到所述控制器。
采用上述进一步方案的有益效果是：传感器的设置更实时监测飞行器是否通过，从而方便控制器控制鼓风装置实现气压的调节。
进一步，所述密封管道的上端竖直设置。
采用上述进一步方案的有益效果是：密封管道的上端竖直设置能使得飞行器在脱离密封管道后具有更大的离心力，便于飞行器脱离地球。
进一步，所述封闭管道的上部的所述鼓风装置以及最低端的所述鼓风装置处设有用于向所述封闭管道内注水或抽水的水开关，所述控制器与所述水开关控制相连，所述控制器控制所述水开关的开启和关闭。具体的，在密闭管道的最高三个和最低一个鼓风装置处并列设置共四个水开关，受控制器的控制，并对活塞式托盘组件之间进行送水和抽水。
采用上述进一步方案的有益效果是：使高山上丰富的冰雪熔化后，加入活塞式托盘组件之间，使发射完成后的牵引装置、压力推动器、活塞式托盘组件复位过程中，除自身的重量外，还可凭高山上熔化后的雪水的重量，巧妙地把密闭管道内的空气抽走，变成准真空，在上一发射初时的海拔最低处把熔化后的雪水放出去。
进一步，还包括用于间隔设置在所述密闭管道外的送风和抽风的鼓风装置的鼓风口采用长条形形状，开关鼓风口的阀门也沿长条形的鼓风口，受控制器控制，沿密闭管道的长度方向进行开闭。
采用上述进一步方案的有益效果是：因为飞行器在密闭管道内以高速向前运行过程中，采用长条形的鼓风口和沿长度方向进行开闭的阀门就能相对更均匀地把风送进或抽出。
本发明还解决的的技术问题是提供一种实现高海拔的货物的运输，利用气压大气压强差和电磁力实现对货物的运载的用山体做支架、尽自然本力为动力的运输装置。
本发明解决上述技术问题的技术方案如下：一种用山体做支架、尽自然本力为动力的运输装置，包括以山体为支架的内壁光滑的密封管道，所述密封管道的底端封闭，所述密封管道的内壁上设有沿所述密封管道的长度方向延伸设置的导轨，所述密封管道内设有活塞式托盘组件和压力推动器，所述活塞式托盘组件设在所述压力推动器远离所述密封管道底端的一侧，所述活塞式托盘组件的周边以及所述压力推动器的周边均与所述密封管道的内壁密封活动连接，所述活塞式托盘组件和所述压力推动器均与所述导轨滑动连接；所述密封管道的顶端开口并设有用于开启和封盖所述密封管道顶部开口的顶端阀门；所述密封管道的管壁上设有多个用于将外部空气送入密封管道内或将密封管道内的空气送出的鼓风装置，多个所述鼓风装置沿所述密封管道的长度方向间隔设置；所述活塞式托盘组件上固定有通电导体，所述密封管道的外壁上设有用于对所述通电导体施加由所述密封管道的底端向所述密封管道的顶端的电磁力的电磁发生装置，所述顶部阀门、所述鼓风装置、所述通电导体、所述电磁发生装置均与控制器控制连接，所述控制器控制所述顶部阀门、所述鼓风装置、所述通电导体、所述电磁发生装置的开启和关闭，以及调节所述鼓风装置的鼓风方向。
采用上述进一步方案的有益效果是：通过大气压强差和电磁力实现对活塞式托盘组件和压力推动器的推送，从而实现对活塞式托盘组件和压力推动器上的货物的输送。
所述密封管道上设有多个用于打开所述密封管道侧壁的取货口，所述取货口处设有用于打开或封盖所述取货口的取货门。
采用上述进一步方案的有益效果是：取货门的设置能方便在设定地点对输送的货物的提取。
附图说明
图1为本发明一种用山体做支架、尽自然本力为动力的发射器的结构示意图；
图2为本发明一种用山体做支架、尽自然本力为动力的发射器的内部示意图；
图3为本发明一种用山体做支架、尽自然本力为动力的运输装置的结构示意图；
图4为本发明一种用山体做支架、尽自然本力为动力的发射器的另一种实施例的结构示意图；
图5为本发明一种用山体做支架、尽自然本力为动力的运输装置的另一种实施例的结构示意图；
附图中，各标号所代表的部件列表如下：
1、密封管道，2、导轨，3、活塞式托盘组件，3-1、托盘A，3-2、托盘B，4、压力推动器，5、顶部阀门，6、鼓风装置，7、通电导体，8、电磁发生装置，9、飞行器，10、牵引装置，11、推动器阀门，12、托盘阀门，13、***推动装置，14、传感器，15、取货口，16、取货门，17、装飞行器(物)门，18、装飞行器(物)口，19、水开关，20、***。
附图中的G 1、G 2、G 3、···、G m、G m+1表示密封管道上安装有鼓风装置的位置；
Gm+1、Gm、Gm-1和G1四处设置与鼓风装置并列设置通入密闭管道内部的水开关；
附图中V 1为发射飞行的初始阶段，V 2为发射飞行器的飞升阶段；
附图中M处为飞行器进入飞升阶段的起始点，具体的，M处设在G m和G m+1之间。
具体实施方式
以下结合附图对本发明的原理和特征进行描述，所举实例只用于解释本发明，并非用于限定本发明的范围。
如图1、图2所示，本发明的一种实施例中，所述用山体做支架、尽自然本力为动力的发射器，包括以山体为支架的内壁光滑的密封管道1，在本发明中，优选的，山体的海拔超过3000米，并且密封管道1依附的山体不能为陡峭的悬崖，否则会对密封管道1的支承造成影响。优选的，所述密封管道1为弧形管道结构；所述密封管道1的底端至顶端由相对低海拔到高海拔的地区延伸，最好从山底到山峰依山建设，充分利用山体基托作用，使密封管道1稳定地抓紧在山体内部或峭壁上，所述密封管道1的底端封闭；
所述密封管道1的内壁上设有沿所述密封管道1的长度方向延伸设置的导轨2，所述导轨2从所述密封管道1的底端延伸至密封管道1的顶端，所述导轨2的数量为两个以上所述导轨2平行设置，两个所述密封管道1内设有活塞式托盘组件3和压力推动器4，所述压力推动器4即可以是电动机产生的机械力，但最好是电磁力推动的，所述活塞式托盘组件3设在所述压力推动器4远离所述密封管道1底端的一侧，所述活塞式托盘组件3的周边以及所述压力推动器4的周边均与所述密封管道1的内壁密封活动连接，所述活塞式托盘组件3和所述压力推动器4均与所述导轨2滑动连接,优选的，所述活塞式托盘组件3和所述压力推动器4均与所述导轨2磁悬浮连接，所述活塞式托盘组件3和压力推动器4可沿所述导轨2的长度方向来回移动；
所述密封管道1的顶部设有用于开启和封盖所述密封管道1顶部开口的顶部阀门5；所述密封管道1的管壁上设有多个用于将外部空气送入密封管道1内或将密封管道1内的空气送出的鼓风装置6，所述鼓风装置6还能实现对鼓风装置6所处的密封管道1的外壁进行密封，鼓风装置6顺开时，使增加密封管道1内的空气压力，逆开时则减低密封管道1内的空气压力，多个所述鼓风装置6沿所述密封管道1的长度方向间隔设置；所述活塞式托盘 组件3上固定有通电导体7，所述密封管道1的外壁上设有用于对所述通电导体7施加由所述密封管道1的底端向所述密封管道1的顶端的电磁力的电磁发生装置8，所述顶部阀门5、所述鼓风装置6、所述通电导体7、所述电磁发生装置8、所述水开关19、所述***20均与控制器(附图中未画出)控制连接，所述控制器控制所述顶部阀门5、所述鼓风装置6、所述通电导体7、所述电磁发生装置8的开启和关闭，以及调节所述鼓风装置6的鼓风方向。利用低海拔地区与高海拔地区的大气压力差，推动沿密封管道1内部运行的飞行器，帮助飞行器上升时克服其自身重力，并在飞行器离开密封管道1上端时，有个初速度。
还包括用于固定和松开所述飞行器的牵引装置10，所述牵引装置10的周边与所述导轨2滑动连接，所述牵引装置10上设有所述通电导体7。牵引装置10能实现对飞行器的牵引固定，避免飞行器在所述活塞式托盘组件3的带动下移动时颠簸不稳定。
***20是一组在飞行器9起飞位置分别固定活塞式托盘组件3和压力推动器4的装置。
所述压力推动器4上设有用于连通所述压力推动器4上下空间的推动器阀门11；所述活塞式托盘组件3上设有用于连通所述活塞式托盘组件3上下空间的托盘阀门12；所述推动器阀门11和所述托盘阀门12均与所述控制器控制连接，所述控制器控制所述推动器阀门11和所述托盘阀门12的开启和关闭，推动器阀门11和托盘阀门12的设置能实现对密封管道1两端气压的调节。所述活塞式托盘组件3包括托盘A3-1和托盘B3-2，所述托盘A3-1和所述托盘B3-2上均设有所述通电导体7，所述托盘A3-1和所述托盘B3-2的周边均与所述密封管道1的内壁密封连接，且均与所述导轨2滑动连接，所述托盘A3-1设在所述托盘B3-2与所述压力推动器4之间，所述托盘A3-1和所述托盘B3-2上均设有所述托盘阀门12。所述托盘A3-1和所述托盘B3-2 之间设有***推动装置13，在本发明的实施例中，所述***推动装置13为***物，所述***推动装置13与所述控制器控制连接，所述控制器控制所述***推动装置13的开启。***推动装置13的设置能在启动时瞬间增大对托盘B3-2的冲击力，使得托盘B3-2上的飞行器能产生更大的加速度，利于飞行器的发射。
在本发明的实施例中，为了方便将飞行器放置于密封管道1内，在所述密封管道1的底部设有连通所述密封管道1内腔的装飞行器(物)口18，在装飞行器(物)口18处设有用于关闭和开启所述装飞行器(物)口18的装飞行器(物)门17。
所述电磁发生装置8为两组沿所述密封管道1的长度方向延伸设置的第一电导线组，且两组所述第一电导线组的平行设置，两组所述第一电导线组位于所述密封管道1相对的外壁上，且两组所述第一电导线组上的电流方向相反；所述通电导体7为与两组所述第一电导线组的连线垂直设置的第二电导线组。根据安培定律及右手定则，两组第一电导线组之间产生磁场，当第二电导线组的电流方向与磁场方向垂直时，通过调节两组第一点导线组的电流方向，可以使得第二电导线组会受到向上的作用力，从而推动活塞式托盘组件3向沿密封管道1的长度方向向密封管道1的上端移动。为了方便通电导体7的电路连接，所述导轨2为导电导轨2，所述导轨2上通有电流，所述第二电导线组通过与所述导轨2连通实现所述第二电导线组的导电。两组所述第一电导线组内通入电流方向相反的直流电流，对所述活塞式托盘组件3、所述牵引装置10上的通电导体7(电流方向相同的第二电导线组)做工，产生垂直于密封管道1的内壁的向上的动力，带动所述活塞式托盘组件3、所述压力推动器4、所述牵引装置10以及飞行器运行。
还包括安装在所述鼓风装置6处用于检测飞行器是否经过的传感器14，所述传感器14与所述控制器数据连接，所述传感器14将检测到的飞行器是 否经过的信息传输到所述控制器。
如图4所示，在本发明的用山体做支架、尽自然本力为动力的发射器的一种实施例中，所述密封管道1为竖直设置的结构。
如图5所示，在本发明的用山体做支架、尽自然本力为动力的运输装置的一种实施例中，所述密封管道1为由多段弧形组成的组合型管道。
如图3所示，本发明还公开一种用山体做支架、尽自然本力为动力的运输装置，包括以山体为支架的内壁光滑的密封管道1，所述密封管道1的底端封闭，所述密封管道1的内壁上设有沿所述密封管道1的长度方向延伸设置的导轨2，所述密封管道1内设有活塞式托盘组件3和压力推动器4，所述活塞式托盘组件3设在所述压力推动器4远离所述密封管道1底端的一侧，所述活塞式托盘组件3的周边以及所述压力推动器4的周边均与所述密封管道1的内壁密封活动连接，所述活塞式托盘组件3和所述压力推动器4均与所述导轨2滑动连接；所述密封管道1的顶部设有用于开启和封盖所述密封管道1顶部开口的顶部阀门5；所述密封管道1的管壁上设有多个用于将外部空气送入密封管道1内或将密封管道1内的空气送出的鼓风装置6，多个所述鼓风装置6沿所述密封管道1的长度方向间隔设置；所述活塞式托盘组件3上固定有通电导体7，所述密封管道1的外壁上设有用于对所述通电导体7施加由所述密封管道1的底端向所述密封管道1的顶端的电磁力的电磁发生装置8，所述顶部阀门5、所述鼓风装置6、所述通电导体7、所述电磁发生装置8均与控制器控制连接，所述控制器控制所述顶部阀门5、所述鼓风装置6、所述通电导体7、所述电磁发生装置8的开启和关闭，以及调节所述鼓风装置6的鼓风方向。通过大气压强差和电磁力实现对活塞式托盘组件3和压力推动器4的推送，从而实现对活塞式托盘组件3和压力推动器4上的货物的输送。所述密封管道1上设有多个用于打开所述密封管道1侧壁的取货口15，所述取货口15处设有用于打开或封盖所述取货口15的取货门 16。取货门16的设置能方便在设定地点对输送的货物的提取。
在密封管道1内，改发射飞行器为运送货物的运输装置，则可以不需要设置***装置，可以单独建设一个活塞式托盘，或者不需要设置电磁发生装置8和通电导体7，而改为普通电机牵引力，或者不需要磁悬浮导轨2而为普通导轨2，主要利用大气压强差，就可以产生推动力把货物从低海拔地区运至高海拔地区，即把货物运送到密封管道1的取货口15处而取出。
工作原理：
1、飞行器的静止和准备飞行
1.1、飞行器的静止：关闭第一电导线组上的电流，打开装飞行器门17，将准备好的飞行器从装飞行器口18处放入静止在密封管道1底端的托盘B3-2上，通过牵引装置10固定，将托盘B3-2、托盘A3-1以及压力推动器4用***20进行定位，所述压力推动器4设在密封管道1的底端处，关闭装飞行器门17；所述托盘A3-1与所述压力推动器4之间间隔设置，在所述托盘A3-1与所述压力推动器4之间设有通过位于G 1位置的鼓风装置6与外界连通的空气柱，连通该空气柱的鼓风装置6处于关闭状态，使得托盘A3-1、托盘B3-2以及固定在所述托盘B3-2上的飞行装置静止。
1.2、准备飞行：打开顶部阀门5，关闭密封管道1上的所有鼓风装置6和托盘A3-1阀门口12，打开托盘B3-2的阀门12，待密封管道1内的空气从密封管道1的顶端开口排向山峰，使得位于托盘B3-2上方的气压与密封管道1上端口所处外界的气压相同，然后关闭顶部阀门5；逆开位于托盘B3-2上方的所有鼓风装置6，即逆开G 2、G 3、G 4、···、G m、G m+1位置上的所有鼓风装置6，将密封管道1位于托盘B3-2上方的空间内的空气抽出，然后顺开位于G1位置的鼓风装置6，增大压力推动器4的底端与所述密封管道1的底端的气压至多个大气压以上时，关闭G 2、G 3、G 4、···、G m、G m+1位置上的所有鼓风装置6，关闭推动器阀门11，开启两个电磁发生装置8(即所述第一电导 线组)，使得两个所述第一电导线组的电流方向相反，松开压力推动器上的***20，开启压力推动器4，压力推动器4的先运行压缩压力推动器4和托盘A3-1之间的空气，使得压力推动器4和托盘A3-1之间的气压有多个大气压。松开***20，托盘A3-1、托盘B3-2和压力推动器4即可带动飞行器开启运行。
2、飞行器在密封管道1内的持续运行
2.1、托盘A3-1和托盘B3-2即可带动飞行器开启运行后，打开牵引装置10、托盘A3-1和托盘B3-2上的通电导体7(即第二电导线组)上的电流开关，在所述电磁发生装置8(即所述第一电导线组)产生的电磁力的驱动下，飞行器进入飞行初始阶段V 1，具体V 1和V 2的位置如图1所示，当飞行器、托盘A3-1和托盘B3-2向上运行经过位于G 2处的鼓风装置6时，位于G 2处的鼓风装置6处的传感器14接收信息，并将信息传输到控制器，制器控制G 2处的鼓风装置6顺开，加大位于托盘A3-1下方的密封管道1空间的气压，同理，当飞行器、托盘A3-1和托盘B3-2向上运行依次经过位于G 3、G 4、···、G m处的鼓风装置6时，对应位置的传感器14发送信号，通过控制器控制对应位置的鼓风装置6的顺开，不断与外界连通，补充进空气，从而补充气压。
2.2、当飞行器达到位于G m处的鼓风装置6和位于G m+1处的鼓风装置6之间M处后，进入到飞行飞升阶段V 2。当飞行器、托盘A3-1和托盘B3-2达到M处后，***推动装置13起爆，关闭托盘A3-1和压力推动器4上的电流，同时关闭位于G 1、G 2、G 3、G 4、···、G m处的鼓风装置6，***对托盘B3-2产生向上的推动力，托盘B3-2、牵引装置10在电磁力以及***产生的推动力的作用下，带动飞行器在上升阶段飞行，运行到一定的接近密封管道1的顶端处时，提前打开顶部阀门5以及逆开位于G m+1处的鼓风装置6，解开牵引装置10，同时使飞行器点火，托盘B3-2、牵引装置10以及电磁发生装置8(即第一电导线组)上的电流关闭，飞行器反推托盘B3-2，冲出密封管道1 顶端，进入空中飞行。
3、托盘A3-1、托盘B3-2以及牵引装置10的回收：(1)飞行器点火进入空中飞行后，托盘A3-1和托盘B3-2的托盘阀门12均打开，压力推动器4上的推动器阀门11也打开，位于G 1、G 2、G 3、G 4、···、G m、G m+1处的鼓风装置6均关闭，牵引装置10、托盘A3-1和托盘B3-2和压力推动器4在重力作用下，沿导轨2慢慢下坠至密封管道1的底端。(2)飞行器点火进入空中飞行后，顶部阀门5、托盘A3-1和托盘B3-2的托盘阀门12均关闭，位于G 1、G 2、G 3、G 4、···、G m、G m+1处的鼓风装置6均打开，托盘B3-2和A3-1分别在电磁力带动下运行Gm+1处的上和下方，通过与在Gm+1处的鼓风装置并列设置的水开关19向所述托盘B3-2和A3-1之间注入水，牵引装置10、托盘A3-1和托盘B3-2、压力推动器4和水在它们的重力作用下，它们沿导轨2慢慢下坠至密封管道1的底端，同时通过Gm、Gm-1、Gm-2···处的鼓风装置6把封闭管道内的空气排出；当托盘A3-1运行至Gm+1处后Gm+1处鼓风装置6关闭；同理，Gm、Gm-1···G3、G2处鼓风装置6逐次关闭，设置在Gm、Gm-1处的水开关19，分别对托盘A3-1和B3-2之间加水，当托盘A3-1、压力推动器4回到初始位置时，打开***20，对托盘A3-1、压力推动器4定位，通过设置G1处水开关19抽出托盘A3-1和B3-2之间的水，最后对托盘B3-2定位，整个下降过程中，实现了对封闭管道内的空气的排出，就抽成了真空。
本发明的发射装置颠覆了目前火箭发射装置发射架的作用，最大的特点在于敢于利用高海拔的山峰做发射架和转大气压力为动力。没有比珠穆朗玛峰更高的发射架了，山峰险峻空气稀薄、理论计算珠穆朗玛峰约只有300百帕的压强，山底沟壑纵深；西部最低的吐鲁番盆地低于海平面154米，大气压力远大于1个标准大气压。如果依山而建，将因势利导使用珠穆朗玛峰做支架，建半径大于7米的航空发射器，仅凭大自然的大气压力将转化为千吨的升力，升力＝面积*压强差＝3.14*7米*7米 *10000*(1.013kg/cm2-0.3kg/cm2)＝1097吨。如果加上把封闭管道抽成真空、压力推动器4的助推压力、加上电磁力等，火箭上天将极大节约航天发射燃料，实现本发明的作用。如建半径10米以上的航空发射器(仅大气升力有2198吨)，几百上千吨的飞行器将被轻松送上地球卫星轨道、月球、乃至火星。
本发明还公开了一种用山体做支架、尽自然本力为动力的运输装置，在密封管道1内，改发射飞行器为运送货物装置，因为不需要超高速度，则可以不需要飞行装置的托盘A3-1和托盘B3-2之间的***物(或建单片式活塞托盘)，或者不需要电磁推动力而为普通电机牵引力，或者不需要磁悬浮导轨而为普通导轨，主要利用大气压强差，就可以把货物从低海拔地区运至高海拔地区，把货物运送到密封管道1的中部取货口15而取出。这种货物运送装置，可以为超长距离、陡峭坡度的山地运输货物提供一种新方法，在依山而建的过程中，穿山越岭的密封管道1，更可以建得平缓些。
以上所述仅为本发明的较佳实施例，并不用以限制本发明，凡在本发明的精神和原则之内，所作的任何修改、等同替换、改进等，均应包含在本发明的保护范围之内。

Claims (9)

  1. 一种用山体做支架、尽自然本力为动力的发射器，其特征在于，包括以山体为支架的内壁光滑的密封管道(1)，所述密封管道(1)的底端封闭，所述密封管道(1)的内壁上设有沿所述密封管道(1)的长度方向延伸设置的导轨(2)，所述密封管道(1)内设有活塞式托盘组件(3)和压力推动器(4)，所述活塞式托盘组件(3)设在所述压力推动器(4)远离所述密封管道(1)底端的一侧，所述活塞式托盘组件(3)的周边以及所述压力推动器(4)的周边均与所述密封管道(1)的内壁密封活动连接，所述活塞式托盘组件(3)和所述压力推动器(4)均与所述导轨(2)滑动连接；
    所述密封管道(1)的顶端开口并设有用于开启和封盖所述密封管道(1)顶端开口的顶部阀门(5)；
    所述密封管道(1)的管壁上设有多个用于将外部空气送入密封管道(1)内或将密封管道(1)内的空气送出的鼓风装置(6)，多个所述鼓风装置(6)沿所述密封管道(1)的长度方向间隔设置；
    所述活塞式托盘组件(3)上固定有通电导体(7)，所述密封管道(1)的外壁上设有用于对所述通电导体(7)施加由所述密封管道(1)的底端向所述密封管道(1)的顶端的电磁力的电磁发生装置(8)；
    所述顶部阀门(5)、所述鼓风装置(6)、所述通电导体(7)、所述电磁发生装置(8)均与控制器控制连接，所述控制器控制所述顶部阀门(5)、所述鼓风装置(6)、所述通电导体(7)、所述电磁发生装置(8)的开启和关闭，以及调节所述鼓风装置(6)的鼓风方向。
  2. 根据权利要求1所述的一种用山体做支架、尽自然本力为动力的发射器，其特征在于，还包括用于固定和松开飞行器的牵引装置(10)，所述牵引装置(10)的周边与所述导轨(2)滑动连接，所述牵引装置(10)上设有所述通电导体(7)。
  3. 根据权利要求1所述的一种用山体做支架、尽自然本力为动力的发射器，其特征在于，所述压力推动器(4)上设有用于连通所述压力推动器(4)上下空间的推动器阀门(11)；所述活塞式托盘组件(3)上设有用于连通所述活塞式托盘组件(3)上下空间的托盘阀门(12)；所述推动器阀门(11)和所述托盘阀门(12)均与所述控制器控制连接，所述控制器控制所述推动器阀门(11)和所述托盘阀门(12)的开启和关闭。
  4. 根据权利要求3所述的一种用山体做支架、尽自然本力为动力的发射器，其特征在于，所述活塞式托盘组件(3)包括托盘A(3-1)和托盘B(3-2)，所述托盘A(3-1)和所述托盘B(3-2)上均设有所述通电导体(7)，所述托盘A(3-1)和所述托盘B(3-2)的周边均与所述密封管道(1)的内壁密封连接，且均与所述导轨(2)滑动连接，所述托盘A(3-1)设在所述托盘B(3-2)与所述压力推动器(4)之间，所述托盘A(3-1)和所述托盘B(3-2)上均设有所述托盘阀门(12)。
  5. 根据权利要求4所述的一种用山体做支架、尽自然本力为动力的发射器，其特征在于，所述托盘A(3-1)和所述托盘B(3-2)之间设有用于在***后对托盘B(3-2)产生瞬间冲击力的***推动装置(13)，所述***推动装置(13)与所述控制器控制连接，所述控制器控制所述***推动装置(13)的开启。
  6. 根据权利要求1至5任一项所述的一种用山体做支架、尽自然本力为动力的发射器，其特征在于，还包括安装在所述鼓风装置(6)处用于检测飞行器是否经过的传感器(14)，所述传感器(14)与所述控制器数据连接，所述传感器(14)将检测到的飞行器是否经过的信息传输到所述控制器。
  7. 根据权利要求1至5任一项所述的一种用山体做支架、尽自然本力为动力的发射器，其特征在于，所述密封管道(1)的上端竖直设置。
  8. 根据权利要求1至5任一项所述的一种用山体做支架、尽自然本力为动力的发射器，其特征在于，所述封闭管道(1)的上部的所述鼓风装置(6) 以及最低端的所述鼓风装置(6)处设有用于向所述封闭管道(1)内注水或抽水的水开关(19)，所述控制器与所述水开关(19)控制相连，所述控制器控制所述水开关(19)的开启和关闭。
  9. 一种用山体做支架、尽自然本力为动力的运输装置，其特征在于，包括以山体为支架的内壁光滑的密封管道(1)，所述密封管道(1)的底端封闭，所述密封管道(1)的内壁上设有沿所述密封管道(1)的长度方向延伸设置的导轨(2)，所述密封管道(1)内设有活塞式托盘组件(3)和压力推动器(4)，所述活塞式托盘组件(3)设在所述压力推动器(4)远离所述密封管道(1)底端的一侧，所述活塞式托盘组件(3)的周边以及所述压力推动器(4)的周边均与所述密封管道(1)的内壁密封活动连接，所述活塞式托盘组件(3)和所述压力推动器(4)均与所述导轨(2)滑动连接；所述密封管道(1)的顶端开口并设有用于开启和封盖所述密封管道(1)顶端开口的顶部阀门(5)；所述密封管道(1)的管壁上设有多个用于将外部空气送入密封管道(1)内或将密封管道(1)内的空气送出的鼓风装置(6)，多个所述鼓风装置(6)沿所述密封管道(1)的长度方向间隔设置；所述活塞式托盘组件(3)上固定有通电导体(7)，所述密封管道(1)的外壁上设有用于对所述通电导体(7)施加由所述密封管道(1)的底端向所述密封管道(1)的顶端的电磁力的电磁发生装置(8)，所述顶部阀门(5)、所述鼓风装置(6)、所述通电导体(7)、所述电磁发生装置(8)均与控制器控制连接，所述控制器控制所述顶部阀门(5)、所述鼓风装置(6)、所述通电导体(7)、所述电磁发生装置(8)的开启和关闭，以及调节所述鼓风装置(6)的鼓风方向，所述密封管道(1)上设有多个用于打开所述密封管道(1)侧壁的取货口(15)，所述取货口(15)处设有用于打开或封盖所述取货口(15)的取货门(16)。
PCT/CN2018/081700 2017-04-07 2018-04-03 用山体做支架、尽自然本力为动力的发射器及运输装置 WO2018184519A1 (zh)

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