CN108384912B - Special space integrated iron manufacturing device and method thereof - Google Patents
Special space integrated iron manufacturing device and method thereof Download PDFInfo
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- CN108384912B CN108384912B CN201810338859.1A CN201810338859A CN108384912B CN 108384912 B CN108384912 B CN 108384912B CN 201810338859 A CN201810338859 A CN 201810338859A CN 108384912 B CN108384912 B CN 108384912B
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21B—MANUFACTURE OF IRON OR STEEL
- C21B11/00—Making pig-iron other than in blast furnaces
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
- B64G1/443—Photovoltaic cell arrays
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- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
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- Organic Chemistry (AREA)
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Abstract
The invention relates to a special space integrated iron manufacturing device and a method thereof, wherein the device comprises a shell, and an electric power system, a power system, an iron manufacturing system and a control unit which are arranged in the shell, wherein the electric power system comprises a solar panel and a power supply; the power system comprises an injection port and rollers, wherein the injection port is provided with four parts, and the rollers are provided with two parts; when the device runs, the roller is put down, and the switches of the jet ports are continuously and alternately changed, so that the shell keeps a proper speed flight at a certain height from the surface of the moon; the iron making system comprises a high-temperature reduction chamber, a three-removal treatment chamber and a printing chamber, and utilizes high-temperature reduced iron oxide to make specific building materials; the control unit is connected with the electric power system, the power system and the iron making system through wires respectively. The integrated iron manufacturing method utilizes the magnetism of the electromagnet and has ingenious mode; the structure is light and convenient, and is suitable for complex terrains; the 3D printing technology is adopted, and the obtained building materials are various; the pollution is small.
Description
Technical Field
The invention relates to the technical field of space, in particular to the technical field of iron manufacture, and specifically relates to a special space integrated iron manufacture device and a method thereof.
Background
With the development of lunar resources, the product of small trial production cannot meet the requirements, and the reproduction needs to be further expanded, so that the lunar production activity gradually goes to mass production. Meanwhile, due to the increase of personnel entering the moon to participate in development, the built moon base is crowded, and the engineering of rebuilding and expanding the base is required to be completed, which clearly requires a large amount of building materials.
The special working environment on the moon creates great difficulties for the extension engineering of the base. The special nature of lunar environments is mainly low gravity, no atmosphere and more complex terrain. Some engineering difficulties caused by the particularity of the lunar environment are summarized as three points: firstly, the low gravity environment of moon is different from the earth, which increases the burden for the manufacturing and transportation process of building materials; secondly, the temperature difference is large, and as the moon has no atmosphere, the temperature difference between the moon and the day and the night is extremely large and can reach more than 200 ℃, the heat resistance of the device material needs to be considered; thirdly, the topography is complex, mountain and mountains on the lunar surface are fluctuated, the peaks and the mountains are densely distributed, and a conveying device in engineering is required to adapt to the complex topography on the moon. From testing the sample taken back from the investigation vessel, it was confirmed that approximately forty trillion tons of iron were contained in five cm thick dust on the moon surface, i.e. the total iron content on the moon surface would be eight trillion tons. Moreover, iron on the moon is much easier to refine and purer than on the earth.
It was found that theoretically iron could be produced by heating sand on the moon to 1400 ℃. Researchers have carried out iron making researches on the moon sand by using a reducing agent on the earth, and have been successful initially. However, at present, the problems of cost and mass production are still more, and the iron-making technology on the moon is difficult to be put into practical use in a short period of time.
Disclosure of Invention
In order to solve the technical problems, the invention provides a special space integrated iron manufacturing device and a special space integrated iron manufacturing method, which aim to solve the manufacturing and transportation work of building materials on the moon and realize reconstruction and extension of a moon base. In order to achieve the above purpose, the present invention adopts the following technical scheme:
a special space integrated iron manufacturing device comprises a shell, and an electric power system, a power system, an iron manufacturing system and a control unit which are arranged in the shell; the power system comprises a solar panel and a power supply, wherein the solar panel is tightly attached to the upper side of the shell and is used for absorbing energy in sunlight and other light rays, and the power supply is used for storing the energy collected by the solar panel and is connected with each energy-consuming element in the device to supply electric energy for the energy-consuming element; the power system comprises an injection port, a fuel area and rollers, wherein the injection port is provided with four parts, the first part of the injection port is positioned on the section of the tail end and used as a main propeller for driving the device to move forward, the second part of the gesture-adjusting injection port is positioned around the injection port on the section of the tail end and used as an auxiliary propeller for driving the device to move forward, and the third part of the injection port is positioned on the shell of the tail end and is formed by collecting along the circumferential direction so as to counteract torque and prevent the device from rotating; the fourth part of lifting jet ports are positioned at the lower end of the device and used for controlling the lifting of the device and changing the opening and closing of each jet port so as to control the flying of the device, the fuel area is used as an area for storing fuel and reacting the fuel, the kinetic energy of the device is increased after the gas generated in the reaction process is ejected out, the kinetic energy is used for providing power for the movement of the device, and the roller rolls on the surface of the moon when working and is used for keeping the distance between the bottom of the device and the surface of the moon; when the device runs, the roller is put down, the roller bearing is locked, and the device keeps proper speed flight at a certain height from the moon surface by continuously and alternately changing the opening and closing of each jet orifice; the system comprises a shell, an iron making system, a high-temperature reduction chamber, a three-removal treatment chamber, a printing chamber, an electromagnet, a sand pushing sheet, a telescopic rod, a magnetic iron slag collecting table and a pipeline, wherein the ultrasonic transmitter transmits high-frequency mechanical oscillation waves to provide heat required by work for the high-temperature reduction chamber and the three-removal treatment chamber, the high-temperature reduction chamber is used as an oxide area of reduced iron, a reducing agent is added during operation, the high-temperature reduction chamber is used for reducing part of the oxide of the iron into elemental iron, the month sand is converted into molten iron, the molten iron enters a subsequent flow of the iron, the three-removal treatment chamber is used as an area for removing impurities in the iron, the corresponding materials are mainly used for removing three unfavorable elements of phosphorus, sulfur and silicon in the molten iron in a high-temperature state, the printing chamber is used as an area for printing metal iron, the melted elemental iron is injected into the printing chamber to obtain a building material with a specific shape, the high-temperature reduction chamber, the three-removal treatment chamber and the printing chamber are collectively called a treatment chamber, the electromagnet is used for controlling the iron making flow, the electromagnet has the property of electromagnetic attraction, the elemental iron and the three-removal treatment chamber can be used for attracting the elemental iron and the part of the iron to enter the subsequent flow of the iron, the three-removal treatment chamber is used for controlling the three-stage to flow into the three-stage, and the three-stage is used for controlling the three-stage to be used for controlling the three-stage sand to flow to be integrally to be used for the sand to be cut and the sand, and the magnetic slag to be removed to be a large-shaped sand, and has a large-shaped iron, and is flowed end, and is used for the magnetic iron is flowed and has a large scale and has a high-shaped material and has a high thickness, and has a high pressure tank and a high quality and a low cost; the control unit is connected with the electric power system, the power system and the iron making system through wires respectively.
Preferably, the housing is bullet-shaped.
Preferably, two rollers are arranged, are respectively arranged at the left side and the right side of the middle of the lower part of the shell, and are universal rollers.
Preferably, the printing room adopts a metal 3D printer for obtaining various building materials.
A special space integrated iron manufacturing method comprises the following steps:
s1: a preparation step, starting a special space integrated iron making device, and adding charcoal into a high-temperature reduction chamber;
s2: a flight step, wherein a control center is controlled to enable a special space integrated iron manufacturing device to fly to a designated place for mining the moon sand;
s3: an iron manufacturing step, namely starting an iron manufacturing system of the special space integrated iron manufacturing device to operate for manufacturing iron;
s4: a flight step, wherein a control center is controlled to enable a special space integrated iron manufacturing device to fly to a designated place where building materials are used;
further, in step S1, the solar cell panel, the roller, and the sand pushing sheet are housed in the case.
Further, in the step S1, the solar panel is pre-developed to collect solar energy, so as to prevent the shortage of electric quantity of the device in the working process.
Further, in the step S3, the power systems are operated simultaneously, and the flying speed of the device is controlled below 8 m/S.
Further, in step S4, after reaching the designated place, the slag in the magnetic slag collection stage is treated.
The beneficial effects of the invention are as follows: the special space integrated iron manufacturing method provided by the invention starts from practicality, and the magnetic control iron manufacturing process of the electromagnet is utilized, so that the iron manufacturing mode is ingenious, and the iron collection, iron manufacturing and iron transportation integration can be realized; the iron making device is light and convenient in structure, can easily fly on the surface of the moon to work, is suitable for complex terrains of the moon, and can obtain various building materials by adopting a metal 3D printing technology. The special space integrated iron making device generates waste materials of oxygen and a small amount of waste residues, the oxygen is clean energy, no additional waste is generated, the amount of the waste residues is small, and the special space integrated iron making device can be buried in the moon.
Drawings
FIG. 1 is a schematic diagram of the device in an undeveloped state;
FIG. 2 is a schematic view of the structure of the device in the working state;
fig. 3 is a schematic diagram of the structure of the iron making system of the iron making device.
In the figure: 1-shell, 2-solar panel, 3-power supply, 4-jet orifice, 401-propulsion jet orifice, 402-gesture-adjusting jet orifice, 403-self-balancing jet orifice, 404-lifting jet orifice, 5-fuel area, 6-roller, 601-roller bearing, 7-iron making system, 701-ultrasonic emitter, 702-high temperature reduction chamber, 703-three-off treatment chamber, 704-printing chamber, 705-electromagnet, 706-sand pushing piece, 707-telescopic rod, 708-magnetic iron slag collecting table, 709-pipeline, 8-control unit and 9-wire.
Detailed Description
For a more complete understanding of the present invention, reference is now made to the following descriptions taken in conjunction with FIGS. 1-3.
As shown in fig. 1 to 3, the special space integrated iron manufacturing device comprises a shell (1), and an electric power system, a power system, an iron manufacturing system (7) and a control unit (8) which are arranged in the shell (1); the power system comprises a solar panel (2) and a power supply (3), wherein the solar panel (2) is connected with the power supply (3) through an electric wire (9), and absorbed energy is stored in the power supply (3); the power system comprises an injection port (4) and a roller (6), wherein the injection port (4) is divided into four parts, each part is connected with a control unit (8) through an electric wire (9), the control units (8) control the opening and closing of each injection port (4) so as to control the operation of the device, a roller bearing (601) is connected with the control units (8) through the electric wire (9), and the control units (8) control the retraction and the extension of the roller (6) through changing the rotation angle of the roller bearing (601); the iron manufacturing system (7) comprises an ultrasonic transmitter (701), a high-temperature reduction chamber (702), a three-release treatment chamber (703), a printing chamber (704), an electromagnet (705), a sand pushing sheet (706) and a pipeline (709), wherein the ultrasonic transmitter (701), the printing chamber (704) and the electromagnet (705) are connected with a control unit (8) through wires (9), the control unit (8) controls the ultrasonic transmitter (701) to be connected with the high-temperature reduction chamber (702) and the three-release treatment chamber (703) so as to heat substances in the two treatment chambers, the high-temperature reduction chamber (702), the three-release treatment chamber (703) and the printing chamber (704) are connected through the pipeline (709), and the electromagnet (705) is arranged at the outer side of the pipeline (709); the control unit (8) is respectively connected with the electric power system, the power system and the iron making system (7) through wires (9); the control unit (8) is connected with the power system to receive the electric energy in the power supply (3), and is connected with the power system and the iron making system (7) to transmit the electric energy to each energy consumption element in the system; the control unit (8) receives, integrates and sends out information to control the operation of the whole device. When the device runs, the roller (6) is put down, the roller bearing (601) is locked, and the device keeps proper speed flight at a certain height from the moon surface by continuously and alternately changing the opening and closing of each jet orifice (4).
Furthermore, the device is arranged in the rocket cabin and can be separated from the cabin body to work independently after entering the moon environment along with the rocket.
Further, an ultrasonic transmitter (701) transmits ultrasonic waves of 20 kHz.
Further, the thickness of the cut lunar sand is 4cm-5cm.
A special space integrated iron manufacturing method comprises the following steps:
s1: a preparation step, starting a special space integrated iron making device, and adding charcoal into a high-temperature reduction chamber;
s2: a flight step, wherein a control center (8) is controlled to enable a special space integrated iron manufacturing device to fly to a designated place for mining the moon sand;
s3: an iron manufacturing step, namely starting to operate an iron manufacturing system (7) of the special space integrated iron manufacturing device to manufacture iron;
s4: a flight step, wherein a control center (8) is controlled to enable a special space integrated iron manufacturing device to fly to a designated place where building materials are used;
further, in step S1, the solar cell panel (2), the roller (6), and the sand pushing sheet (706) are housed in the case (1).
Further, in the step S1, the solar cell panel (2) is unfolded in advance to collect solar energy, so that insufficient electric quantity of the device in the working process is prevented.
Further, in the step S3, the power systems are operated simultaneously, and the flying speed of the device is controlled below 8 m/S.
Further, in step S4, after reaching a predetermined place, the slag in the magnetic slag collection stage (708) is treated.
The foregoing description is only an example to further illustrate the technical content of the present invention, so that the reader can easily understand the technical content, but the embodiments of the present invention are not limited thereto, and any technical extension or recreating according to the present invention is protected by the present invention.
Claims (5)
1. The utility model provides a special space integration system iron device, installs in rocket cabin, can break away from cabin body independent work after the rocket gets into moon environment, includes bullet head shape casing (1) and locates electrical power system, driving system, system of making iron (7) and control unit (8) in casing (1), and control unit (8) are connected its characterized in that through electric power system, driving system and system of making iron (7) electric wire (9) respectively:
the power system comprises a solar panel (2) and a power supply (3); the solar cell panel (2) is tightly attached to the upper side of the shell (1) and is used for absorbing energy in sunlight and other light rays; the power supply (3) is used for storing the energy collected by the solar panel (2) and is connected with each energy consumption element in the device to supply electric energy for the energy consumption element;
the power system comprises an injection port (4), a fuel zone (5) and a universal roller (6); the jet orifice (4) is provided with four parts, the first part of the propelling jet orifice (401) is positioned on the section of the tail end and is used as a main propeller for driving the device to advance, the second part of the gesture adjusting jet orifice (402) is positioned around the propelling jet orifice (401) on the section of the tail end, the second part of the gesture adjusting jet orifice is used as an auxiliary propeller for driving the device to advance, the running direction of the device is changed up and down and left and right, and the third part of the self-balancing jet orifice (403) is positioned on the shell at the tail part of the device and is formed by collecting along the circumferential direction and is used for counteracting torque to prevent the device from rotating; the fourth part of lifting jet ports (404) are positioned at the lower end of the device and used for controlling the lifting of the device and changing the opening and closing of each jet port (4) so as to control the flying of the device, the fuel area (5) is used as an area for storing fuel and reacting the fuel, the kinetic energy of the device is increased after the gas generated in the reaction process is jetted out and used for providing power for the movement of the device, and the roller (6) rolls on the surface of the moon when working and is used for keeping the distance between the bottom of the device and the surface of the moon; when the device runs, the roller (6) is put down, the roller bearing (601) is locked, and the device keeps a proper speed flight with a certain height from the moon surface by continuously and alternately changing the opening and closing of each jet orifice (4);
the iron making system (7) is positioned at the middle part of the shell and comprises an ultrasonic transmitter (701), a high-temperature reduction chamber (702), a three-release treatment chamber (703), a printing chamber (704), an electromagnet (705), a sand pushing sheet (706), a telescopic rod (707), a magnetic iron slag collecting table (708) and a pipeline (709); the ultrasonic transmitter (701) transmits a 20kHz high-frequency mechanical oscillation wave to provide heat required by work for the high-temperature reduction chamber (702) and the three-removal treatment chamber (703); the high-temperature reduction chamber (702) is used as a region for reducing the oxide of iron, a reducing agent is added during operation, partial oxide of iron is reduced into elemental iron by utilizing high temperature, and the iron is sanded into molten iron and enters the subsequent process of iron production; the three-stripping treatment chamber (703) is used as a region for removing impurities in iron, and corresponding materials are added at a high temperature state to mainly remove three unfavorable elements of phosphorus, sulfur and silicon in molten iron; the printing chamber (704) is used as a region for printing metallic iron, molten elemental iron is injected into the printing chamber (704), and a metallic 3D printer is adopted to obtain a building material with a specific shape; the high-temperature reduction chamber (702), the three-removal processing chamber (703) and the printing chamber (704) are collectively called as a processing chamber; the electromagnet (705) is used for controlling an iron making process, the electromagnet (705) has the property of electrification and magnetism generation, when the electromagnet is electrified, the electromagnet can attract an iron simple substance and partial iron oxide, the inflow and outflow of substances in three processing chambers are controlled, the front end of the sand pushing piece (706) is thin, the rear end of the sand pushing piece is thick, the whole sand pushing piece is streamline and is used for cutting moon sand, the cutting thickness is 4cm-5cm, the telescopic rod (707) is used for controlling the expansion and contraction of the sand pushing piece (706) to determine the thickness of the cut moon sand, the pipeline blockage caused by overlarge magnetism of the electromagnet (705) is avoided, the magnetic iron slag collecting table (708) is a closed container and is used for collecting waste materials generated in the high-temperature reduction chamber (702) and the three-removal processing chamber (703), and the pipeline (709) is used for connecting each processing chamber and guiding the flow of the substances in each processing chamber.
2. A special space integrated iron making method of a special space integrated iron making device according to claim 1, comprising the steps of:
s1: a preparation step, namely starting an integrated iron manufacturing device, and adding charcoal into a high-temperature reduction chamber;
s2: a flight step, wherein the control unit (8) is controlled to enable the integrated iron making device to fly to a designated place for exploiting the moon sand;
s3: an iron manufacturing step, wherein an iron manufacturing system of the integrated iron manufacturing device starts to operate to manufacture iron;
s4: and a flying step, wherein the control unit (8) is controlled to fly the integrated iron making device to a designated place using the building material.
3. The special space integrated iron manufacturing method according to claim 2, wherein in the step S1, the solar cell panel (2), the roller (6) and the sand pushing sheet (706) are stored in the shell (1), and an electric power system is opened in advance to prevent the electric quantity of the device from being insufficient in the working process.
4. The special space integrated iron manufacturing method according to claim 2, wherein in the step S3, the electromagnet (705) is used for controlling the material to enter and exit in each processing chamber by utilizing the property that the simple substance and part of oxide of iron can be attracted by magnetic materials, the power system is operated simultaneously, and the flying speed of the device is controlled below 8 m/S.
5. The special space-integrated iron manufacturing method according to claim 2, wherein in the step S4, after reaching a specified place, the waste residue in the magnetic iron slag collection table (708) is treated.
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| CN108384912A (en) | 2018-08-10 |
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