DEVICE FOR CONVERSION OF CARBON DIOXIDE TO OXYGEN

Abstract

A device for conversion of carbon dioxide to oxygen, includes, in order, an axial compressor, a centrifuge compressor, a drum, an air pump, and a housing which provides an accommodating space to house the above assemblies together. The axial compressor and centrifuge compressor inhale the carbon dioxide rich air into the accommodating space, then the carbon dioxide rich air pass through the surface of the reactor drum which cause the carbon dioxide bouncing between the reactor drum and the wall of the accommodating space, the collisions of the carbon dioxide molecules will bend and break the molecule bond between carbon and oxygen to produce oxygen. The device, as mentioned earlier, provides a solution to the greenhouse effect, which eliminates the carbon dioxide and generates oxygen by physical method, and advances a design to enhance the conversion process, which has the potential of being enlargement.

Claims

1. A device for conversion of carbon dioxide to oxygen, the device comprising: a housing defining an accommodating space; an axial compressor disposed in the head end of the accommodating space; a air pump disposed in the tail end of the accommodating space; a reactor drum disposed between the axial compressors and the air pump; a centrifuge compressor disposed between the axial compressor and the drum, and the centrifuge compressor is connected with the axial compressor by an axial; a head motor connected with the axial compressor and the centrifuge compressor; a tail motor connected with the air pump; wherein a plurality of drum craterlets are disposed on the surface of the drum; wherein a plurality of housing craterlets are disposed on the wall of the accommodating space that adjacent to the drum.

2. The device of claim 1, further comprising a wind turbine disposed adjacent to the air pump and connected with the drum through an inner shaft.

3. The device of claim 2, wherein the wind turbine includes a serial fan blade mounted on the inner shaft.

4. The device of claim 1, wherein a diameter of the drum craterlets and housing craterlets are double their depth.

5. The device of claim 1, wherein a diameter of the drum craterlets and housing craterlets are 1 cm.

6. The device of claim 1, wherein the surface of the drum and the wall of the housing are coated with silicon carbide.

7. The device of claim 1, wherein the drum is made from light weight metal.

8. The device of claim 1, wherein a distance between the surface of the drum and the wall of the housing is 1 cm.

9. The device of claim 1 generates an airflow thru the reactor drum at a flow rate of over 5 km per second

10. The device of claim 1, wherein the rotational speed of the head motor and the tail motor are 20000 rpm, and the rated power are from 8 to 89 kw.

11. The device of claim 1, wherein the rotational of the compressor and the air pump are in opposite direction.

12. The device of claim 2, wherein the wind turbine receives an exhale air to thrust the reactor drum, wherein the exhale air is generates by the axial compressor, the centrifuge compressor, and the air pump.

13. The device of claim 12, wherein the wind turbine receives the exhale air to decrease the flow rate of the exhale air.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0011] FIG. 1 shows a schematic diagram of the device.

[0012] FIG. 2 shows a schematic diagram of axial compressor and centrifuge compressor.

[0013] FIG. 3 shows a schematic diagram of reactor drum.

[0014] FIG. 4 shows a schematic diagram of the portion of reactor drum and accommodating space.

[0015] FIG. 5 shows a schematic diagram of air pump and wind turbine.

DETAILED DESCRIPTION OF THE INVENTION

[0016] Referring FIG. 1 shows a schematic diagram of the device. The device comprises, in order, an axial compressor 1, a centrifuge compressor 2, a reactor drum 3, and an air pump 4, wherein the device further comprises a housing 5 provided an accommodating space 50 to house the above assemblies together.

[0017] Wherein the device further comprises a wind turbine 6 placed behind the air pump 4, and the wind turbine 6 connected with the reactor drum 3 by an inner shaft 7 which cut through the air pump 4 and reach the reactor drum 3. Wherein the pump motor 92 installed besides the air pump 4, and an outer shaft 8 equipped on the axle center of the air pump 4, the pump motor 92 further engaged with the outer shaft 8 by a pair of gears to drive the air pump 4. In other words, the inner shaft 7 is covered by the outer shaft 8.

[0018] Referring FIG. 2 shows a schematic diagram of axial compressor 1 and centrifuge compressor 2. Axial Compressor 1 and centrifuge compressor 2 is combined to inhale the carbon dioxide rich air into the accommodating space 50, and a compressor motor 91 is provided to connect with the axial compressor 1 and centrifuge compressor 2. The axial compressor 1 is constituted by plenty of interleaved rotor blades 11 and stator 12 to inhale the carbon dioxide, then the centrifuge compressor 2 further tosses the carbon dioxide rich air and then it will flow thru the accommodating space 50; moreover, the air pump 4 also accelerates the flow rate to a high speed to simulate the comet's speed to bend and break the carbon dioxide molecule. The comet's speed which this invention simulated is based on the discovery in Le Roy, Léna, et al. “Inventory of the volatiles on comet 67P/Churyumov-Gerasimenko from Rosetta/ROSINA.” Astronomy & Astrophysics 583 (2015): A1.

[0019] Referring FIG. 3 shows a schematic diagram of reactor drum 3. Reactor drum 3 is a cylinder with a plurality of drum craterlets 31 covering the reactor drum 3. The wall of the accommodating space 50 also has a plurality of housing craterlets 51 relatives to the drum craterlets 31.

[0020] Referring FIG. 4 shows a schematic diagram of the portion of drum 3 and accommodating space 50. The distance between the reactor drum 3 and the accommodating space 50 is 1 cm, the diameter of the craterlet is 1 cm, and the depth of the craterlet is 5 mm. In addition, the surface of the reactor drum 3 and the wall of the accommodating space 50 is coated with silicon carbide, which this material is a non-oxidation minerals and have the hardness to take the constant beating, and can tolerate the high temperature, and have rough surfaces to bend and break the carbon dioxide molecule apart more efficiently.

[0021] When the carbon dioxide flow enters the accommodating space 50 where the reactor drum 3 is placed, and the carbon dioxide molecules 10 keeps bouncing between the drum craterlets 31 and the housing craterlets 51, plus the hitting force of the spinning reactor drum 3 which cause a solid collision to the carbon dioxide molecules 10. When this collision happens at a high speed, the molecule bonds of the carbon dioxide molecules will bend and break and convert the carbon dioxide molecules into carbon atom and oxygen atoms. Wherein the rotation of the reactor drum 3 will also increase the strength and the rate of the collision.

[0022] Referring FIG. 5 shows a schematic diagram of air pump 4 and wind turbine 6. The surface of the air pump 4 is mounted with a plurality of rotor blades 41; when the pump motor 92 thrust the air pump 4 which collaborate with axial compressor 1 and centrifuge compressor 2 to maintain the air speed in the converter, the air pump 4 will drag the oxygen rich air out of the housing 5. Wherein the wind turbine 6 comprises a serial of propeller blades 61; the turbine 6 is designed to reuse the wind energy to generate an extra thrust to rotate the reactor drum 3 faster to increase the strength and rate of the collision. Furthermore, the wind turbine 6 has been designed in a trump shape to increase its ability to collect the exhale wind.

[0023] In an embodiment, the head motor and the tail motor are both the Rexroth IndraDyn H motors presented by Bosch, wherein the rotational speed of the head motor and the tail motor is 20000 rpm, their rated power is from 8 to 89 kw. The head motor provides the axial compressor 1 and centrifuge compressor 2, plus the tail motor provides the air pump 4 to generate airflow at a flow rate of over 5 km per second.

[0024] Furthermore, while the reactor drum 3 and the air pump 4 rotate in a counterclockwise direction, the axial compressor 1 and centrifuge compressor 2 shall be rotates in a clockwise direction in order to maintain the housing 5 stability.

[0025] Wherein the dimensions of the device are 1 m by 7 m, and the size can be enlarged to increase its capacity as long as the cratorlets size and spacing between the cratorlets are remained.

[0026] As state above, the device is capable of converting carbon dioxide to oxygen. It could be utilized in the coal & fossil fuel power plant, incineration facilities, steel & cement manufacturing, and other polluting industries as an air treatment facility. The farmer could also use the device to treat the agriculture waste, including concentrated animal farm and composting yard or in the metropolitan heavy traffic area and large building indoor.

[0027] The device is also an oxygen generator that supplies air for airtight structures, including subway tunnels, mine tunnels, and underground military facilities.

[0028] Besides, the device generates an airflow at a flow rate of over 5 km per second, enabling it to be a part of the Hyperloop high-speed transportation system founded by Musk Elon. The device could help the Hyperloop high-speed transportation system by piping this convertor's exhale air into the tunnel as a thrust to push the capsule forward.

[0029] The device, as mentioned earlier, provides a solution to the greenhouse effect, which eliminates the carbon dioxide and generates oxygen by physical method, and advances a design to enhance the conversion process, which has the potential of being enlargement.