Patent Application
20170254224
Not applicable.
Not applicable.
The Vortex Turbine Engine also known as apparatus-(A) 02 is a useful powertrain for eliminating range anxiety in mobile or power moving units. The said (A) 02 is a useful powertrain in all kinds of vehicles; cars, vans, auto trucks, buses, or watercrafts. Be a useful powertrain for the residential, commercial or industrial uses.
The apparatus-(A) 02 uses no water for its non-vapor compression heating, cooling and refrigeration embodiment portion, and would be known as the apparatus-NVCHACR-(NV) 02NV (non-vapor compression, heating, cooling and refrigeration) systems. The said (NV) 02NV split-system with its temperatures separation effect would be useful for its non-vapor compression, heating and cooling and refrigeration systems. Although the present invention references the said (A) 02, other are within the scope and can equally benefits from the invention. The water the said does use is use to have and cold water to steam conversion, that being used for the steam turbine-(M) 24.
The apparatus-(A) 02 is useful for its non-polluting energy-efficient system. The said (A) 02 uses no fuel, like oil or gas, the only energy that being used is the electricity for the cylinder motor. Of the main portion of the embodiment there will be only two moving embodiments. With a minimum of moving embodiments this translates into virtually little maintenance.
The apparatus-(A) 02 application generally relates to a two or a plurality of the narrowing spiral tube-(B) 04 and by using the narrowing vortex cylinder-(G) 14 for its temperatures separation effect, having its air-radiation heat separate from its air stream. The separated high temperatures would be used to have a water-to-steam conversion. The said steam would be used in the steam turbine-(M) 24, producing torque for its applications needs. The said (A) 02 temperatures separation effect would be useful for its non-vapor compression, heating and cooling and refrigeration systems.
The apparatus-(A) 02 relates generally by using a low pressure kinetic ambient air medium that being drawn in, then being able to by generating this medium to a very high kinetic moving air pressure. The said (A) 02 is a closed area that would have an opening at each one of the narrowing spiral tube-(B) 04 at its ambient air intakes, with an opening at the radiation boiler chamber-(H) 16 at its air heat outlet, and with an opening at the flash steam cooling air chamber-(K) 20 at its cold air outlet.
The air stream gains velocity while the circumventing air move forward, the air is drawn circumventing through its one of the one, two or a plurality of the said narrowing spiral tube-(B) 04 with its ingrained vortex nozzle and then through its one of the two or a plurality of the narrowing volute generator-(C) 06 with its ingrained vortex nozzle. There would be the same amount of numbers of the said (B) 04 with its vortex nozzle as there are in numbers of the said (C) 06 with its vortex nozzle.
Each one of the said narrowing spiral tube-(B) 04 vortex nozzle would be connected to its one of the said narrowing volute generator-(C) 06. Each one of the said (B) 04 and along with each one of the said (C) 06, all of these would have a converging portion that would have a greater diameter than the diverging portion, to enhance its vortices intensity. The drawing of the air causes a low pressure in front of the high pressured regions, causing the molecules to accelerate toward the low pressure regions.
The said narrowing spiral tube-(B) 04 with its vortex nozzle, the said narrowing volute generator-(C) 06 with its vortex nozzle, the fan chamber-(D) 08, and their air stream is being drawn into the said apparatus-(A) 02 by the cyclone narrowing cylinder-(E) 10. The said (E) 10 joined to and would lay in-between the said (D) 08 within its inner wall. The said (E) 10 spin on its horizontal-axis between the diameter interior side walls of the said (D) 08. Then the said (E) 10 drives the air stream to via the advance narrowing chamber-(F) 12.
The said advance narrowing chamber-(F) 12 having an narrowing tube air outlets with its high speed air stream to via and to advance, generate, and helps to form a vortex within the narrowing vortex cylinder-(G) 14 giving the said (G) 14 with continuous air stream. The said (G) 14 there would be a temperature separation effect, separating the air-radiation heat from its air stream. The said (G) 14 cold air stream would via the cold air cooling chamber-(J) 18. The said (G) 14 with its said air-radiation heat to via its hot narrowing tube outlet and then its air-radiation heat to via its adjustable hot outlet valve and then the said air-radiation heat would via the said radiation boiler chamber-(H) 16.
Using the said narrowing vortex cylinder-(G) 14 with its air-radiation heat on the cold/warm water in effect, would cause a warm water-to-steam conversion within the radiation steam line-(L) 22. The said (L) 22 with its steam, the steam would via the steam turbine-(M) 24. The said steam would drive the said (M) 24. The said (M) 24 uses the steam to force the drive shaft-(N) 26 to rotate on its horizontal-axis producing torque.
The said narrowing vortex cylinder-(G) 14 with its inner cold end, its cold air being used with the return water line-(P) 28, the cold air stream would absorb the latent heat energy from the hot water coming from the said steam turbine-(M) 24, having the hot water-to-warm water conversion. The cold temperature in effect would return the hot water coming from the said (M) 24 that would via the said (P) 28, to have a conversion from hot water to warm water therefore commence the warm water back to-steam within the said radiation steam line-(L) 22 having a conversion cycles thereat. The said (P) 28 uses the warm water pump-(R) 30 to pump the warm water to via the said (L) 22 for the said cycle thereat.
The air-radiation heat emerging from today's vortex tube. The said today's vortex tube outer hot end can reach temperatures as high as +200° C. and the air emerging from its inner cold end can reach −50° C. The said narrowing vortex cylinder-(G) 14 would separate its air stream into an air-radiation heat stream and a cold stream. Each one of the said narrowing spiral tube-(B) 04 narrowing passageways, along with each one of the said narrowing volute generator-(C) 06 narrowing passageways, the said advance narrowing chamber-(F) 12 narrowing tube air outlets, the said (G) 14, each one of these would have a converging portion that would have a greater diameter than the diverging portion, as these would enhance the vortices intensity giving an added higher temperatures and pressure.
The said narrowing vortex cylinder-(G) 14 with its hot narrowing tube outlet with its adjustable hot outlet valve, this would give the needed added higher pressure and temperature. Giving the said steam turbine-(M) 24 the needed 500° C. (932° F.) steam temperature (500 kPa=72.5188 Psi−up to 700 kPa=101.52642 Psi). Results in an increase of the twice maximized cooling heat transfer rate of nearly 330% from 300 kPa to 700 kPa. The said (G) 14 with its adjustable hot outlet valve temperature and pressure output information is based on the publication of: Engenharia Termica (Thermal Engineering), Vol. 11 * No. 1-2 * June and December 2012-p. 85-92.
The water boils at 100° C. at the standard temperature and pressure. The said narrowing vortex cylinder-(G) 14 with its outer hot end would be using its air-radiation heat and the warm water lying within the said radiation steam line-(L) 22. The said (G) 14 outer hot end would be releasing its air-radiation heat energy to heat the water, to have a warm-water-to-hot-water-to-steam conversion. The said (G) 14, its inner cold end would be releasing its cold air to cool the water, to have a steam-to-hot-to-warm water conversion.
The flash thermostatic valve-(T) 32 with its diverter valve, the diverter valve would divert the flash steam from the said return water line-(P) 28 to via the flash steam line-chamber-(V) 34 to be cooled by the cool air within the said flash steam cooling air chamber-(K) 20. The said (K) 20 with its hot/warm water within, the hot/warm water would be pumped by the flash water pump-(W) 36. The said (W) 36 would pump this hot-warm water to via the said return water line-(P) 28 toward the said warm water pump-(R) 30.
The air-radiation heat would transfer to the warm water to make a steam conversion are well known. The cold air would lie within the said cold air cooling chamber-(J) 18. The steam and the hot water heat transfer to the cold air also are well known. The Ranque-Hilsch vortex tube and the steam turbines are well known. The said narrowing vortex cylinder-(G) 14 is similar to and with many characterize of the Uni-flow vortex tube. The said steam turbine-(M) 24 is similar to and with many characterize of other steam turbines.
The apparatus-(A) 02 will have a much broader use by using an air-radiation heat transfer systems, as an alternative to the conventional fuel driven systems. The said (A) 02 is a non-polluting energy-efficient system. The said (A) 02 uses no fuel, like oil or gas, the only energy that being used is the electricity for the cylinder motor.
The apparatus-(A) 02 uses a two or a plurality of the narrowing spiral tube-(B) 04 with its vortex nozzle that would be connected with its one of the two or a plurality of the narrowing volute generator-(C) 06 to produce a high moving air stream medium for the narrowing vortex cylinder-(G) 14. There would be the same amount of numbers of the said (B) 04 with its vortex nozzle as there are in numbers of the said (C) 06 with its vortex nozzle. The said (G) 14 with its vortex, the vortex would have a temperatures separation effect. The vortex separated high temperatures would produce the heat for the steam to be use by the steam turbine-(M) 24 producing torque for the drive shaft-(N) 26.
The Ranque-Hilsch vortex tube and the steam turbines are well known, as these has many characterize with the narrowing vortex cylinder-(G) 14 and with the steam turbine-(M) 24. The apparatus-(A) 02 is an energy-efficient system, by using a low pressure ambient air to produce a high moving air stream medium. The said (G) 14 would produce the air-radiation heat energy to generate the water conversion for the needed steam to drive the said (M) 24 producing torque for the drive shaft-(N) 26.
The government regulations and consumer demands strongly encourage more energy-efficient fuel systems. Energy-efficient fuel systems are needed in: residential, commercial, industrial, automobiles, and watercrafts motors. These systems are now being used, would generally be using a relatively high amount of energy. The apparatus-(A) 02 is useful for its non-polluting high energy-efficient system.
The United States emission standards and managed by the Environmental Protection Agency (EPA) and California Air Resources Board wields an enormous influence over the emissions requirements, set specific limits to the amount of pollution that can be released into the environment. America's has roughly 1,600 existing coal and gas-fired plants generate about 40% of the country's carbon dioxide emissions. The apparatus-(A) 02 is useful in cutting down on these carbon dioxide emissions requirements. Be useful in power stations, generating stations and or generating plants.
The United Nations' Intergovernmental Panel on climate Change says that global warming is here, human-caused and probably already dangerous. In studying the problems caused by the burning of fossil fuels, such as coal, oil and gas paints a harsh warning of what's causing global warming. Continued emission of greenhouse gases will cause further warming and long-lasting changes in all components of the climate system. Power plants account for roughly one-third of all U.S. emissions of the heat-trapping gases blamed for global warming, making them the largest single source. The apparatus-(A) 02 is useful in meeting the global warming requirements.
Research from NASA'S Goddard Space Flight Center shows that large quantities of a chemical responsible for depleting the ozone layer are still being emitted, ever years after an international ban. Though the ozone layer has seemed some recovery since the Montreal Protocol, the ozone hole still persists today. The apparatus-(A) 02 is useful in meeting these ozone requirements, by using non-polluting ambient air medium for its energy needs.
The current torque driven systems utilize a considerable amount of energy. As oil or gas shortages have started to drive the fuel cost up there is concern about the cost of running these current torque systems. The current torque systems need to be designed with considerations of being low in polluting, with efficiency in mind, with an attempt to obtain more energetic systems. The apparatus-(A) 02 meets this efficiency.
The apparatus-(A) 02 eliminate the problem of range anxiety associated to all-electric vehicles. Other benefits include improved national energy security, with the convenience of home recharging, opportunities to provide emergency backup power in the home, and vehicle-to grid (V2G) applications.
The apparatus-(A) 02 replaces a lot of the current high energetic mobile driven systems with the said (A) 02 energy saving system. The said (A) 02 is useful powertrain in versions for all kinds of vehicles, vans, trucks, buses, and watercrafts.
The apparatus-(A) 02 also would be known as the Vortex Turbine Engine; the present invention relates to an air driven and a steam driven system. The said (A) 02 will have a much broader use by using an air-radiation heat transfer systems, as an alternative to the conventional fuel driven systems. The said (A) 02 is a non-polluting energy-efficient system.
The said apparatus-(A) 02 is a closed area that would have an opening at each one of the narrowing spiral tube-(B) 04 at its ambient air intakes, with an opening at the radiation boiler chamber-(H) 16 at its air heat outlet, and with an opening at the flash steam cooling air chamber-(K) 20 at its cold air outlet. The said (A) 02 is suitable as a one, two, or a plurality of units.
Of the main portion of the embodiments there will be only two moving said embodiments; that being the cyclone narrowing cylinder-(E) 10 that being powered by the cylinder motor and the other one would be the steam turbine-(M) 24 producing torque for the drive shaft-(N) 26. The said apparatus-(A) 02 uses no fuel, like oil or gas, the only energy that being used is the electricity for the said cylinder motor. The said (A) 02 uses no refrigerant of any kind to cool the air stream. With only a minimal of moving parts, this translates into virtually little maintenance.
The ambient air medium being drawn into each one of the said narrowing spiral tube-(B) 04 ambient air intakes, the air stream is being drawn in by the said cyclone narrowing cylinder-(E) 10 that being powered by the cylinder motor. The said (E) 10 converts the mechanical energy from the said cylinder motor, to energize the moving air stream.
The said apparatus-(A) 02 uses a two or a plurality of the said narrowing spiral tube-(8) 04 with its ingrained vortex nozzle, these would be connected to its one of the narrowing volute generator-(C) 06 with its ingrained vortex nozzle, these would produce a high moving air stream medium from the said ambient air medium. There would be the same amount of numbers of the said (B) 04 with its vortex nozzle as there are in numbers of the said (C) 06 with its vortex nozzle.
Each one of the said narrowing spiral tube-(B) 04 and along with each one of the said narrowing volute generator-(C) 06, each one of these would have a converging portion that would have a greater diameter than the diverging portion, as these would enhance the vortices intensity. The drawing of the air causes a low pressure in front of the high pressured regions, causing the molecules to accelerate toward the low pressure regions.
The said narrowing spiral tube-(B) 04 with its vortex nozzle with its air stream, the air stream would via the said narrowing volute generator-(C) 06 with its vortex nozzle. The said (C) 06 with its vortex nozzle with its air stream, the air stream would via the fan chamber-(D) 08. The said cyclone narrowing cylinder-(E) 10 joined to and would lay in-between the said (D) 08 within its inner wall. The said (E) 10 spin on its horizontal-axis between the diameter interior side walls of the said (D) 08. The said (D) 08 bottom converging portion being round has a greater diameter than the top portion being round, to enhance its air stream intensity. The said (D) 08 with its air stream, the air stream would via the said (E) 10.
The said cyclone narrowing cylinder-(E) 10 with its air stream now being driven by the said (E) 10 would via the advance narrowing chamber-(F) 12. Each one of the said (F) 12 narrowing tube air outlets would be connected to the narrowing vortex cylinder-(G) 14. The said (F) 12 narrowing tube air outlets would enhance the vortices intensity within the said (G) 14.
The said narrowing vortex cylinder-(G) 14 would have a temperatures separation effect, separating its vortex intensity air stream into an air-radiation heat stream and a cold stream. The said (G) 14 with its air-radiation heat, the air-radiation heat would via the said (G) 14 that would have a hot narrowing tube outlet with adjustable hot outlet valve. The said (G) 14 having its adjustable hot outlet valve with its air-radiation heat, the air-radiation heat would via the said radiation boiler chamber-(H) 16.
The radiation steam line-(L) 22 with its warm water, the warm water would absorb the latent heat lying within the said radiation boiler chamber-(H) 16 having an warm water-to-steam conversion. The said (L) 22 with its warm water-to-steam conversion, the said steam would via the said steam turbine-(M) 24.
The said steam turbine-(M) 24 with its steam flow would generate a rotating motion force, forcing the said drive shaft-(N) 26 to rotate on its horizontal-axis producing torque. The said (M) 24 with its hot steam, the hot water of the steam would via the return water line-(P) 28. The hot water coming from the said (M) 24, this hot water sometimes would flash evaporation. The flash steam would via the flash thermostatic valve-(T) 32 with its diverter valve.
The said return water line-(P) 28 with its hot water, the hot water that did not flash evaporate to flash steam would via toward the warm water pump-(R) 30. The said flash thermostatic valve-(T) 32 with its diverter valve, the diverter valve would divert the flash steam to via the flash steam line-chamber-(V) 34. The said flash steam cooling air chamber-(K) 20 with its cold air, the cold air stream would absorb the flash steam latent heat that would be lying within the said (V) 34 having a steam-to-hot-warm water conversion.
The said flash steam line-chamber-(V) 34 with its steam-to-hot-warm water conversion, the hot-warm water would via the flash water pump-(W) 36. The said (W) 36 would pump this hot-warm water to via the said return water line-(P) 28 toward the said warm water pump-(R) 30. The said narrowing vortex cylinder-(G) 14 with its narrowing tube cold outlet with its cold air, the cold air would via the cold air cooling chamber-(J) 18.
The said cold air cooling chamber-(J) 18 with its cold air, the cold air would via the said flash steam cooling air chamber-(K) 20. The said (J) 18 with its cold air stream, the cold air stream would absorb the latent heat from the hot water lying within the said return water line-(P) 28 having a hot-to-warm water conversion.
The said return water line-(P) 28 with its hot-to-warm water conversion, the warm water would via the said warm water pump-(R) 30. The said (R) 30 with its warm water, pumps the warm water to via the said radiation steam line-(L) 22. The pumping causes a vacuum within the said (P) 28, drawing the said water toward the said (R) 30. The said (L) 22 with its warm water-to-steam conversion therefore commence the warm water-to-steam conversion cycle thereat.
A portion of the apparatus-(A) 02 is a non-vapor compression embodiment, this portion of the said (A) 02 would be known as; the apparatus-NVCHACR-(NV) 02NV (non-vapor compression, heating, cooling and refrigeration) systems. The said (NV) 02NV is a non-vapor compression that uses no refrigerant. The said (NV) 02NV split-system with its temperatures separation effect would be useful for its non-vapor compression, heating and cooling and refrigeration systems.
The said split-system separate its cold temperatures (cold air stream) from its heat temperatures (air-radiation heat). The said cold air stream to via a cold air cooling chamber-(J) 18 and the said air-radiation heat to via its adjustable hot outlet valve and then the said air-radiation heat would via the radiation boiler chamber-(H) 16.
The said apparatus-NVCHACR-(NV) 02NV comprises of: The narrowing spiral tube-(B) 04, the narrowing volute generator-(C) 06, the fan chamber-(D) 08, the cyclone narrowing cylinder-(E) 10, the advance narrowing chamber-(F) 12, and the said narrowing vortex cylinder-(G) 14.
The said apparatus-NVCHACR-(NV) 02NV uses the said narrowing spiral tube-(B) 04, and the said narrowing volute generator-(C) 06, the said fan chamber-(D) 08, the said cyclone narrowing cylinder-(E) 10, the said advance narrowing chamber-(F) 12, along with the said narrowing vortex cylinder-(G) 14. The said (G) 14 outer hot end would by releasing its air-radiation heat would be used for the heating systems. The said (G) 14 inner cold end would by releasing its cold air stream would be used for the cooling and refrigeration systems.
The embodiments will now be described with reference to the accompanying drawing, wherein like reference numbers designate corresponding or identical elements throughout the various drawing. The drawings described herein are for illustration possible only and are not intended to limit the scope of the present disclosure in any way.
The embodiments will now be described with reference to the accompanying drawing, wherein like reference numbers designate corresponding or identical elements throughout the drawing. The Vortex Turbine Engine also would be known as the apparatus-(A) 02. The said (A) 02 uses the apparatus-NVCHACR-(NV) 02NV for its split-system with its temperatures separation effect system.
The said apparatus-NVCHACR-(NV) 02NV comprises of: The narrowing spiral tube-(B) 04, the narrowing volute generator-(C) 06, the fan chamber-(D) 08, the cyclone narrowing cylinder-(E) 10, the advance narrowing chamber-(F) 12, and the narrowing vortex cylinder-(G) 14.
The ambient air medium being drawn into each one of the said narrowing spiral tube-(B) 04 ambient air intakes, the air stream is being drawn in by the said cyclone narrowing cylinder-(E) 10. The said (B) 04 ambient air intake with its ambient air stream, the forward circumventing air stream would via the said (B) 04. The said (B) 04 with its air stream, the air stream would via its vortex nozzle.
The said narrowing spiral tube-(B) 04 vortex nozzle with its air stream, the circumventing air stream would via its one of the said narrowing volute generator-(C) 06. The said (C) 06 with its forward circumventing air stream, the air stream would via its vortex nozzle. The said (C) 06 vortex nozzle with its moving air stream, the air stream would via the said fan chamber-(D) 08.
The said cyclone narrowing cylinder-(E) 10 joined to and would lay in-between the said fan chamber-(D) 08 within its inner wall. The said (D) 08 bottom converging portion being round has a greater diameter than the top portion being round, to enhance its air stream intensity. The said (E) 10 spin on its horizontal-axis between the diameter interior side walls of the said (D) 08. The said (D) 08 with its air stream, the air stream would via the said (E) 10. The said narrowing spiral tube-(B) 04 ambient air intake, the said air stream is being drawn in by the said (E) 10 that being powered by the cylinder motor.
The air stream after being drawn in by the said cyclone narrowing cylinder-(E) 10, the air stream is then driven by the said (E) 10. The said (E) 10 with its driven air stream, the air stream would via the said advance narrowing chamber-(F) 12. The said (F) 12 with its air stream, the air stream would via its said narrowing tube air outlets.
Each one of the said advance narrowing chamber-(F) 12 narrowing tube air outlets with its air stream, the air stream would via the said narrowing vortex cylinder-(G) 14. The said (G) 14 having its temperatures, its temperatures would have a separation effect within its vortex. The said (G) 14, its vortex outer air-radiation heat temperature would separate from its inner cold air.
The said narrowing vortex cylinder-(G) 14 with its temperatures separation effect would have the said vortex with an outer hot end releasing its air-radiation heat. The said (G) 14 with an outer hot end releasing its air-radiation heat to via the air-radiation heat would via its hot narrowing tube outlet and would then via its adjustable hot outlet valve. The said (G) 14 having its adjustable hot outlet valve with its air-radiation heat, the air-radiation heat would via the radiation boiler chamber-(H) 16.
The said narrowing vortex cylinder-(G) 14 with its temperatures separation effect would have the said vortex with an inner cold end releasing its cold air. The said (G) 14 with an inner cold end releasing its cold to via the said (G) 14 with its narrowing tube cold outlet with its cold air, the cold air would via the cold air cooling chamber-(J) 18.
The radiation steam line-(L) 22 with its warm water, the warm water would absorb the air-radiation latent heat lying within the said radiation boiler chamber-(H) 16. The said air-radiation heat would be lying within the said (H) 16. The said warm water conversion to stream would be lying within the said (L) 22. The said (L) 22 would have a warm water-to-steam conversion. The said (H) 16 with its air-radiation heat, the air-radiation heat would via it's the said (H) 16 air heat outlet.
The said radiation boiler chamber-(H) 16 with its air heat outlet with its air-radiation heat, the now cooler air-radiation heat would exit the said apparatus-(A) 02. The return water line-(P) 28 would be lying within the said cold air cooling chamber-(J) 18. The said (J) 18 with its cold air, the cold air stream would absorb the hot-warm water latent heat lying within the said (P) 28.
The said cold air would be lying within the said cold air cooling chamber-(J) 18. The said hot water would be lying within the said return water line-(P) 28. The said (P) 28 would have a hot-to-warm water conversion. The said (J) 18 with its cold air stream, the cold air stream would via the flash steam cooling air chamber-(K) 20. The flash steam line-chamber-(V) 34 would be lying within the said (K) 20.
The said flash steam cooling air chamber-(K) 20 with its warm-cold air, the warm-cold air stream would absorb the flash steam latent heat lying within the said flash steam line-chamber-(V) 34. The said cold air would be lying within the said (K) 20. The said flash steam heat would be lying within the said (V) 34. The said (V) 34 would have a steam-to-hot-warm water conversion. The said (K) 20 with its warm-cold air, the warm-cold air would via its cold air outlet, and then the warm-cold air stream would exit the said apparatus-(A) 02.
The embodiments will now be described with reference to the accompanying drawing, wherein like reference numbers designate corresponding or identical elements throughout the drawing.
The Vortex Turbine Engine also would be known as the apparatus-(A) 02. The water and steam embodiments portion of the said (A) 02 comprises of: The radiation boiler chamber-(H) 16, the cold air cooling chamber-(J) 18, the flash steam cooling air chamber-(K) 20, the radiation steam line-(L) 22, the steam turbine-(M) 24, the drive shaft-(N) 26, the return water line-(P) 28, the warm water pump-(R) 30, the flash thermostatic valve-(T) 32, the flash steam line-chamber-(V) 34, the flash water pump-(W) 36.
The said radiation steam line-(L) 22 would be lying within the said radiation boiler chamber-(H) 16. The said air-radiation heat would be lying within the said (H) 16. The said warm water conversion to stream would be lying within the said (L) 22. The said flash steam line-chamber-(V) 34 would be lying within the said flash steam cooling air chamber-(K) 20. The said cold air would be lying within the said (K) 20.
The said flash steam heat to hot water would be lying within the said flash steam line-chamber-(V) 34. The said return water line-(P) 28 would be lying within the said cold air cooling chamber-(J) 18. The said cold air would be lying within the said (J) 18. The said hot water to warm water would be lying within the said (P) 28.
The said warm water pump-(R) 30 with its warm water, pumps the warm water to via the said radiation steam line-(L) 22. The said (L) 22 with its warm water, the warm water would absorb the latent heat lying within the said radiation boiler chamber-(H) 16. The said (L) 22 would have a warm water-to-steam conversion. The said (L) 22 with its warm water-to-steam conversion, the steam would via the said steam turbine-(M) 24.
The said steam turbine-(M) 24 with its steam flow would generate a rotating motion force, forcing the said drive shaft-(N) 26 to rotate on its horizontal-axis producing torque. The said (N) 26 would be joined to, being part of the said (M) 24. The said (M) 24 would have a steam turning back to hot water conversion. The said (M) 24 with its hot steam, the hot water of the steam would via the said return water line-(P) 28.
The hot water coming from the said steam turbine-(M) 24, this hot water sometimes would flash evaporation within the said return water line-(P) 28. The said flash steam within the said (P) 28 with its flash steam, the flash steam would via the said flash thermostatic valve-(T) 32 with its diverter valve. The said (P) 28 with its hot water, the hot water that did not flash to flash steam would via toward the said warm water pump-(R) 30.
The said flash thermostatic valve-(T) 32 with its diverter valve, the diverter valve would divert the flash steam to via the said flash steam line-chamber-(V) 34. The flash steam that would flash evaporation is released by the said (T) 32 with its diverter valve. The said (T) 32 with its diverter valve with its flash steam, the flash steam would via the said (V) 34.
The said flash steam cooling air chamber-(K) 20 with its cold air, the cold air stream would absorb the flash steam latent heat lying within the said flash steam line-chamber-(V) 34. The said (V) 34 would have a steam-to-hot-warm water conversion. The said (V) 34 with its steam-to-hot-warm water conversion, the hot-warm water would via the said flash water pump-(W) 36. The said (W) 36 with its hot-warm water, pumps the hot-warm water to via the said return water line-(P) 28.
The said flash water pump-(W) 36 would pump this hot-warm water to via the said return water line-(P) 28. The said (P) 28 with its hot water, the water that did not flash to flash steam would via toward the said (R) 30. The said (W) 36 with its hot-warm water, this hot-warm water being pump into the said (P) 28 would be pump toward the said (R) 30. The said cold air cooling chamber-(J) 18 with its cold air stream, the cold air stream would absorb the latent heat from the hot water lying within the said (P) 28.
The said return water line-(P) 28 would have a hot water-to-warm water conversion. The said (P) 28 with its hot-to-warm water conversion, the warm water would via the said warm water pump-(R) 30. The said (R) 30 with its warm water, pumps the warm water to via the said radiation steam line-(L) 22. The said (L) 22 with its warm water-to-steam conversion therefore commence the warm water-to-steam conversion cycle thereat.
The embodiments will now be described with reference to the accompanying drawing, wherein like reference numbers designate corresponding or identical elements throughout the drawing. The Vortex Turbine Engine also would be known as the apparatus-(A) 02.
The apparatus-(A) 02 comprises of: The apparatus-NVCHACR-(NV) 02NV, the radiation boiler chamber-(H) 16, the cold air cooling chamber-(J) 18, the flash steam cooling air chamber-(K) 20, the radiation steam line-(L) 22, the steam turbine-(M) 24, the drive shaft-(N) 26, the return water line-(P) 28, the warm water pump-(R) 30, the flash thermostatic valve-(T) 32, the flash steam line-chamber-(V) 34, the flash water pump-(W) 36.
The apparatus-NVCHACR-(NV) 02NV comprises of: The narrowing spiral tube-(B) 04, the narrowing volute generator-(C) 06, the fan chamber-(D) 08, the cyclone narrowing cylinder-(E) 10, the advance narrowing chamber-(F) 12, and the narrowing vortex cylinder-(G) 14. The said (NV) 02NV embodiment portion would be a closed area that would have an opening at each one of the said narrowing spiral tube-(B) 04 at its ambient air intakes, the said narrowing vortex cylinder-(G) 14 at its narrowing tube cold outlet, and the said (G) 14 at its adjustable hot outlet valve.
The apparatus-(A) 02: The said (A) 02 is suitable as a one, two, or a plurality of units. The said (A) 02 is a closed area that would have an opening at each one of the narrowing spiral tube-(B) 04 at its ambient air intakes, the radiation boiler chamber-(H) 16 at its air heat outlet, and the flash steam cooling air chamber-(K) 20 at its cold air outlet.
The narrowing spiral tube-(B) 04: The apparatus-(A) 02 would contain two or a plurality of the said (B) 04 with each one with an ambient air intake and an ingrained vortex nozzle. There would be the same amount of numbers of the said (B) 04 with its vortex nozzle as there are in numbers of the narrowing volute generator-(C) 06 with its vortex nozzle.
The narrowing spiral tube-(B) 04: The ambient air medium being drawn into each one of the said (B) 04 ambient air intakes, the air stream is being drawn in by the cyclone narrowing cylinder-(E) 10. Each one of the said (B) 04 ambient air intakes is set at an angle to advance, generate, forming a vortex within each one of its one of the said (B) 04. Each one of the said (B) 04 contains a vortex.
The narrowing spiral tube-(B) 04: The air stream gains velocity while circumventing into the said (B) 04 through its ambient air intake and is drawn circumventing through the said (B) 04 and through its vortex nozzle. Each one of the said (B) 04 vortex nozzle is set at an angle to advance, generate, forming a vortex within each one of it's one of the narrowing volute generator-(C) 06.
The narrowing spiral tube-(B) 04: Each one of the said (B) 04 converging portion has a greater diameter than the diverging portion, to enhance the vortices intensity. Each one of the said (B) 04 converging portion has a greater diameter than the diverging portion, to enhance the vortices intensity within each one of it's one of the narrowing volute generator-(C) 06. The said (B) 04 with its air stream, the air stream would via its said vortex nozzle. Each one of the said (B) 04 vortex nozzle with its air stream, the air stream would via it's one of the said (C) 06.
The narrowing volute generator-(C) 06: Each one of the narrowing spiral tube-(B) 04 vortex nozzle with its air stream, the air stream would via it's one of the said (C) 06. The apparatus-(A) 02 would contain two or a plurality of the said (C) 06 with each one with an ingrained vortex nozzle. There would be the same amount of numbers of the said (C) 06 with its vortex nozzle as there are in numbers of the said (B) 04 with its vortex nozzle. Each one of the said (C) 06 converging portion has a greater diameter than the diverging portion, to enhance its vortices intensity. Each one of the said (C) 06 contains a vortex.
The narrowing volute generator-(C) 06: The air stream is drawn circumventing into the said (C) 06 and through its vortex nozzle. The said (C) 06 air stream gains velocity while circumventing, being drawn through the said (C) 06 and through its vortex nozzle. Each one of the said (C) 06 vortex nozzle with its air stream, the air stream would via the fan chamber-(D) 08.
The fan chamber-(D) 08: Each one of the narrowing volute generator-(C) 06 vortex nozzle with its air stream, the air stream would via the said (D) 08. The said (D) 08 is connected to the advance narrowing chamber-(F) 12. The cyclone narrowing cylinder-(E) 10 joined to and would lay in-between the said (D) 08 within its inner wall. The said (E) 10 spin on its horizontal-axis between the diameter interior side walls of the said (D) 08. The said (D) 08 bottom converging portion being round has a greater diameter than the top portion being round, to enhance its air stream intensity. The said (D) 08 with its air stream, the air stream would via the said (E) 10.
The cyclone narrowing cylinder-(E) 10: The said (E) 10 converts the mechanical energy from the cylinder motor, to energize the moving air stream. The energy of the said cylinder motor would energize the said (E) 10 through its rotating movement. The said (E) 10 air holes would energize its rotating movement with an angle to capture the kinetic energy. The said (E) 10 joined to and would lay in-between the fan chamber-(D) 08 within its inner wall. The said (E) 10 spin on its horizontal-axis between the diameter interior side walls of the said (D) 08. The said (E) 10 would be joined to at the bottom of the said (D) 08.
The cyclone narrowing cylinder-(E) 10: The fan chamber-(D) 08 with its air stream, the air stream would via the said (E) 10. The ambient air medium being drawn into each one of the narrowing spiral tube-(B) 04 ambient air intakes, the air stream is being drawn in by the said (E) 10. The air stream is then driven by the said (E) 10. The said (E) 10 converging portion would have a greater diameter than the diverging portion, to enhance the air flow intensity within the advance narrowing chamber-(F) 12. The said (E) 10 with its forward driven air stream, the air stream would via the said (F) 12.
The advance narrowing chamber-(F) 12: The cyclone narrowing cylinder-(E) 10 with its forward driven air stream, the air stream would via the said (F) 12. The said (F) 12 converging portion has a greater diameter than the diverging portion, to enhance the air flow intensity within each one of its narrowing tube air outlets. The said (F) 12 would contain two or a plurality of its narrowing tube air outlets.
The advance narrowing chamber-(F) 12: Each one of the said (F) 12 narrowing tube air outlets converging portion would have a greater diameter than the diverging portion, to enhance the vortices intensity within the narrowing vortex cylinder-(G) 14. Each one of the said (F) 12 narrowing tube air outlets would be connected to the said (G) 14. Each one of the said (F) 12 narrowing tube air outlets contains a vortex. The fan chamber-(D) 08 is connected to the said (F) 12.
The advance narrowing chamber-(F) 12: The said (F) 12 with its air stream would be driven by the cyclone narrowing cylinder-(E) 10. The said (F) 12 with its air stream, the air stream would via it's the said (F) 12 narrowing tube air outlets. Each one of the said (F) 12 narrowing tube air outlets is set at an angle to advance, generate, and helps to form a vortex within the narrowing vortex cylinder-(G) 14. Each one of the said (F) 12 narrowing tube air outlets with its air stream, the air stream would via the said (G) 14.
The narrowing vortex cylinder-(G) 14: Each one of the advance narrowing chamber-(F) 12 narrowing tube air outlets with its air stream, the air stream would via the said (G) 14. The said (G) 14 would separate its compressed vortex air stream into an air-radiation heat stream and a cold stream. The said (G) 14 converging portion would have a greater diameter than the diverging portion, to enhance the vortices intensity, along with its air-radiation heat intensity of the vortex. The said (G) 14 contains a vortex.
The narrowing vortex cylinder-(G) 14: The said (G) 14 having its temperatures, its temperatures would have a separation effect within its vortex. The said (G) 14, its vortex outer air-radiation heat temperature would separate from its inner cold air. The said (G) 14 with its temperatures separation effect would have the said vortex with an outer hot end releasing its air-radiation heat. The said (G) 14 with its temperatures separation effect, this would have its vortex with an inner cold end releasing its cold air.
The narrowing vortex cylinder-(G) 14: The said (G) 14 would have an hot narrowing tube outlet at the outer top end of the said (G) 14. The said (G) 14 hot narrowing tube outlet converging portion would have a greater diameter than the diverging portion, to enhance the air-radiation heat intensity. The said (G) 14 hot narrowing tube outlet would have an adjustable hot outlet valve at the outer top end of the said (G) 14 to adjust its air-radiation heat outward flow.
The narrowing vortex cylinder-(G) 14: The said (G) 14 with an outer hot end releasing its air-radiation heat, the air-radiation heat would via its hot narrowing tube outlet and would then via its adjustable hot outlet valve. The said (G) 14 having its adjustable hot outlet valve with its air-radiation heat, the air-radiation heat would via the radiation boiler chamber-(H) 16.
The narrowing vortex cylinder-(G) 14: The said (G) 14 would have an narrowing tube cold outlet near the outer top end of the said (G) 14. The said (G) 14 would have narrowing tube cold outlet with its adjustable hot outlet valve. The said (G) 14 with an inner cold end releasing its cold air, the cold air would via it's the said (G) 14 narrowing tube cold outlet. The said (G) 14 with its narrowing tube cold outlet with its cold air, the cold air would via the cold air cooling chamber-(J) 18.
The radiation boiler chamber-(H) 16: The narrowing vortex cylinder-(G) 14 having its adjustable hot outlet valve with its air-radiation heat, the air-radiation heat would via the said (H) 16. The radiation steam line-(L) 22 would be lying within the said (H) 16. The said (L) 22 with its warm water, the warm water would absorb the latent heat lying within the said (H) 16. The said air-radiation heat would be lying within the said (H) 16. The said warm water conversion to stream would be lying within the said (L) 22. The said (L) 22 would have a warm water-to-steam conversion.
The radiation boiler chamber-(H) 16: The said (H) 16 with its air-radiation heat within, the air-radiation heat would via its air heat outlet. The said (H) 16 with its air heat outlet with its air-radiation heat, the now cooler air-radiation heat would exit the apparatus-(A) 02.
The cold air cooling chamber-(J) 18: The narrowing vortex cylinder-(G) 14 with its narrowing tube cold outlet with its cold air, the cold air would via the said (J) 18. The return water line-(P) 28 would be lying within the said (J) 18. The said (J) 18 with its cold air stream, the cold air stream would absorb the latent heat from the hot water lying within the said (P) 28. The said cold air would be lying within the said (J) 18. The said hot water would be lying within the said (P) 28. The said (P) 28 would have a hot-to-warm water conversion. The said (J) 18 with its cold air, the cold air would via the flash steam cooling air chamber-(K) 20.
The flash steam cooling air chamber-(K) 20: The cold air cooling chamber-(J) 18 with its cold air, the cold air would via the said (K) 20. The flash steam line-chamber-(V) 34 would be lying within the said (K) 20. The said (K) 20 with its cold air, the cold air stream would absorb the flash steam latent heat lying within the said (V) 34. The said cold air would be lying within the said (K) 20. The said flash steam heat would be lying within the said (V) 34. The said (V) 34 would have a steam-to-hot-warm water conversion. The said (K) 20 with its cold-warm air, the cold-warm air would via its cold air outlet. The said (K) 20 with its cold air outlet with its cold-warm air, the cold-warm air would exit the apparatus-(A) 02.
The radiation steam line-(L) 22: The warm water pump-(R) 30 with its warm water, pumps the warm water to via the said (L) 22. The said (L) 22 would be lying within the radiation boiler chamber-(H) 16. The said (L) 22 with its warm water, the warm water would absorb the latent heat lying within the said (H) 16. The said air-radiation heat would be lying within the said (H) 16. The said warm water conversion to stream would be lying within the said (L) 22. The said (L) 22 would have a warm water-to-steam conversion. The said (L) 22 with its warm water-to-steam conversion, the steam would via the steam turbine-(M) 24.
The steam turbine-(M) 24: The radiation steam line-(L) 22 with its warm water-to-steam conversion, the steam would via the said (M) 24. The said (M) 24 with its steam flow would generate a rotating motion force, forcing the drive shaft-(N) 26 to rotate on its horizontal-axis producing torque. The said (N) 26 would be joined to, being part of the said (M) 24. The said (M) 24 would have a steam turning back to hot water conversion. The said (M) 24 with its hot steam, the hot water of the steam would via the return water line-(P) 28.
The drive shaft-(N) 26: The steam turbine-(M) 24 with its steam flow would generate a rotating motion force, forcing the said (N) 26 to rotate on its horizontal-axis producing torque. The said (N) 26 would be joined to, being part of the said (M) 24.
The return water line-(P) 28: The steam turbine-(M) 24 with its hot steam, the hot water of the steam would via the said (P) 28. The hot water coming from the said (M) 24, this hot water sometimes would flash evaporation (also known as flash steam). The said (P) 28 with its flash steam, the flash steam would via the flash thermostatic valve-(T) 32 with its diverter valve. The said (P) 28 with its hot water, the hot water that did not flash evaporate to flash steam would via toward the warm water pump-(R) 30.
The flash thermostatic valve-(T) 32: The return water line-(P) 28 with its flash steam, the flash steam would via the said (T) 32 with its diverter valve. The said (T) 32 with its diverter valve, the diverter valve would divert the flash steam to via the flash steam line-chamber-(V) 34. The flash steam that would flash evaporation is released by the said (T) 32 with its diverter valve. The said (T) 32 diverter valve with its flash steam, the flash steam would via the said (V) 34.
The flash steam line-chamber-(V) 34: The flash thermostatic valve-(T) 32 diverter valve with its flash steam, the flash steam would via the said (V) 34. The flash steam cooling air chamber-(K) 20 would be lying within the said (V) 34. The said (K) 20 with its cold air, the cold air stream would absorb the flash steam latent heat lying within the said (V) 34.
The flash steam line-chamber-(V) 34: The said cold air would be lying within the flash steam cooling air chamber-(K) 20. The said flash steam heat would be lying within the said (V) 34. The said (V) 34 would have a steam-to-hot-warm water conversion. The said (V) 34 with its steam-to-hot-warm water conversion, the hot-warm water would via the flash water pump-(W) 36.
The flash water pump-(W) 36: The flash steam line-chamber-(V) 34 with its steam-to-hot-warm water conversion, the hot-warm water would via the said (W) 36. The said (W) 36 with its hot-warm water, pumps the hot-warm water to via the return water line-(P) 28. The said (W) 36 would pump this hot-warm water to via the said (P) 28 toward the warm water pump-(R) 30.
The return water line-(P) 28: The flash water pump-(W) 36 with its hot-warm water, pumps the hot-warm water to via the said (P) 28. The said (P) 28 with its hot water, the water that did not flash to flash steam lying within the said (P) 28 would via toward the warm water pump-(R) 30. The said (P) 28 would be lying within the cold air cooling chamber-(J) 18.
The return water line-(P) 28: The cold air cooling chamber-(J) 18 with its cold air stream, the cold air stream would absorb the latent heat from the hot water lying within the said (P) 28. The said cold air would be lying within the said (J) 18. The said hot water would be lying within the said (P) 28. The said (P) 28 would have a hot-to-warm water conversion. The said (P) 28 with its hot-to-warm water conversion, the warm water would via the warm water pump-(R) 30.
The warm water pump-(R) 30: The return water line-(P) 28 with its hot water-to-warm water, the warm water would via toward the said (R) 30. The said (R) 30 with its warm water, pumps the warm water to via the radiation steam line-(L) 22. The pumping causes a vacuum within the said (P) 28, drawing the said water toward the said (R) 30. The said (L) 22 with its warm water-to-steam conversion therefore commence the warm water-to-steam conversion cycle thereat.
The apparatus-NVCHACR-(NV) 02NV: A portion of the apparatus-(A) 02 is a non-vapor compression. This portion of the said (A) 02 would be known as; the said (NV) 02NV (non-vapor compression, heating, cooling and refrigeration). The said (NV) 02NV with its temperatures separation effect, separating its cold air from its latent heat is an embodiment portion of the said (A) 02. The said (NV) 02NV systems, is the systems being used in the said (A) 02 to heat and cool its air stream. The said (NV) 02NV is a non-vapor compression that uses no refrigerant.
The apparatus-NVCHACR-(NV) 02NV: The said (NV) 02NV systems embodiment portion would be a closed area that would have an opening at each one of the narrowing spiral tube-(B) 04 at its ambient air intakes, the narrowing vortex cylinder-(G) 14 at its narrowing tube cold outlet, and the said (G) 14 at its adjustable hot outlet valve. The said (NV) 02NV would contain two or a plurality of the said (B) 04 with each one with an ambient air intake and an ingrained vortex nozzle. The ambient air medium being drawn into each one of the said (B) 04 ambient air intakes, the air stream is being drawn in by the cyclone narrowing cylinder-(E) 10.
The narrowing spiral tube-(B) 04: Each one of the said (B) 04 ambient air intakes is set at an angle to advance, generate, forming a vortex within each one of its one of the said (B) 04. Each one of the said (B) 04 contains a vortex. The air stream gains velocity while circumventing into the said (B) 04 through its ambient air intake and is drawn circumventing through the said (B) 04 and through its vortex nozzle. Each one of the said (B) 04 vortex nozzle is set at an angle to advance, generate, forming a vortex within each one of it's one of the narrowing volute generator-(C) 06.
The narrowing spiral tube-(B) 04: Each one of the said (B) 04 converging portion has a greater diameter than the diverging portion, to enhance the vortices intensity. Each one of the said (B) 04 converging portion has a greater diameter than the diverging portion, to enhance the vortices intensity within each one of it's one of the narrowing volute generator-(C) 06. The said (B) 04 with its air stream, the air stream would via its said vortex nozzle. Each one of the said (B) 04 vortex nozzle with its air stream, the air stream would via within each of its own one of the said (C) 06. There would be the same amount of numbers of the said (B) 04 with its vortex nozzle as there are in numbers of the said (C) 06 with its vortex nozzle.
The narrowing volute generator-(C) 06: Each one of the narrowing spiral tube-(B) 04 vortex nozzle with its air stream, the air stream would via it's one of the said (C) 06. The apparatus-NVCHACR-(NV) 02NV would contain two or a plurality of the said (C) 06 with each one with an ingrained vortex nozzle. There would be the same amount of numbers of the said (C) 06 with its vortex nozzle as there are in numbers of the said (B) 04 with its vortex nozzle. Each one of the said (C) 06 converging portion has a greater diameter than the diverging portion, to enhance its vortices intensity.
The narrowing volute generator-(C) 06: Each one of the said (C) 06 contains a vortex. The air stream is drawn circumventing into the said (C) 06 and through its vortex nozzle. The said (C) 06 air stream gains velocity while circumventing, being drawn through the said (C) 06 and through its vortex nozzle. Each one of the said (C) 06 vortex nozzle with its air stream, the air stream would via the fan chamber-(D) 08.
The fan chamber-(D) 08: Each one of the narrowing volute generator-(C) 06 vortex nozzle with its air stream, the air stream would via the said (D) 08. The said (D) 08 is connected to the advance narrowing chamber-(F) 12. The cyclone narrowing cylinder-(E) 10 joined to and would lay in-between the said (D) 08 within its inner wall. The said (E) 10 spin on its horizontal-axis between the diameter interior side walls of the said (D) 08. The said (D) 08 bottom converging portion being round has a greater diameter than the top portion being round, to enhance its air stream intensity.
The cyclone narrowing cylinder-(E) 10: The said (E) 10 converts the mechanical energy from the cylinder motor, to energize the moving air stream. The energy of the said cylinder motor would energize the said (E) 10 through its rotating movement. The said (E) 10 air holes would energize its rotating movement with an angle to capture the kinetic energy. The said (E) 10 joined to and would lay in-between the fan chamber-(D) 08 within its inner wall. The said (E) 10 spin on its horizontal-axis between the diameter interior side walls of the said (D) 08. The said (E) 10 would be joined to at the bottom of the said (D) 08.
The cyclone narrowing cylinder-(E) 10: The fan chamber-(D) 08 with its air stream, the air stream would via the said (E) 10. The ambient air medium being drawn into each one of the narrowing spiral tube-(B) 04 ambient air intakes, the air stream is being drawn in by the said (E) 10. The air stream is then driven by the said (E) 10. The said (E) 10 converging portion would have a greater diameter than the diverging portion, to enhance the air flow intensity within the advance narrowing chamber-(F) 12. The said (E) 10 with its forward driven air stream, the air stream would via the said (F) 12.
The advance narrowing chamber-(F) 12: The cyclone narrowing cylinder-(E) 10 with its forward driven air stream, the air stream would via the said (F) 12. The said (F) 12 converging portion has a greater diameter than the diverging portion, to enhance the air flow intensity within each one of its narrowing tube air outlets. The said (F) 12 would contain two or a plurality of its narrowing tube air outlets.
The advance narrowing chamber-(F) 12: Each one of the said (F) 12 narrowing tube air outlets converging portion would have a greater diameter than the diverging portion, to enhance the vortices intensity within the narrowing vortex cylinder-(G) 14. Each one of the said (F) 12 narrowing tube air outlets would be connected to the said (G) 14. Each one of the said (F) 12 narrowing tube air outlets contains a vortex. The fan chamber-(D) 08 is connected to the said (F) 12.
The advance narrowing chamber-(F) 12: The said (F) 12 with its air stream would be driven by the cyclone narrowing cylinder-(E) 10. The said (F) 12 with its air stream, the air stream would via it's the said (F) 12 narrowing tube air outlets. Each one of the said (F) 12 narrowing tube air outlets is set at an angle to advance, generate, and helps to form a vortex within the narrowing vortex cylinder-(G) 14. Each one of the said (F) 12 narrowing tube air outlets with its air stream, the air stream would via the said (G) 14.
The narrowing vortex cylinder-(G) 14: Each one of the advance narrowing chamber-(F) 12 narrowing tube air outlets with its air stream, the air stream would via the said (G) 14. The said (G) 14 would separate its compressed vortex air stream into an air-radiation heat stream and a cold stream. The said (G) 14 converging portion would have a greater diameter than the diverging portion, to enhance the vortices intensity, along with its air-radiation heat intensity of the vortex. The said (G) 14 contains a vortex.
The narrowing vortex cylinder-(G) 14: The said (G) 14 having its temperatures, its temperatures would have a separation effect within its vortex. The said (G) 14, its vortex outer air-radiation heat temperature would separate from its inner cold air. The said (G) 14 with its temperatures separation effect would have the said vortex with an outer hot end releasing its air-radiation heat. The said (G) 14 with its temperatures separation effect, this would have its vortex with an inner cold end releasing its cold air.
The narrowing vortex cylinder-(G) 14: The said (G) 14 would have an hot narrowing tube outlet at the outer top end of the said (G) 14. The said (G) 14 hot narrowing tube outlet converging portion would have a greater diameter than the diverging portion, to enhance the air-radiation heat intensity. The said (G) 14 hot narrowing tube outlet would have an adjustable hot outlet valve at the outer top end of the said (G) 14 to adjust its air-radiation heat outward flow.
The narrowing vortex cylinder-(G) 14: The said (G) 14 with an outer hot end releasing its air-radiation heat, the air-radiation heat would via its hot narrowing tube outlet and would then via its adjustable hot outlet valve. The said (G) 14 having its adjustable hot outlet valve with its air-radiation heat, the air-radiation heat would exit the apparatus-NVCHACR-(NV) 02NV.
The narrowing vortex cylinder-(G) 14: The said (G) 14 would have an narrowing tube cold outlet near the outer top end of the said (G) 14. The said (G) 14 with an inner cold end releasing its cold air, the cold air would via it's the said (G) 14 narrowing tube cold outlet. The said (G) 14 with its narrowing tube cold outlet with its cold air, the cold air would exit the apparatus-NVCHACR-(NV) 02NV.
Air induction: The air being drawn into the narrowing spiral tube-(B) 04, causing an air pressure buildup on the atmospheric high pressure regions. The vacuum in the front of the molecules, in this high pressure region causes the molecules (matter) to accelerate toward the low pressure regions. Air induction is used within the said (B) 04 and then the air flow would via its one of the narrowing volute generator-(C) 06.
Atmospheric gases: The common name given to the atmospheric gases used in breathing and photosynthesis is air. In a gas, the molecules have enough energetic so that the effect of intermolecular forces is small, and the typical distance between neighboring molecules is much greater than the molecular size.
Atmospheric pressure: Is the force per unit area exerted on a surface by the weight of air above that surface, the higher the atmospheric pressure, the higher the ambient air pressure buildup. The drawing of the ambient air pressure causes a vacuum in the high pressure regions. The vacuum in the front of the molecules causes the molecules to accelerate toward the low pressure regions.
Atmospheric pressure: The apparatus-(A) 02 uses the atmospheric pressure high and low pressure regions. The cyclone narrowing cylinder-(E) 10 draws the ambient air medium into the said (A) 02, through the narrowing spiral tube-(B) 04 ambient air intake, then through its ingrained vortex nozzle, the narrowing volute generator-(C) 06 with its ingrained vortex nozzle, then driven through the advance narrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets and the narrowing vortex cylinder-(G) 14. The drawing of its air from the high pressured regions causes a vacuum in front of the high pressured regions. This cause a vacuum (low pressure) in the atmospheric high pressure regions, this vacuum in front of the high pressure causes the molecules to accelerate toward the low pressure regions.
Bernoulli principle: The correlation between air speed and pressure, as speed increases pressure decreases, as the air is curving. The continuous change of position of a body of air stream curving within the apparatus-(A) 02, so that every partied of the body follows a straight-line path. The Bernoulli principle is used in the narrowing spiral tube-(B) 04 with its ingrained vortex nozzle, the narrowing volute generator-(C) 06 with its ingrained vortex nozzle, the advance narrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets and the narrowing vortex cylinder-(G) 14.
Conservation laws, in physics: As air is drawn circumventing into the narrowing spiral tube-(B) 04, the narrowing volute generator-(C) 06, then driven through the advance narrowing chamber-(F) 12 with its narrowing tube air outlets and the said (F) 12, and the said (F) 12 narrowing tube air outlets, a corresponding volume must move a greater distance in their narrowing of the passageways and thus have a greater speed. At the same time, the work done by corresponding volumes in the narrowing of the passageways will be expressed by the product of the pressure and the volume. Since the speed is greater in the narrowing of the passageways, the energetic of that volume is greater. Then, by the law of conservation of energy, this increase in kinetic energy must be balanced by a decrease in the pressure-volume product, or, since the volumes are equal, by a decrease in pressure.
Converging and diverging portions: Each one of these: The narrowing spiral tube-(B) 04 with its ingrained vortex nozzle, the narrowing volute generator-(C) 06 with its ingrained vortex nozzle, the advance narrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets and the narrowing vortex cylinder-(G) 14, all of these has a converging and diverging portion, to enhance the vortices intensity. The said (G) 14 hot narrowing tube outlet would have a converging and diverging portion, to enhance the air-radiation heat temperature intensity. The converging portion has a greater diameter than the diverging portion. The converging portion has a high capacity and a low velocity. The diverging portion will have a low capacity and a high velocity with a back pressure. The ambient pressure, referred to as lower atmospheric pressure, (back pressure) causes the air stream to accelerate. By reducing the pressure of the air at the exit of the expansion portion, in effect, the molecules leave the outlets at their thermal speed without colliding with other molecules. This is because the molecules are all moving in the same relative direction and at the same speed.
Diverter valve: The pressure is relieved by allowing the pressurized steam (flash evaporation) to flow from the return water line-(P) 28, the pressurized steam would via the diverter valve of the flash thermostatic valve-(T) 32. The diverter valve is designed or set to open at a predetermined set pressure to protect the said (P) 28 and the other equipment from being subjected to pressures that exceed their design limits. The said (T) 32 control the volume and temperature, and by using a diverter valve this would divert the steam that would be released by the said (T) 32, this pressurized steam would via the flash steam line-chamber-(V) 34.
Flash steam: Is a name given to the steam formed from hot condensate when the pressure is reduced. Flash steam is no different from normal steam. The hot water that is produced from the steam turbine-(M) 24, this hot water would via the return water line-(P) 28. Whereas flash steam occurs when high pressure and high temperature condensate is exposed to a large pressure drop such as when being released by the said (M) 24 and would via the said (P) 28. High temperature condensate contains high energy that cannot remain in liquid form at a lower pressure because there is more energy than that required to achieve saturated water at the lower pressure. The result is that some of the excess energy causes a % of the condensate to flash within the said (P) 28.
Heat transfer: Describes the exchange of thermal energy, between physical systems depending on the temperature and pressure, by dissipating heat. The fundamental modes of heat transfer are conduction or diffusion, convection and radiation. The exchange of kinetic energy of particles: Through the boundary between two systems at different temperatures, from each other from their surroundings. Heat transfer always occurs from a region of high temperature to another region of lower temperature. Heat transfer changes the internal energy of both systems involved according to the First Law of Thermodynamics. The Second Law of Thermodynamics defines the concept of thermodynamic entropy, by measurable heat transfer. The apparatus-(A) 02 uses its two systems with the different temperatures. The narrowing vortex cylinder-(G) 14 would have a narrowing tube cold outlet, releasing its cold air. With the inner cold end, the flash steam line-chamber-(V) 34 and the return water line-(P) 28 would have a hot to cold conversion. The said (G) 14 would have an adjustable hot outlet valve, releasing its air-radiation heat. With the outer hot end, the radiation steam line-(L) 22 would have a cold/warm to steam conversion.
Kinetic Molecular Theory of Matter: Is a concept that basically states that atoms and molecules possess energy of motion (kinetic energy) that we perceive as temperature. In other words, atoms and molecules are constantly in motion, and we measure the energy of these movements as the temperature of that substance. This means if there is an increase in temperature, the atoms and molecules will gain more energy (kinetic energy) and move even faster. The narrowing spiral tube-(B) 04, the narrowing volute generator-(C) 06, the advance narrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets, the narrowing vortex cylinder-(G) 14; possesses energy of motion.
Kinetic momentum: The momentum which a particle possesses because of its motion, equal to the particle's mass times it velocity. The narrowing spiral tube-(B) 04, the narrowing volute generator-(C) 06, the advance narrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets, the narrowing vortex cylinder-(G) 14 air outward motion mass, equal times it velocity. The rotational energetic depends on rotation about an axis, and for a body of constant moment of inertia is equal to the product of half the moment of inertia times the square of the angular velocity. In relativistic physics kinetic energy is equal to the product of the increase of mass caused by motion times the square of the speed of light.
Mach number=1: Assuming air to be an ideal gas, the formula to compute Mach number in a subsonic compressible flow is found from Bernoulli's equation for M<1.
Narrowing vortex cylinder-(G) 14: The said (G) 14 with a converging portion that has a greater diameter than the diverging portion. The said (G) 14 consists of a high pressure circumventing air stream that enters the said (G) 14 and the air-radiation heat passes through its said hot narrowing tube outlet and then through it's said adjustable hot outlet valve. The gas expands through its said adjustable hot outlet valve and achieves a high angular velocity, causing a vortex-type flow. There are two exits to the said (G) 14: the said hot narrowing tube outlet that the air-radiation heat passing through and then through the said adjustable hot outlet valve, that exit is placed near the outer radius of the said (G) 14 at the end away from its said narrowing tube cold outlet exit that is placed at the center of the said (G) 14 at the same end as the said adjustable hot outlet valve. By adjusting its said hot narrowing tube outlet with its said adjustable hot outlet valve downstream of the said exit, it is possible to vary the fraction of the incoming air flow that leaves through it's said narrowing tube cold outlet, referred as cold fraction. This adjustment affects the amount of cold and hot energy that leaves the said (G) 14 through its exits. Results in an increase of the twice maximized cooling heat transfer rate of nearly 330% from 300 kPa to 700 kPa. (700 kPa=101.52642 Psi) The said (G) 14 with its said adjustable hot outlet valve temperature and pressure output information is based on the publication of: Engenharia Termica (Thermal Engineering), Vol. 11 * No. 1-2 * June and December 2012-p. 85-92.
Newton's first law of motion: Linear motion is the basic of all motion. According to Newton's first law of motion, objects that do not experience any net force will continue to move in a straight line with a constant velocity until they are subjected to a net force.
Pressure: Is a defined as the force per unit area exerted against a surface by the weight of the air above that surface. In terms of molecules, if the number of molecules above a surface increases, there are more molecules to exert a force on that surface and consequently, the pressure increases.
Air-radiation heat transfer: Radiation is a method of heat transfer that does not rely upon any contact between the heat source and the heated object as is the case with conduction and convection. Heat can be transmitted though empty space by thermal radiation is often called infrared radiation. The narrowing vortex cylinder-(G) 14 uses the air-radiation heat transfer. The transfer of the air-radiation heat coming from the said (G) 14 this said air-radiation heat stream would be transferred through its adjustable hot outlet valve. With this transfer of the said air-radiation heat, the radiation steam line-(L) 22 would have a cold/warm water to steam conversion.
Ranque-Hilsch vortex tube: The vortex tube has been used for many decades in various engineering applications. Because of its compact design and little maintenance requirements, it is very popular in heating and cooling processes. There is no unifying theory that explains the temperature separation phenomenon inside the vortex tube. The vortex tube is a mechanical device that separates compressed air into an outward radial high temperature region and an inner lower one. There are two classifications of the vortex tube. Both of these are currently in use in the industry. The more popular is the counter-row vortex tube and the Uni-flow vortex tube. The narrowing vortex cylinder-(G) 14 is similar to with many characterize of the Uni-flow vortex tube.
Sound waves: In physics, sound is a vibration that propagates as a typically audible mechanical wave of pressure and displacement, through a medium such as air. In physiology and psychology, sound is the reception of such waves and their perception by the brain. The apparatus-(A) 02 in accordance with its design has the means to adjust its outward air flow speed, therefore reducing its sound waves.
Steam: Is a term for the gaseous phase of water, which is formed when water boils. Technically speaking, in terms of the chemistry and physics, steam is invisible and cannot be seen, however in common language it is often used to refer to the visible mist or aerosol of water droplets formed as this water vapor condenses in the presence of (cooler) air. At lower pressures, such as in the upper atmosphere or at the top of high mountains water boils at a lower temperature than the nominal 100° C. (212° F.) at standard temperature and pressure. Today's vortex tube with its adjustable valve can reach temperatures as high as +200° C. and the air emerging from its inner cold end can reach −50° C. are possible. The narrowing vortex cylinder-(G) 14 would separate its air stream into an air-radiation heat stream and a cold stream. The said (G) 14, the converging portion has a greater diameter than the diverging portion, to enhance the vortices intensity giving this an added higher temperatures along with its hot narrowing tube outlet with its adjustable hot outlet valve. The steam turbine-(M) 24 needs 500° C. (932° F.) (500 kPa=72.5188 Psi) to produce its needed steam pressure. The said (G) 14 with its hot narrowing tube outlet and along with its adjustable hot outlet valve giving the needed 500° C. (932° F.) (500 kPa=72.5188 Psi) to produce its needed steam pressure. To increase of the twice maximized cooling heat transfer rate of nearly 330% from 300 kPa to 700 kPa. (700 kPa=101.52642 Psi).
Steam turbine: There are two basic types of the steam turbines; blades or the nozzles. Blades move entirely due to the impact of steam on them and their profiles do not converge. This results in a steam velocity drop and essentially no pressure drop as steam moves through the blades. A turbine composed of blades alternating with fixed nozzles is called an impulse turbine, Curtis turbine, Rateau turbine, or Brown-Curtis turbine. Nozzles appear similar to blades, but their profiles converge near the exit. This results in a steam pressure drop and velocity increase as steam moves through the nozzles. Nozzles move due to both the impact of steam on them and the reaction due to the high-velocity steam at the exit. A turbine composed of moving nozzle alternating with fixed nozzles is called a reaction turbine or Parsons Turbine. The steam turbines are well known, as these has many characterize of the steam turbine-(M) 24.
Subsonic: As a gas is forced through a tube, the gas molecules are deflected by the walls of the tube. If the speed of the gas is much less than the speed of sound of the gas, the density of the gas remains constant and the velocity of the flow increases. However, as the speed of the flow approaches the speed of sound we must consider compressibility effects on the gas. The density of the gas varies from one location to the next. Considering flow through a tube, if the flow is very gradually compressed (area decreases) and then gradually expanded (area increases), the flow conditions return to their original values. We say that such a process is reversible. From a consideration of the second law of thermodynamics, a reversible flow maintains a constant value of entropy.
Vacuum: An approximation to such vacuum is a region with a gaseous pressure much less than atmospheric. This causes the circumventing air stream (molecule) to accelerate toward the low pressure regions. The apparatus-(A) 02 uses these vacuums to move the air stream from high pressure regions to low pressure regions. The drawing of the air from the high pressured regions causes a vacuum in front of the high pressured regions. This causes a vacuum (low pressure) in the atmospheric high pressure region, with this vacuum in front of the high pressure causes the molecules would accelerate toward the low pressure regions. The narrowing spiral tube-(B) 04 along with the narrowing volute generator-(C) 06, use this drawing of the ambient air medium, causing a vacuum (low pressure). The return water line-(P) 28 uses the (vacuum) low pressure regions to draw the flowing water toward the warm water pump-(R) 30.
Vortex: The vortices are a measure of the intensity of a vortex. An important mechanism that enhances the vortices is the stretching of the vortex—stretching along the axis of the vortex, makes it rotate faster and decreases its diameter in order to constantly maintain its kinetic momentum. The narrowing spiral tube-(B) 04, the narrowing volute generator-(C) 06, the advance narrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets and the narrowing vortex cylinder-(G) 14 uses this stretching to enhance the vortices intensity.
Vortex nozzle: The vortex nozzle is also call a CD-nozzle or a convergent-divergent nozzle. The air enters the converging section, its velocity increases, considering the mass flow rate to be constant. The gas passes through the throat, it attains sonic velocity (Mach number=1). As the gas passes through the divergent section, the gas would velocity to be supersonic (also Mach 1). The air speed would be keep subsonic. The narrowing spiral tube-(B) 04 with its vortex nozzle, along with the narrowing volute generator-(C) 06 with its vortex nozzle, all of these would use its converging and divergent to increase velocity.
Vortex tube: The water boils at 100° C. at the standard temperature and pressure. Today's vortex tube outer hot end can reach temperatures as high as +200° C. and the air emerging from its inner cold end can reach −50° C. are possible. The narrowing vortex cylinder-(G) 14 would separate its compressed air into an air-radiation heat stream and a cold stream. Each one of the narrowing spiral tube-(B) 04 narrowing passageways, along with each one of the narrowing volute generator-(C) 06 narrowing passageways, the advance narrowing chamber-(F) 12 and the said (F) 12 narrowing tube air outlets, and along with the said (G) 14, all of these would have their converging portion would have a greater diameter than the diverging portion, to enhance the vortices intensity giving an added higher temperatures and pressure. The said (G) 14 with its hot narrowing tube outlet and along with its adjustable hot outlet valve giving the needed 500° C. (932° F.) (500 kPa=72.5188 Psi) to produce its needed steam pressure. The adjustable hot outlet valve increase of the twice maximized cooling heat transfer rate of nearly 330% from 300 kPa to 700 kPa. (700 kPa=101.52642 Psi).
Embodiment has the means to be attached, connected, continuous, joined to or in transmission of something from one point to another point. The apparatus-(A) 02 has the means to attach to and supports each one of the structures of its embodiments. The said (A) 02 in communication with one, two, or with a plurality of units or an assembly of units. The said (A) 02 has the means to and would be in communication with each embodiment. Each embodiment would be in communication with the said (A) 02.
Each one of the narrowing spiral tube-(B) 04 would have an ambient air intake. Each one of the said (B) 04 with its ingrained vortex nozzle is connected to it's one of the narrowing volute generator-(C) 06. Each one of the said (C) 06 with its ingrained vortex nozzle is connected to the fan chamber-(D) 08.
The fan chamber-(D) 08 is connected to the advance narrowing chamber-(F) 12. The said (D) 08 is joined to and would have the means to support the structure of the cyclone narrowing cylinder-(E) 10. The said (E) 10 would be joined to the cylinder with its motor shaft. The said (E) 10 would be joined to and would lay in-between the said (D) 08 within its inner wall. The cylinder motor with its drive shaft would be joined to the said (E) 10. The said cylinder motor with its drive shaft would be joined to and made part of the said cylinder motor. The said cylinder motor with its drive shaft would be not shown in the drawing.
Each one of the advance narrowing chamber-(F) 12 narrowing tube air outlets is connected to the narrowing vortex cylinder-(G) 14. The said (G) 14 with its hot narrowing tube outlet with its adjustable hot outlet valve is connected to the radiation boiler chamber-(H) 16. The said (H) 16 would have an air heat outlet, exiting the apparatus-(A) 02. The said (G) 14 with its narrowing tube cold outlet is connected to the cold air cooling chamber-(J) 18. The said (J) 18 is connected to the flash steam cooling air chamber-(K) 20. The said (K) 20 would have a cold air outlet, exiting the said (A) 02.
The radiation steam line-(L) 22 is connected to the steam turbine-(M) 24. The drive shaft-(N) 26 would be joined to, being part of the said (M) 24. The said (M) 24 is connected to the return water line-(P) 28. The said (P) 28 is connected to the flash thermostatic valve-(T) 32 with its diverter valve. The said (P) 28 is also connected to the warm water pump-(R) 30. The said (P) 28 is also connected to the flash water pump-(W) 36.
The flash thermostatic valve-(T) 32 with its diverter valve is connected to the flash steam line-chamber-(V) 34. The said (V) 34 is connected to the flash water pump-(W) 36. The said (W) 36 is connected to the return water line-(P) 28. The warm water pump-(R) 30 is connected to the radiation steam line-(L) 22.
Transfer to: The narrowing spiral tube-(B) 04, narrowing volute generator-(C) 06, fan chamber-(D) 08, cyclone narrowing cylinder-(E) 10, the advance narrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets, narrowing vortex cylinder-(G) 14, the said (G) 14 narrowing tube cold outlet, the said (G) 14 hot narrowing tube outlet or being hot narrowing tube outlets, the radiation boiler chamber-(H) 16, the cold air cooling chamber-(J) 18, and the flash steam cooling air chamber-(K) 20, are compartment, tube or pipe with the means to transfer the air stream and or the air-radiation heat from one point to the next point.
Transfer to: The radiation steam line-(L) 22, return water line-(P) 28, flash steam line-chamber-(V) 34 are compartment, tube or pipe with the means to transfer the steam and or the hot-warm water from one point to the next point. The warm water pump-(R) 30 and along with the flash water pump-(W) 36 with the means to transfer the hot-warm water or cold/warm water from one point to the next point.
Means to: The apparatus-(A) 02 to have means to start, stop, and control or adjust the cylinder motor to rotate or to spin the cyclone narrowing cylinder-(E) 10 on its horizontal-axis shaft. The said (E) 10 would be joined within and at the bottom end of the fan chamber-(D) 08, with the means to rotate on its horizontal-axis. The said (E) 10 utilizes the said cylinder motor with the means to start, stop, and control or adjust its rotating or spinning within the said (D) 08. The said cylinder motor has the means to force the said (E) 10 on its horizontal-axis shaft to rotate or to spin.
Means to: The apparatus-(A) 02 to have means to start, stop, and control, adjust the warm water pump-(R) 30, the flash water pump-(W) 36, and the flash thermostatic valve-(T) 32 with its diverter valve. A sensor with the means to adjust and control the water level that being release by the said (R) 30. The radiation steam line-(L) 22, the return water line-(P) 28, and the flash steam line-chamber-(V) 34 would have the means, to adjust and/or control the water level or its water temperature.
Means to: The narrowing vortex cylinder-(G) 14 hot narrowing tube outlet with its adjustable hot outlet valve has the means to adjust, this adjustment to have the effects of the amount of cold and hot energy that leaves the said (G) 14 through its exits. The said (G) 14 hot narrowing tube outlet with an adjustable hot outlet valve built into the outer hot end releasing its air-radiation heat.
The hydrophilic polymers: The hydrophilic polymers grafting treatment along walls that are exposed to water as needed: The radiation steam line-(L) 22, the steam turbine-(M) 24, the return water line-(P) 28, the warm water pump-(R) 30, the diverter valve of the flash thermostatic valve-(T) 32, the flash steam line-chamber-(V) 34, and the flash water pump-(W) 36, with the option to use, have, or be grafted along any or any other areas, where treatment is needed.
HydroLAST™: HydroLAST™ is a process by which hydrophilic polymers are grafted permanently to the surface of a hydrophobic substrate. The hydrophilic polymer has carboxyl, hydroxil, or amine functionalities that serve to loosely bind water. Once treated, the substrate “wets out” and allows water and reagents to flow easily over or through it (in the case of porous substrates). Unlike conventional hydrophilic treatments such as straight plasma, corona, or ozone processing, the surface is permanently rather than transiently hydrophilic.
Any such methods are natural outgrowths of the system or apparatus claims. Natural outgrowths, alternative embodiment are not shown in the drawing.
The apparatus-(A) 02 alternative: The said (A) 02 would have an alternative to use only one and not the other one: the two or a plurality of the narrowing spiral tube-(B) 04 with its ingrained vortex nozzle or to use the two or a plurality of the narrowing volute generator-(C) 06 with its ingrained vortex nozzle. Each one of the said (B) 04 narrowing passageways or the said (C) 06 narrowing passageways; being used with its vortex nozzle would be connected to the fan chamber-(D) 08.
The apparatus-(A) 02 alternative: The said (A) 02 would have an alternative to use one, two or a plurality of additional cylinders and joined to their motor or motors. The said additional cylinders would be in front of and near or joined to the narrowing spiral tube-(B) 04 ambient air intakes, driving the ambient air medium into each one of the said ambient air intakes. The said alternative would be used to keep the air pressure moving through the said (B) 04 ambient air intakes and then through the said (B) 04 narrowing passageways. The said (B) 04 additional cylinder being used would be in unison with the drawing of the air stream of the cyclone narrowing cylinder-(E) 10 through the said (B) 04 narrowing passageways.
The narrowing spiral tube-(B) 04 alternative: The said (B) 04 would have an alternative with the means to open, close, partial open or adjust its angle on the said (B) 04 vortex nozzle, and or to use other kinds of narrowing passageways or nozzles.
The narrowing vortex cylinder-(G) 14 alternative: The said (G) 14 narrowing tube cold outlet would have an alternative to have an adjustable cold outlet valve near the inner top end of the said (G) 14 to adjust its cold air outward flow.
The radiation boiler chamber-(H) 16 alternative: The said (H) 16 would have the alternative with a sensor to adjust the amount of air-radiation heat, flowing through the said (H) 16. The said (H) 16 would have an alternative to use a release valve, adjusting the amount air-radiation heat, exiting the apparatus-(A) 02.
The cold air cooling chamber-(J) 18 alternative: The said (J) 18 would have the alternative with sensors to adjust the amount of cold air, flowing through the said (J) 18. The said (J) 18 would have alternative release outlet, to adjust it measurement of flow out, to be able to release its adjusted amount of cold air being released to exit the apparatus-(A) 02.
The steam turbine-(M) 24 alternative: The said (M) 24 would have the alternative of using any one of these different possible uses or use other different possible uses. The said (M) 24 turbine blades are of two basic types, blades and nozzles. Blades move entirely due to the impact of steam on them and their profiles do not converge. This results in a steam velocity drop and essentially no pressure drop as steam moves through the blades. A turbine composed of blades alternating with fixed nozzles is called an impulse turbine, Curtis turbine, Rateau turbine, or Brown-Curtis turbine. Nozzles appear similar to blades, but their profiles converge near the exit. This results in a steam pressure drop and velocity increase as steam moves through the nozzles. Nozzles move due to both the impact of steam on them and the reaction due to the high-velocity steam at the exit. A turbine composed of moving nozzles alternating with fixed nozzles is called a reaction turbine or Parsons Turbine.
The return water line-(P) 28 alternative: The said (P) 28 would have the alternative to be fitted with an check valve to prevent a water back-flow and alternative be fitted with an control valve to control its water level. The said sensor with the alternative would be to adjust and control the water temperature being release by the warm water pump-(R) 30.
The flash steam line-chamber-(V) 34 alternative: The said (V) 34 would have the alternative to use an added or an back up flash thermostatic valve-(T) 32 with an diverter valve, to divert and release its flash steam to exit the apparatus-(A) 02 if needed.
In describing a preferred embodiment of the invention illustrated in the drawings, specific terminology will be resorted to for the sake of clarity. However, the invention is not intended to be limited to the specific terms so selected, and it is to be understood that each specific term includes all technical equivalents which operate in a similar manner to accomplish a similar purpose.
The present description provides for the Vortex Turbine Engine also would be known as the apparatus-(A) 02: The said (A) 02 is a closed area that would have an opening at each one of the narrowing spiral tube-(B) 04 at its ambient air intakes, the radiation boiler chamber-(H) 16 at its air heat outlet, and the flash steam cooling air chamber-(K) 20 at its cold air outlet.
The said apparatus-(A) 02 comprises of the apparatus-NVCHACR-(NV) 02NV, the said radiation boiler chamber-(H) 16, the cold air cooling chamber-(J) 18, the said flash steam cooling air chamber-(K) 20, the radiation steam line-(L) 22, the steam turbine-(M) 24, the drive shaft-(N) 26, the return water line-(P) 28, the warm water pump-(R) 30, the flash thermostatic valve-(T) 32, the flash steam line-chamber-(V) 34, the flash water pump-(W) 36. The said (NV) 02NV comprises of: The said narrowing spiral tube-(B) 04, the narrowing volute generator-(C) 06, the fan chamber-(D) 08, the cyclone narrowing cylinder-(E) 10, the advance narrowing chamber-(F) 12, the narrowing vortex cylinder-(G) 14.
The said apparatus-NVCHACR-(NV) 02NV embodiment portion would be a closed area that would have an opening at each one of the said narrowing spiral tube-(B) 04 at its ambient air intakes, the said narrowing vortex cylinder-(G) 14 at its narrowing tube cold outlet, and the said (G) 14 at its adjustable hot outlet valve.
The said apparatus-(A) 02 would contain two or a plurality of the said narrowing spiral tube-(B) 04 with each one with an ambient air intake and an ingrained vortex nozzle. Each one of the said (B) 04 ambient air intakes is set at an angle to advance, generate, forming a vortex within each one of its one of the said (B) 04. The ambient air medium being drawn into each one of the said (B) 04 ambient air intakes, the air stream is being drawn in by the said cyclone narrowing cylinder-(E) 10.
Each one of the said narrowing spiral tube-(B) 04 converging portion has a greater diameter than the diverging portion, to enhance the vortices intensity. Each one of the said (B) 04 converging portion has a greater diameter than the diverging portion, to enhance the vortices intensity within each one of it's one of the said narrowing volute generator-(C) 06.
Each one of the said narrowing spiral tube-(B) 04 contains a vortex. Each one of the said (B) 04 vortex nozzle is set at an angle to advance, generate, forming a vortex within each one of its one of the said narrowing volute generator-(C) 06. The said (B) 04 with its air stream, the air stream would via its said vortex nozzle. Each one of the said (B) 04 vortex nozzle with its air stream, the air stream would via it's one of the said (C) 06.
The said apparatus-(A) 02 would contain two or a plurality of the said narrowing volute generator-(C) 06 with each one with an ingrained vortex nozzle. There would be the same amount of numbers of the said narrowing spiral tube-(B) 04 with its vortex nozzle as there are in numbers of the said narrowing volute generator-(C) 06 with its vortex nozzle. Each one of the said (C) 06 converging portion has a greater diameter than the diverging portion, to enhance its vortices intensity. Each one of the said (C) 06 contains a vortex.
The air stream is drawn circumventing into the said narrowing volute generator-(C) 06 and through its vortex nozzle. The said (C) 06 air stream gains velocity while circumventing, being drawn through the said (C) 06 and through its vortex nozzle. Each one of the said (C) 06 vortex nozzle with its air stream, the air stream would via the said fan chamber-(D) 08.
The said fan chamber-(D) 08 is connected to the said advance narrowing chamber-(F) 12. The said cyclone narrowing cylinder-(E) 10 joined to and would lay in-between the said (D) 08 within its inner wall. The said (E) 10 spin on its horizontal-axis between the diameter interior side walls of the said (D) 08. The said (D) 08 bottom converging portion being round has a greater diameter than the top portion being round, to enhance its air stream intensity. The said (D) 08 with its air stream, the air stream would via the said (E) 10.
The said cyclone narrowing cylinder-(E) 10 converts the mechanical energy from the cylinder motor, to energize the moving air stream. The energy of the said cylinder motor would energize the said (E) 10 through its rotating movement. The said (E) 10 air holes would energize its rotating movement with an angle to capture the kinetic energy. The said (E) 10 would be joined to and would lay in-between the said fan chamber-(D) 08 within its inner wall. The said (E) 10 would be joined to at the bottom of the said (D) 08.
The ambient air medium being drawn into each one of the said narrowing spiral tube-(B) 04 ambient air intakes, the air stream is being drawn in by the said cyclone narrowing cylinder-(E) 10. The air stream is then driven by the said (E) 10. The said (E) 10 converging portion would have a greater diameter than the diverging portion, to enhance the air flow intensity within the said advance narrowing chamber-(F) 12. The said (E) 10 with its forward driven air stream, the air stream would via the said (F) 12.
The said advance narrowing chamber-(F) 12 converging portion has a greater diameter than the diverging portion, to enhance the air flow intensity within each one of its narrowing tube air outlets. The said (F) 12 would contain two or a plurality of its narrowing tube air outlets. Each one of the said (F) 12 narrowing tube air outlets converging portion would have a greater diameter than the diverging portion, to enhance the vortices intensity within the said narrowing vortex cylinder-(G) 14.
Each one of the said advance narrowing chamber-(F) 12 narrowing tube air outlets would be connected to the said narrowing vortex cylinder-(G) 14. Each one of the said (F) 12 narrowing tube air outlets contains a vortex. The said fan chamber-(D) 08 is connected to the said (F) 12. The said (F) 12 with its air stream would be driven by the said cyclone narrowing cylinder-(E) 10.
The said advance narrowing chamber-(F) 12 with its air stream, the air stream would via its said narrowing tube air outlets. Each one of the said (F) 12 narrowing tube air outlets is set at an angle to advance, generate, and helps to form a vortex within the said narrowing vortex cylinder-(G) 14. Each one of the said (F) 12 narrowing tube air outlets with its air stream, the air stream would via the said (G) 14.
The said narrowing vortex cylinder-(G) 14 would separate its compressed air into an air-radiation heat stream and a cold stream. The said (G) 14 converging portion would have a greater diameter than the diverging portion, to enhance the vortices intensity, along with its air-radiation heat intensity of the vortex. The said (G) 14 contains a vortex.
The said narrowing vortex cylinder-(G) 14 having its temperatures, its temperatures would have a separation effect within its vortex. The said (G) 14, its vortex outer air-radiation heat temperature would separate from its inner cold air. The said (G) 14 with its temperatures separation effect would have the said vortex with an outer hot end releasing its air-radiation heat. The said (G) 14 with its temperatures separation effect would have its vortex with an inner cold end releasing its cold air.
The said narrowing vortex cylinder-(G) 14 would have an hot narrowing tube outlet at the outer top end of the said (G) 14. The said (G) 14 hot narrowing tube outlet converging portion would have a greater diameter than the diverging portion, to enhance the air-radiation heat intensity. The said (G) 14 hot narrowing tube outlet would have an adjustable hot outlet valve at the outer top end of the said (G) 14 to adjust its air-radiation heat outward flow.
The said narrowing vortex cylinder-(G) 14 with an outer hot end releasing its air-radiation heat, the air-radiation heat would via its hot narrowing tube outlet and would then via its adjustable hot outlet valve. The said (G) 14 having its adjustable hot outlet valve with its air-radiation heat, the air-radiation heat would via the said radiation boiler chamber-(H) 16.
The said narrowing vortex cylinder-(G) 14 would have an narrowing tube cold outlet near the outer top end of the said (G) 14. The said (G) 14 narrowing tube cold outlet be near the inner top end of the said (G) 14. The said (G) 14 with an inner cold end releasing its cold air, the cold air would via it's the said (G) 14 narrowing tube cold outlet. The said (G) 14 with its narrowing tube cold outlet, with its cold air, the cold air would via the said cold air cooling chamber-(J) 18.
The said air-radiation heat would be lying within the said radiation boiler chamber-(H) 16. The said radiation steam line-(L) 22 would be lying within the said (H) 16. The said (L) 22 with its warm water, the warm water would absorb the latent heat lying within the said (H) 16. The said warm water conversion to stream would be lying within the said (L) 22. The said (L) 22 would have a warm water-to-steam conversion. The said (H) 16 with its air-radiation heat within, the air-radiation heat would via its air heat outlet. The said (H) 16 with its air heat outlet with its air-radiation heat, the now cooler air-radiation heat would exit the said apparatus-(A) 02.
The said cold air cooling chamber-(J) 18 with its cold air stream, the cold air stream would absorb the latent heat from the hot water lying within the said return water line-(P) 28. The said (P) 28 would be lying within the said (J) 18. The said cold air would be lying within the said (J) 18. The said hot water would be lying within the said (P) 28. The said (P) 28 would have a hot-to-warm water conversion. The said (J) 18 with its cold air, the cold air would via the said flash steam cooling air chamber-(K) 20.
The said flash steam cooling air chamber-(K) 20 with its cold air, the cold air stream would absorb the flash steam latent heat lying within the said flash steam line-chamber-(V) 34. The said (V) 34 would be lying within the said (K) 20. The said cold air would be lying within the said (K) 20. Said flash steam heat would be lying within the said (V) 34. The said (V) 34 would have a steam-to-hot-warm water conversion. The said (K) 20 with its cold-warm air, the cold-warm air would via its cold air outlet. The said (K) 20 with its cold air outlet with its cold-warm air, the cold-warm air would exit the said apparatus-(A) 02.
The said warm water pump-(R) 30 with its warm water, pumps the warm water to via the said radiation steam line-(L) 22. The said (L) 22 with its warm water-to-steam conversion, the steam would via the said steam turbine-(M) 24. The said (M) 24 with its steam flow would generate a rotating motion force, forcing the said drive shaft-(N) 26 to rotate on its horizontal-axis producing torque.
The said drive shaft-(N) 26 would be joined to, being part of the said steam turbine-(M) 24. The said (M) 24 would have a steam turning back to hot water conversion. The said (M) 24 with its hot steam, the hot water of the steam would via the said return water line-(P) 28. The hot water coming from the said (M) 24, this hot water sometimes would flash evaporation (also known as flash steam).
The said return water line-(P) 28 with its flash steam, the flash steam would via the said flash thermostatic valve-(T) 32 with its diverter valve. The said (P) 28 with its hot water, the hot water that did not flash evaporate to flash steam would via toward the said warm water pump-(R) 30.
The said flash thermostatic valve-(T) 32 with its diverter valve, the diverter valve would divert the flash steam to via the said flash steam line-chamber-(V) 34. The said flash steam that would flash evaporation is released by the said (T) 32 with its diverter valve. The said (T) 32 diverter valve with its flash steam, the flash steam would via the said (V) 34.
The said flash steam line-chamber-(V) 34 with its steam-to-hot-warm water conversion, the hot-warm water would via the said flash water pump-(W) 36. The said (V) 34 with its steam-to-hot-warm water conversion, the hot-warm water would via the said (W) 36. The said (W) 36 with its hot-warm water, pumps the hot-warm water to via the said return water line-(P) 28. The said (W) 36 would pump this hot-warm water to via the said (P) 28 toward the said warm water pump-(R) 30.
The said return water line-(P) 28 with its hot water, the water that did not flash to flash steam lying within the said (P) 28 would via toward the said warm water pump-(R) 30. The said (P) 28 with its hot-to-warm water conversion, the warm water would via the said (R) 30.
The said warm water pump-(R) 30 with its warm water, pumps the warm water to via the said radiation steam line-(L) 22. The pumping causes a vacuum within the said return water line-(P) 28, drawing the said water toward the said (R) 30. The said (L) 22 with its warm water-to-steam conversion therefore commence the warm water-to-steam conversion cycle thereat.
While the invention is susceptible to embodiment in many different forms, as shown in the drawings and will be described to herein in detail, specific embodiments thereof with the understanding that the present disclosure is to be considered as an exemplification of the principles of the invention and is not to be limited to the specific embodiments described.
Each example is provided by way of explanation of the invention, not limitation of the invention. In fact, it will be apparent to those skilled in the art that various modifications and variations can be made in the present invention without departing from the scope or spirit of the invention.
For instance, features illustrated or described as component of one embodiment can be used with another embodiment to yield a still further embodiment.
Thus, it is intended that the present invention covers such modification and variations as come within the scope of the appended claims and their equivalents. It should be appreciated that the present invention is not limited to any particular type or style depicted in Figure's and is for illustrative purposes only.
Although preferred embodiments have been depicted and described in detail therein, it will be apparent to those skilled in the relevant art that various modifications, additions, substitutions and the like can be made without departing from the spirit of the invention and these are therefore considered to be within the scope of the invention as defined in the following claims. All water temperatures, pressurized steam, air temperatures, air velocity or air pressures used are an estimate, based on information attained.
One of these changes could be without departing from essence present invention, by having other kinds of air moving devices, such as using other kinds of engines, motors or multi-speed turbo fan motors to pull and drive the air stream into and through the apparatus. Having the motor placed in other locations, on, within or outside of the apparatus. Having the apparatus to use other kinds of, air blower holes or blades. There being other kinds of means to drive the apparatus other than electrically. Other kinds of power sources, like using solar energy. Use isolation material and formulation to reduce vibrations and dissipate shock energy for the motor and air mover.
Other change could be having the air intakes or air outlets, placed higher or lower, smaller or larger, more or less of them on the apparatus. There being other kinds of tubes or piping, or more vortexes or other kinds of on-off switches, nozzles, controllers, rate adjusters or other kinds of adjuster.
It is not practical to describe in claims all possible embodiments, Embodiments may be accomplished generally in keeping with present invention. Disclosure may include, separately or collectively, aspects described found throughout description of patent. While these may be added to explicitly include such details. Existing claims should construe to encompass such aspects.
To the extent methods claimed in present invention are not further discussed. Any such methods are natural outgrowths of the system or apparatus claims.
Therefore, separate and further discussions of the methods are deemed unnecessary. Otherwise claim steps implicit in use and manufacture or systems or apparatus claims.
Furthermore, steps organized in logical fashion and other sequences can and do occur. Therefore, method claims should not be construed to include only this order. Other order and sequence steps may be presented.
Notice: Subject to any disclaimer, the term of patent is extended or adjusted under 35 U.S.C. 154(b) by 501 days.
It is to be understood that the present invention is not limited to the embodiments described above, but encompasses any and all embodiments within the following scope of the following claims.
