Patent Application
20210215162
The Split-System Heat-Air Conditioning: An apparatus useful for heating and cooling: Idea suitable for an ample supply of uses; to be use in residential, commercial or industrial, low/high-rise buildings, retail stores, educational facilities, hospitals, automobiles, commercial or industrial vehicles; an air conditioning system creating hot and cold air “gas” at the same time.
The apparatus 2 uses no refrigerant of any kind for its cooling and heating the said apparatus 2, being non-polluting energy-efficient, and has only 3 moving components, the electric motor 4 to provides the rotary power, the rotary axis 6 is connected and provides the rotary to the said compressor volute hub 8 and the throttle valve 30, meeting all of the requirements by any regulatory body and in with the accordance with any regulations that impacting the HVAC industry.
The Split-System Heat-Air Conditioning: also known as; Split-System Heat-Air Conditioning apparatus 2 and known as the apparatus 2 and the gas are also known as air; the said apparatus 2 relate to gas, mixture mainly of oxygen and nitrogen. There is a great deal of empty space between particles, which have a lot of kinetic energy. The particles exert more force on the interior volume of the container. The components are known as; the electric motor 4, the rotary axis 6, the compressor volute fan blade 12 an component of the compressor volute hub 8, the impeller housing 10 supports the weight of the said apparatus 2, the compressor velocity tube 14, the compressor supersonic tube 16, the inlet connection 18 and the counter flow vortex tube 20 and the casing tube 32 that is attached to the said counter flow vortex tube 20; and.
The said electric motor 4 remained stationary provides the power to the and for the said rotary axis 6. The said electric motor 4 and are configuration design to be and are joined to the said rotary axis 6 being rotary. The said rotary axis 6 is connected to and is a configuration design to be able to provide the rotary to the said compressor volute hub 8 with an ample supply of the said compressor volute fan blade 12. Each one of the said compressor volute fan blade 12 is a component of the said compressor volute hub 8. The said compressor volute hub 8 with an ample supply of inlets; with each inlet there is an outlet, with each one of the said inlets is connected to its one positioned on the said compressor volute fan blade 12 with having a de Lava nozzle outlet opening; and.
Each one of the said compressor volute fan blade 12 draws in a medium low pressure gas also known as air and therefore the said gas via upstream and therefore the said gas via the said compressor volute fan blade 12. Each one of the said compressor volute fan blade 12 is configured to and communicate transporting downstream the gas as the said gas accelerating within and therefore the said gas via and be connected to its one positioned on the said compressor volute hub 8 inlets opening, therefore transporting gas through and then the said gas via the said compressor volute hub 8 outlet openings. The said compressor volute hub 8 as rotary the said gas to via and as the said gas therefore passing over and communicating transporting downstream gas, the said gas is accelerating, the said compressor volute hub 8 outlets opening is joined to a lineup of inlets opening of the said compressor velocity tube 14; and.
The said compressor volute fan blade 12 outlet is connected to it's one of the said compressor volute hub 8 inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub 8 inlets. The gas flows into the bell of the said compressor volute hub 8 therefore its gases expands with the transporting as the said gas accelerating, and therefore the said gas via its de Lava nozzle outlet increasing its flow rate and therefore the said gas via the said compressor velocity tube 14 opening. The lower atmospheric pressure, “back pressure” causes the gas stream to accelerate. The said compressor volute hub 8 has ample supply of inlets; with each one with having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest. As the gas travels down the expansion part of the nozzle, the pressure and the temperature decrease, while the speed of the gas increases.
There is an ample supply of the compressor velocity tube 14 remained stationary. Each one of the said compressor velocity tube 14 in communications transporting the gas also known as air and therefore the said gas via and be connected to the compressor supersonic tube 16. There is an ample supply of the said compressor velocity tube 14 remained stationary; the said compressor velocity tube 14 has ample supply having all outlets into one outlet opening. Each one of the said compressor velocity tube 14 has the same outlet connected to the said compressor supersonic tube 16 inlet opening; and
The gas flows into the bell of the said compressor velocity tube 14 therefore its gases expands with the transporting as the said gas accelerating, and therefore the said gas via its subsonic de Lava nozzle outlet, increasing its flow rate and therefore the said gas via the said compressor supersonic tube 16 opening imparting kinetic energy. The lower atmospheric pressure, “back pressure” causes the gas stream to accelerate. The said compressor velocity tube 14 has ample supply of inlets; with each one with having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest. As the gas travels down the expansion part of the nozzle, the pressure and temperature decrease, while the speed of the gas increases; and.
Having the entire of ample supply of the said compressor velocity tube 14 is connected having all outlets into one outlet therefore via the said compressor supersonic tube 16 remained stationary. To optimally designed so as to convert the potential energy in the form of pressurized gas into a highest state of kinetic energy in the form of moving gas particles.
The gas flows into the bell of the compressor supersonic tube 16 therefore its gases expands with the transporting as the said gas accelerating, and therefore the said gas via its supersonic de Lava nozzle outlet increasing its flow rate and therefore the said gas via the inlet connection 18 opening imparting kinetic energy. The lower atmospheric pressure, “back pressure” causes the gas stream to accelerate. The said compressor supersonic tube 16 with having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest. As the gas also known as air travels down the expansion part of the nozzle, the pressure and temperature decrease, while the speed of the gas increases.
The inlet connection 18 remained stationary permitting the gas downstream communication and therefore the said gas via the counter flow vortex tube 20 remained stationary. The said inlet connection 18 is connected to the said counter flow vortex tube 20 and the casing tube 32 that is attached to the said counter flow vortex tube 20. To optimally designed to impart kinetic energy.
The rotary axis 6 is connected to the compressor volute hub 8. The rotary axis 6 provides the rotary to the said compressor volute hub 8. The said compressor volute hub 8 is a component of the unit U8. The said unit U8 is suitable as a one, two, or an ample supply of units. The said rotary axis 6 and with configuration design to permit and provides the rotary to one, two, or an ample supply of the said unit U8.
FIRST compressor: “
The said compressor volute fan blade 12 outlet is connected to it's one of the said compressor volute hub 8 inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub 8 inlets. The gas flows into the bell of the said compressor volute hub 8 therefore its gases expands with the transporting as the said gas accelerating, and therefore the said gas via its de Lava nozzle outlet increasing its flow rate and therefore the said gas via the said compressor velocity tube 14 opening. The lower atmospheric pressure, “back pressure” causes the gas stream to accelerate. The said compressor volute hub 8 has ample supply of inlets; with each one with having an outlet opening. As the gas travels down the expansion part of the nozzle, the pressure and the temperature decrease, while the speed of the gas increases.
SECOND compressor: “
The gas flows into the bell of the said compressor velocity tube 14 therefore its gases expands with the transporting as the said gas accelerating, then therefore exiting its subsonic de Lava nozzle outlet, increasing its flow rate and therefore the said gas via the said compressor supersonic tube 16 opening imparting kinetic energy. The lower atmospheric pressure, “back pressure” causes the gas stream to accelerate. The said compressor velocity tube 14 has ample supply of inlets; having an outlet opening. As the gas travels down the expansion part of the nozzle, the pressure and temperature decrease, while the speed of the gas increases. Having the entire of ample supply of the said compressor velocity tube 14 is connected having all outlets into one outlet therefore via the said compressor supersonic tube 16 remained stationary.
THIRD compressor 3: “
The inlet connection 18 permitting the gas downstream communication and therefore the said gas via the counter flow vortex tube 20 remained stationary. The said inlet connection 18 is connected to the said counter flow vortex tube 20.
Split-System Heat-Air Conditioning: also known as a Split-System Heat-Air Conditioning apparatus 2 and also known as an apparatus 2—electric motor 4—rotary axis 6—compressor volute hub 8—impeller housing 10—compressor volute fan blade 12—compressor velocity tube 14—compressor supersonic tube 16—inlet connection 18—counter flow vortex tube 20—cold nozzle 22—cool gas product outlet 24—apertures 26—hot air exit 28—throttle valve 30—casing tube 32—converging-diverging tube 34—primary swirl chamber 36—primary transition zone 38—tube wall 40—short section 42—stability chamber 44—boundary layer nozzles 46—outer tube 48—secondary transition zone 50—gas separator 52.
Cross-sectional of
Bernoulli equation: States that, here points 1 and 2 lie on a streamline, the gas has constant density, the flow is steady, and there is no friction. Pressure/velocity variation: Consider the steady, flow of a constant density gas in a converging duct, without losses due to friction. The flow therefore satisfies all the restrictions governing the use of Bernoulli's equation. Upstream and downstream of the contraction we make the one-dimensional assumption that the velocity is constant over the inlet and outlet areas and parallel. When streamlines are parallel the pressure is constant across them, except for hydrostatic head differences (if the pressure was higher in the middle of the duct, for example, we would expect the streamlines to diverge, and vice versa). If we ignore gravity, then the pressures over the inlet and outlet areas are constant. Along a streamline on the centerline, the Bernoulli equation and the one-dimensional continuity equation give, respectively. Bernoulli equation used in the apparatus 2. Bernoulli equation used in the compressor volute fan blade 12, the compressor velocity tube 14 and the compressor supersonic tube 16.
Bernoulli principle: The correlation between gas speed and pressure, as speed increases pressure decreases, as the gas is curving. The continuous change of position of a body of gas stream curving so that every partied of the body follows a straight-line path. Bernoulli equation is used in the apparatus 2. Bernoulli principle is used in the compressor volute fan blade 12 the compressor velocity tube 14 and the compressor supersonic tube 16.
Convergent-divergent type of nozzle: Nozzles are actually used to modify the flow of a gas (i.e. by increasing kinetic energy of the flow in expense of its pressure). Convergent-divergent type of nozzles; mostly used for supersonic flows because it is impossible to create supersonic flows in convergent type of nozzles and therefore it restricts us to a limited amount of mass flow through a particular nozzle. In convergent-divergent type of nozzles we can increase the flow velocity much higher than sonic velocity that is why these types of nozzles have a wide application such as propelling nozzles in jet engines or in gas intake for engines working at high rpms. Convergent-divergent type of nozzles is used in the compressor volute fan blade 12, the compressor velocity tube 14 and the compressor supersonic tube 16.
Converging and diverging portions: 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 gas stream to accelerate. By reducing the pressure of the gases 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. Converging and diverging portions is used in the apparatus 2, converging and diverging portions and use in the compressor volute fan blade 12, the compressor velocity tube 14 and the compressor supersonic tube 16.
A de Lava nozzle (or convergent-divergent nozzle, CD nozzle or con-di nozzle) is a tube that is pinched in the middle, making a carefully balanced, asymmetric hourglass shape. In a subsonic flow sound will propagate through the gas. At the “throat”, where the cross-sectional area is at its minimum, the gas velocity locally becomes sonic (Mach number=1.0), a condition called choked flow. In a supersonic de Lava with nozzle: It is used to accelerate a hot, pressurized gas passing through it to a higher supersonic speed in the axial (thrust) direction, by converting the heat energy of the flow into kinetic energy. These de Lava nozzles are uses in the compressor volute fan blade 12, the compressor velocity tube 14 and the compressor supersonic tube 16.
A de Laval type nozzle: A nozzle is a relatively simple device, just a specially shaped tube through which hot gas flow. At the “throat”, where the cross-sectional area is at its minimum, the gas velocity locally becomes sonic (Mach number=1.0), a condition called choked flow. As the nozzle cross-sectional area increases, the gas begins to expand and the gas flow increases to supersonic velocities where a sound wave will not propagate backwards through the gas as viewed in the frame of reference of the nozzle (Mach number>1.0). This nozzle configuration is called a convergent-divergent, or CD, nozzle. These de Lava nozzles are used in the compressor volute fan blade 12, the compressor velocity tube 14 and the compressor supersonic tube 16.
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 gas 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 flow vortex tube with the vortex nozzle and the uni-flow vortex tube. The counter flow vortex tube 20 is similar to with many characterize of the counter flow vortex tube with the vortex nozzle. The said counter flow vortex tube 20 used in the apparatus 2.
Compressor 1: The rotary axis 6 is connected to the compressor volute hub 8. The compressor volute fan blade 12; is a component of the said compressor volute hub 8. Each one of the ample supply of the said compressor volute fan blade 12 is attached to its one positioned on the said compressor volute hub 8. Each one of the said compressor volute fan blade 12 outlets opening is connected to its one positioned on the said compressor volute hub 8 inlet opening; and.
Each one of the said ample supply of the said compressor volute fan blade 12; with each one communication transporting and therefore the upstream gas via the said compressor volute fan blade 12 inlet openings. An ample supply of the said compressor volute fan blade 12 permitting the said ambient gas to communication downstream and therefore the said gas via the said compressor volute hub 8 inlets opening, with its outlet opening, the outlet opening passes over the compressor velocity tube 14 inlet opening imparting kinetic energy; and
Each one of the said compressor volute fan blade 12 connected to its one positioned on the said compressor volute hub 8. Each one of the said compressor volute fan blade 12 connected to its one positioned on the said compressor volute hub 8. Each of the said compressor volute hub 8 being; round with an inlet and outlet opening. The said compressor volute fan blade 12 between and adjacent to the volutes of the said compressor volute fan blade 12 accelerate the gas which is drawn thereto from openings between peripherally adjacent channel, and direct that accelerated gas speed; and
The said compressor volute fan blade 12 are configuration design to permit the said compressor volute hub 8 with an ample supply of inlet opening with its outlet opening, the outlet opening passes over in communication transporting and therefore the said gas via therefore passing over and is joined to said openings, the gas as passing the gas to communication to the whole entire of ample supply of the remained stationary in lineup with said inlet openings of the said compressor velocity tube 14 imparting kinetic energy.
Compressor 2: The ample supply of with a designed of the compressor velocity tube 14 permitting the gas to communication and therefore the said gas via the compressor supersonic tube 16. The said compressor velocity tube 14; communication transporting and therefore the said gas via the said compressor supersonic tube 16 imparting kinetic; and.
Having whole entire of ample supply of the said compressor velocity tube 14 is permitting the gas to communication and therefore the said gas via the said compressor supersonic tube 16. The said whole entire of ample supply of the said compressor velocity tube 14 is connected having all outlets into one outlet therefore via the said compressor supersonic tube 16 to impart kinetic energy.
Compressor 3: The compressor supersonic tube 16 and communication transporting and therefore the said gas via the inlet connection 18. The said inlet connection 18; is permitting the gas to communication and therefore the said gas via the counter flow vortex tube 20 to impart kinetic energy.
The Split-System Heat-Air Conditioning: also known as; Split-System Heat-Air Conditioning apparatus 2 and gas also known as: The apparatus 2 is capable of providing hot and cold gas thereof is upon demand. The said apparatus 2 relate to gas, mixture mainly of oxygen and nitrogen. There is a great deal of empty space between particles, which have a lot of kinetic energy. The said apparatus 2 is designed suitable as a one, two, or with an ample supply of units.
The Split-System Heat-Air Conditioning: also known as; Split-System Heat-Air Conditioning apparatus 2 and known as the apparatus 2 and the gas are also known as air: The components are known as; the electric motor 4, the rotary axis 6, the compressor volute fan blade 12 an component of the compressor volute hub 8, the impeller housing 10 supports the weight of the said apparatus 2, the compressor velocity tube 14, the compressor supersonic tube 16, the inlet connection 18 and the counter flow vortex tube 20 and the casing tube 32.
The said compressor volute hub 8 is a component of the unit U8. The said unit U8 is suitable as a one, two, or an ample supply of units. The rotary axis 6 and are configuration design to provide the rotary to one, two, or an ample supply of the said unit U8. A unit is an individual component of a larger or more complex whole. The said unit U8 also known as: larger and more complex unit.
The apparatus 2 has only 3 moving components: Moving components are with a configuration design of the electric motor 4 remained stationary provides the rotary power to be able rotary and are configuration design to permit to be and is joined to the rotary axis 6 and the said rotary axis 6 is connected to and provides the rotary to the compressor volute hub 8. The other moving component is the throttle valve 30 “also known as cone valve” a movement in changing position. The said throttle valve 30 is a component of the counter flow vortex tube 20.
The apparatus 2 comprises of: The impeller housing 10; the electric motor 4; the rotary axis 6; and the unit U8: The said unit U8 comprises of and also known as a: larger and more complex unit. The compressor volute hub 8; the compressor volute fan blade 12 is a component of the said compressor volute hub 8; the said unit U8 also includes: The compressor velocity tube 14; the compressor supersonic tube 16; the inlet connection 18; the counter flow vortex tube 20; the casing tube 32 that is attached to the said counter flow vortex tube 20.
The electric motor 4 remained stationary provides the power to the rotary axis 6. The said electric motor 4 and are configuration design to be and are joined to the said rotary axis 6 being rotary. The said rotary axis 6 is connected and provides the rotary to the said compressor volute hub 8 being rotary with an ample supply of inlets. The said rotary axis 6 and is configuration design to permit to and provides the rotary powers to one, two, or an ample supply of the unit U8, also known as: larger and more complex unit.
The said electric motor 4 remained stationary provides the power to the and for the said rotary axis 6. The said electric motor 4 and are configuration design to be and are joined to the said rotary axis 6 being rotary. The said rotary axis 6 is connected to and is a configuration design to be able to provide the rotary to the said compressor volute hub 8 with an ample supply of the said compressor volute fan blade 12.
Each one of the said compressor volute fan blade 12 is a component of the said compressor volute hub 8. The said compressor volute hub 8 with an ample supply of inlets; with each inlet there is an outlet, with each one of the said inlets is connected to its one positioned on the said compressor volute fan blade 12 with having a de Lava nozzle outlet opening; and.
Each one of the said compressor volute fan blade 12 draws in a medium low pressure gas also known as air and therefore the said gas via upstream and therefore the said gas via the said compressor volute fan blade 12. Each one of the said compressor volute fan blade 12 is configured to and communicate transporting downstream the gas as the said gas accelerating within and therefore the said gas via and be connected to its one positioned on the said compressor volute hub 8 inlets opening, therefore transporting gas through and then the said gas via the said compressor volute hub 8 outlet openings. The said compressor volute hub 8 as rotary the said gas to via and as the said gas therefore passing over and communicating transporting downstream gas, the said gas is accelerating, the said compressor volute hub 8 outlets opening is joined to a lineup of inlets opening of the said compressor velocity tube 14; and.
The said compressor volute fan blade 12 outlet is connected to it's one of the said compressor volute hub 8 inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub 8 inlets. The gas flows into the bell of the said compressor volute hub 8 as rotary therefore its gases expands with the transporting as the said gas accelerating, and therefore the said gas via its de Lava nozzle outlet increasing its flow rate and therefore the said gas via the said compressor velocity tube 14 joined to a lineup of inlets opening; and.
The lower atmospheric pressure, “back pressure” causes the gas stream to accelerate. The said compressor volute hub 8 has ample supply of inlets; with each one with having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest. As the gas travels down the expansion part of the nozzle, the pressure and the temperature decrease, while the speed of the gas increases.
There is an ample supply of the compressor velocity tube 14 remained stationary. Each one of the said compressor velocity tube 14 in communications transporting the gas also known as air and therefore the said gas via and be connected to the compressor supersonic tube 16; there being the entire of the ample supply of the said compressor velocity tube 14, the entire of the ample supply of the said compressor velocity tube 14 and all of the said entire of the ample supply having all outlets into one outlet the said gases is permitting to communicate and therefore via the said compressor supersonic tube 16; and.
The gas flows into the bell of the said compressor velocity tube 14 therefore its gases expands with the transporting as the said gas accelerating, and therefore the said gas via its subsonic de Lava nozzle outlet, increasing its flow rate and therefore the said gas via the said compressor supersonic tube 16 opening imparting kinetic energy; and.
The lower atmospheric pressure, “back pressure” causes the gas stream to accelerate. The said compressor velocity tube 14 has ample supply of inlets; with each one with having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest. As the gas travels down the expansion part of the nozzle, the pressure and temperature decrease, while the speed of the gas increases; and.
Having the entire of ample supply of the said compressor velocity tube 14 is connected having all outlets into one outlet therefore via the said compressor supersonic tube 16 remained stationary. To optimally designed so as to convert the potential energy in the form of pressurized gas into a highest state of kinetic energy in the form of moving gas particles.
The gas flows into the bell of the compressor supersonic tube 16 therefore its gases expands with the transporting as the said gas accelerating, and therefore the said gas via its supersonic de Lava nozzle outlet increasing its flow rate and therefore the said gas via the inlet connection 18 opening imparting kinetic energy. The lower atmospheric pressure, “back pressure” causes the gas stream to accelerate. The said compressor supersonic tube 16 with having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest. As the gas also known as air travels down the expansion part of the nozzle, the pressure and temperature decrease, while the speed of the gas increases.
The inlet connection 18 remained stationary outlet opening permitting the gas downstream communication and therefore the said gas via the counter flow vortex tube 20 remained stationary inlet opening. The said inlet connection 18 is connected to the said counter flow vortex tube 20 and the casing tube 32 that is attached to the said counter flow vortex tube 20. To optimally designed to impart kinetic energy.
The compressor supersonic tube 16 outlet opening is designed and is connected to and is and therefore in gas communication downstream in therefore via the inlet opening connection 18 outlet opening is connected to and is therefore the said gases to communication downstream and therefore via the counter flow vortex tube 20 inlets opening to impart kinetic energy; and.
The said compressor supersonic tube 16 is optimally designed so as to convert the potential energy in the form of pressurized gas into the highest state of kinetic energy in the form of moving gas particles. The gas and therefore via the said inlet connection 18 and is therefore the said gas via through the said counter flow vortex tube 20, which houses the boundary layer nozzles 46 optimally designed so as to convert the potential energy in the form of pressurized gas into the highest state of kinetic energy in the form of moving gas particles.
