Split-system heat-air conditioning

Abstract

A apparatus with 3 compressors converting gas pressure: Split-system heat-air conditioning comprising of: The apparatus for converting first gas having a medium low pressure gas being drawn by the compressor volute fan blade therefore the said gas via upstream to the 1st compressor the compressor volute hub converting to an increased gas pressure therefore the said gas via downstream to the 2nd compressor the velocity tube converting to an increasing this gas pressure therefore the said gas via downstream to the 3st compressor the compressor supersonic tube then increasing gas pressure gas again therefore the said gas via the inlet connection the pressure gas therefore via the counter flow vortex tube.

1 - 20 . (canceled) 
     
     
         21 . A apparatus comprising of: The apparatus comprises of; the impeller housing; the electric motor; the rotary axis; and the larger and more complex unit; the compressor volute hub; the compressor volute fan blade is a component of the said compressor volute hub; the said larger and more complex unit also includes; the compressor velocity tube; the compressor supersonic tube; the inlet connection; the counter flow vortex tube; the casing tube that is attached to the said counter flow vortex tube; and
 The said apparatus is suitable as a one, two, or an ample supply of units; and   The said larger and more complex unit also includes; the said compressor velocity tube; the said compressor supersonic tube; the said inlet connection; the said counter flow vortex tube; the said casing tube that is attached to the said counter flow vortex tube; and   The said electric motor remained stationary provides the power for the said rotary axis; the said electric motor with a configuration design and are joined to the said rotary axis having rotation; the said rotary axis is connected and provides the rotation for the said compressor volute hub having rotation with an ample supply of inlets; the said rotary axis and is configuration design to permit to and the rotation power to one, two, or an ample supply of the said larger and more complex unit; and   The said rotary axis is connected to and is a configuration design to be able to provide the rotary to the said compressor volute hub with an ample supply of the said compressor volute fan blade; and   Each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the said compressor volute hub 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 with having a de Lava nozzle opening; and   Each one of the ample supply of the said compressor volute fan blade draws in a medium low pressure gas air and therefore the upstream said gas via the said compressor volute fan blade; each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of the said compressor volute fan blade is configured to and communicate transporting downstream the gas as the said gas accelerating being channeled via and be connected to its one positioned on the said compressor volute hub, transporting the downstream said gas via the said compressor volute hub; the said compressor volute hub with rotation the said gas flow design to channel gas flow as passing over the said gas flow is channeled to via an inlet of the said compressor velocity tube as the downstream said gas flow passing over said inlet is now communicating transporting downstream the gas flow intercepting the next in line of the said inlets of the ample supply of inlets of the said compressor velocity tube as the said gas accelerating the downstream said gas via the joined said inlets of the said compressor velocity tube; and   Each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; and   The said compressor volute fan blade de Lava nozzle is connected to the one positioned on the said compressor volute hub inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub inlets; each one of ample supply of the said compressor volute hub channel has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the gas flows into the bell of the said compressor volute hub as rotary the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands with the transporting as the said gas accelerating, and the downstream said gas via its de Lava nozzle increasing its flow rate and the downstream said gas via the said compressor velocity tube joined to a lineup of inlets opening; and   The said compressor volute hub with each the said compressor volute hub having the inlet opening and an outlet opening to be configured to be and is joined to be in lineup with the designed inlets opening with the design of the stationary of the said compressor velocity vortex tube with a designed of a subsonic de Lava nozzle; and   There is an ample supply of the said compressor velocity tube remained stationary; each one of the said compressor velocity tube in communications transporting the gas also known as air and therefore the downstream said gas via and be connected to the said compressor supersonic tube remained stationary; there is an ample supply of the said compressor velocity tube, the said ample supply of the said inlets lead into just one outlet opening, the downstream said gas to via this one said outlet opening only; the said compressor velocity tube subsonic de Lava nozzle connected to the said compressor supersonic tube inlet opening; and   The said compressor velocity tube has ample supply of inlets; with each one having a channel with hollow core having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands; as the gas travels down the expansion part of the nozzle, the pressure and the temperature decrease, while the speed of the gas increases; the gas flows into the bell of the said compressor velocity tube with the transporting as the said gas accelerating, and the downstream said gas via its subsonic de Lava nozzle, increasing its flow rate and the downstream said gas via the said compressor supersonic tube opening imparting kinetic energy; and   The designed is to permit the whole entire of ample supply of the said compressor velocity tube permitting the gas is in communication to the said compressor supersonic tube; having the whole entire of ample supply of the said compressor velocity tube is connected to the said compressor supersonic tube; and   The said compressor supersonic tube remained stationary with a design; the channel with hollow core having straight parallel sides and a circular cross-section being hollow at the nozzle throat, where the cross-sectional area is the smallest; the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands; then the gas flows into the bell of the said compressor vortex tube then expands and goes supersonic; the said compressor supersonic tube having communication transporting the gas and via said gas and is permitting the gas downstream having communication and via the said inlet connection; and   The said compressor supersonic tube is permitting the gas downstream communication to the said inlet connection; the said inlet connection permitting the gas downstream communication to the said counter flow vortex tube; the said inlet connection is connected to the said counter flow vortex tube; and   The said inlet connection is permitting letting the gas downstream communication to the said counter flow vortex tube; the said counter flow vortex tube stationary design having and using the said casing tube; the said inlet connection remained stationary outlet opening permitting the gas downstream communication and therefore the downstream said gas via the said counter flow vortex tube remained stationary inlet opening; the said inlet connection is connected to the said counter flow vortex tube; the said casing tube is attached to the said counter flow vortex tube.   
     
     
         22 . The apparatus of claim  1  wherein: I Claim. The rotary axis is connected to and is a configuration design to be able to provide the rotary to the compressor volute hub with an ample supply of the compressor volute fan blade; and
 Each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the said compressor volute hub 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 with having a de Lava nozzle opening; and 
 Each one of the ample supply of the said compressor volute fan blade draws in a medium low pressure gas air and therefore the upstream said gas via the said compressor volute fan blade; each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of the said compressor volute fan blade is configured to and communicate transporting downstream the gas as the said gas accelerating being channeled via and be connected to its one positioned on the said compressor volute hub, transporting the downstream said gas via the said compressor volute hub; the said compressor volute hub with rotation the said gas flow design to channel gas flow as passing over the said gas flow is channeled to via an inlet of the compressor velocity tube as the downstream said gas flow passing over said inlet is now communicating transporting downstream the gas flow intercepting the next in line of the said inlets of the ample supply of inlets of the said compressor velocity tube as the said gas accelerating the downstream said gas via the joined said inlets of the said compressor velocity tube; and 
 Each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; and 
 The said compressor volute fan blade de Lava nozzle is connected to the one positioned on the said compressor volute hub inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub inlets; each one of ample supply of the said compressor volute hub channel has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the gas flows into the bell of the said compressor volute hub as rotary the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands with the transporting as the said gas accelerating, and the downstream said gas via its de Lava nozzle increasing its flow rate and the downstream said gas via the said compressor velocity tube joined to a lineup of inlets opening; and 
 The said compressor volute hub with each the said compressor volute hub having the inlet opening and an outlet opening to be configured to be and is joined to be in lineup with the designed inlets opening with the design of the stationary of the said compressor velocity vortex tube with a designed of a subsonic de Lava nozzle; and 
 There is an ample supply of the said compressor velocity tube remained stationary; each one of the said compressor velocity tube in communications transporting the gas also known as air and therefore the downstream said gas via and be connected to the compressor supersonic tube remained stationary; 
 there is an ample supply of the said compressor velocity tube, the said ample supply of the said inlets lead into just one outlet opening, the downstream said gas to via this one said outlet opening only; the said compressor velocity tube subsonic de Lava nozzle connected to the said compressor supersonic tube inlet opening; and 
 The said compressor velocity tube has ample supply of inlets; with each one having a channel with hollow core having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands; as the gas travels down the expansion part of the nozzle, the pressure and the temperature decrease, while the speed of the gas increases; the gas flows into the bell of the said compressor velocity tube with the transporting as the said gas accelerating, and the downstream said gas via its subsonic de Lava nozzle, increasing its flow rate and the downstream said gas via the said compressor supersonic tube opening imparting kinetic energy; and 
 The designed is to permit the whole entire of ample supply of the said compressor velocity tube permitting the gas is in communication to the said compressor supersonic tube; having the whole entire of ample supply of the said compressor velocity tube is connected to the said compressor supersonic tube; and 
 The said compressor supersonic tube remained stationary with a design; the channel with hollow core having straight parallel sides and a circular cross-section being hollow at the nozzle throat, where the cross-sectional area is the smallest; the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands; then the gas flows into the bell of the said compressor vortex tube then expands and goes supersonic; the said compressor supersonic tube having communication transporting the gas and via said gas and is permitting the gas downstream exiting. 
 
     
     
         23 . The apparatus of claim  1  wherein: The rotary axis is connected to and is a configuration design to be able to provide the rotary to the compressor volute hub with an ample supply of the compressor volute fan blade; and
 Each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional a rea is the smallest; the said compressor volute hub 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 with having a de Lava nozzle opening; and 
 Each one of the ample supply of the said compressor volute fan blade draws in a medium low pressure gas air and therefore the upstream said gas via the said compressor volute fan blade; each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of the said compressor volute fan blade is configured to and communicate transporting downstream the gas as the said gas accelerating being channeled via and be connected to its one positioned on the said compressor volute hub, transporting the downstream said gas via the said compressor volute hub; the said compressor volute hub with rotation the said gas flow design to channel gas flow as passing over the said gas flow is channeled to via an inlet of the compressor velocity tube as the downstream said gas flow passing over said inlet is now communicating transporting downstream the gas flow intercepting the next in line of the said inlets of the ample supply of inlets of the said compressor velocity tube as the said gas accelerating the downstream said gas via the joined said inlets of the said compressor velocity tube; and 
 Each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; and 
 The said compressor volute fan blade de Lava nozzle is connected to the one positioned on the said compressor volute hub inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub inlets; each one of ample supply of the said compressor volute hub channel has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the gas flows into the bell of the said compressor volute hub as rotary the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands with the transporting as the said gas accelerating, and the downstream said gas via its de Lava nozzle increasing its flow rate and the downstream said gas via the said compressor velocity tube joined to a lineup of inlets opening; and 
 The said compressor volute hub with each the said compressor volute hub having the inlet opening and an outlet opening to be configured to be and is joined to be in lineup with the designed inlets opening with the design of the stationary of the said compressor velocity vortex tube with a designed of a subsonic de Lava nozzle; and 
 There is an ample supply of the said compressor velocity tube remained stationary; each one of the said compressor velocity tube in communications transporting the gas also known as air and therefore the downstream said gas via and be connected to the compressor supersonic tube remained stationary; there is an ample supply of the said compressor velocity tube, the said ample supply of the said inlets lead into just one outlet opening, the downstream said gas to via this one said outlet opening only; and 
 The said compressor velocity tube has ample supply of inlets; with each one having a channel with hollow core having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands; as the gas travels down the expansion part of the nozzle, the pressure and the temperature decrease, while the speed of the gas increases; the gas flows into the bell of the said compressor velocity tube with the transporting as the said gas accelerating, and the downstream said gas via its subsonic de Lava nozzle, increasing its flow rate; the designed is to permit the whole entire of ample supply of the said compressor velocity tube permitting the gas downstream exiting. 
 
     
     
         24 . The apparatus of claim  1  wherein: The rotary axis is connected to and is a configuration design to be able to provide the rotary to the compressor volute hub with an ample supply of the compressor volute fan blade; and
 Each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the said compressor volute hub 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 with having a de Lava nozzle opening; and 
 Each one of the ample supply of the said compressor volute fan blade draws in a medium low pressure gas air and therefore the upstream said gas via the said compressor volute fan blade; each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of the said compressor volute fan blade is configured to and communicate transporting downstream the gas as the said gas accelerating being channeled via and be connected to its one positioned on the said compressor volute hub, transporting the downstream said gas via the said compressor volute hub; the said compressor volute hub with rotation the said gas flow design to channel gas flow as passing over the said gas flow is channeled to via an inlet permitting the gas downstream exit as the downstream said gas flow passing over said inlet is now communicating transporting downstream the gas flow intercepting the next in line of the said inlets of the ample supply of inlets permitting the gas downstream exit as the said gas accelerating the downstream said gas via the joined said inlets permitting the gas downstream exit; and 
 Each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; and 
 The said compressor volute fan blade de Lava nozzle is connected to the one positioned on the said compressor volute hub inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub inlets; each one of ample supply of the said compressor volute hub channel has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the gas flows into the bell of the said compressor volute hub as rotary the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands with the transporting as the said gas accelerating, and the downstream said gas via its de Lava nozzle increasing its flow rate and the downstream said gas permitting the gas downstream exit the joined to a lineup of inlets opening; and 
 The said compressor volute hub with each the said compressor volute hub having the inlet opening and an outlet opening to be configured to be and is joined to be in lineup with the designed inlets opening permitting the gas downstream exiting. 
 
     
     
         25 . The apparatus of claim  1  wherein: The rotary axis is connected to and is a configuration design to be able to provide the rotary to the compressor volute hub with an ample supply of the compressor volute fan blade; and
 Each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the said compressor volute hub 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 with having a de Lava nozzle opening; and 
 Each one of the ample supply of the said compressor volute fan blade draws in a medium low pressure gas air and therefore the upstream said gas via the said compressor volute fan blade; each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of the said compressor volute fan blade is configured to and communicate transporting downstream the gas as the said gas accelerating being channeled via and be connected to its one positioned on the said compressor volute hub, transporting the downstream said gas via the said compressor volute hub; the said compressor volute hub with rotation the said gas flow design to channel gas flow as passing over the said gas flow is channeled to via an inlet as the downstream said gas flow passing over said inlet is now communicating transporting downstream the gas flow intercepting the next in line of the said inlets of the ample supply of inlets as the said gas accelerating the downstream said gas via the joined said inlets and 
 Each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; and 
 The said compressor volute fan blade de Lava nozzle is connected to the one positioned on the said compressor volute hub inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub inlets; each one of ample supply of the said compressor volute hub channel has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the gas flows into the bell of the said compressor volute hub as rotary the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands with the transporting as the said gas accelerating, and the downstream said gas via its de Lava nozzle increasing its flow rate and the downstream said gas via the joined to a lineup of inlets opening; and 
 The said compressor volute hub with each the said compressor volute hub having the inlet opening and an outlet opening to be configured to be and is joined to be in lineup with the designed inlets opening permitting the gas downstream exiting. 
 
     
     
         26 . The apparatus of claim  1  wherein: Each one of the compressor volute fan blade is a component of the compressor volute hub; each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the said compressor volute hub 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 with having a de Lava nozzle opening; and
 Each one of the ample supply of the said compressor volute fan blade draws in a medium low pressure gas air and therefore the upstream said gas via the said compressor volute fan blade; each one of the said compressor volute fan blade is a component of the said compressor volute hub; each one of the said compressor volute fan blade is configured to and communicate transporting downstream the gas as the said gas accelerating being channeled via and be connected to its one positioned on the said compressor volute hub, transporting the downstream said gas via the said compressor volute hub; the said compressor volute hub with rotation the said gas flow design to channel gas flow as passing over the said gas flow is channeled to via an inlet as the downstream said gas flow passing over said inlet is now communicating transporting downstream the gas flow intercepting the next in line of the said inlets of the ample supply of inlets as the said gas accelerating the downstream said gas via the joined said inlets; and 
 Each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; and 
 The said compressor volute fan blade de Lava nozzle is connected to the one positioned on the said compressor volute hub inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub inlets; each one of ample supply of the said compressor volute hub channel has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the gas flows into the bell of the said compressor volute hub as rotary the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands with the transporting as the said gas accelerating, and the downstream said gas via its de Lava nozzle increasing its flow rate and the downstream said gas via the joined to a lineup of inlets opening; and 
 The said compressor volute hub with each the said compressor volute hub having the inlet opening and an outlet opening to be configured to be and is joined to be in lineup with the designed inlets opening permitting the gas downstream exiting. 
 
     
     
         27 . The apparatus of claim  1  wherein: There is an ample supply of the compressor velocity tube remained stationary; each one of the said compressor velocity tube in communications transporting the gas also known as air and therefore the downstream said gas via; there is an ample supply of the said compressor velocity tube, the said ample supply of the said inlets lead into just one outlet opening, the downstream said gas to via this one said outlet opening only; the said compressor velocity tube having an subsonic de Lava nozzle; and
 The said compressor velocity tube has ample supply of inlets; with each one having a channel with hollow core having straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands; as the gas travels down the expansion part of the nozzle, the pressure and the temperature decrease, while the speed of the gas increases; the gas flows into the bell of the said compressor velocity tube with the transporting as the said gas accelerating, and the downstream said gas via its subsonic de Lava nozzle, increasing its flow rate imparting kinetic energy; and 
 The designed is to permit the whole entire of ample supply of the said compressor velocity tube permitting the gas is in communication having the whole entire of ample supply of the said compressor velocity tube permitting the gas downstream exiting. 
 
     
     
         28 . The apparatus of claim  1  wherein: Each one of the compressor volute hub channels; the said compressor volute hub with an ample supply of inlets; with each inlet there is an outlet; and
 The said compressor volute hub, transporting the downstream said gas via the said compressor volute hub; the said compressor volute hub with rotation the said gas flow design to channel gas flow as passing over the said gas flow is channeled to via an inlet as the downstream said gas flow passing over said inlet is now communicating transporting downstream the gas flow intercepting the next in line of the said inlets of the ample supply of inlets as the said gas accelerating the downstream said gas via the joined said inlets and the one positioned on the said compressor volute hub inlet opening, are configuration design to permit incoming ambient downstream gas permitting gas to communicate to each one of the said compressor volute hub inlets; and 
 Each one of ample supply of the said compressor volute hub channel has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a straight parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; and 
 The gas flows into the bell of the said compressor volute hub as rotary the lower atmospheric pressure, back pressure, causes the gas stream to accelerate therefore the gases expands with the transporting as the said gas accelerating, and the downstream said gas via its de Lava nozzle increasing its flow rate and the downstream said gas via the joined to a lineup of inlets opening; and 
 The said compressor volute hub with each the said compressor volute hub having the inlet opening and an outlet opening to be configured to be and is joined to be in lineup with the designed inlets opening permitting the gas downstream exiting. 
 
     
     
         29 . The apparatus of claim  1  wherein: Each one of ample supply of the compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; and
 Each one of the ample supply of the said compressor volute fan blade draws in a medium low pressure gas air and therefore the upstream said gas via the said compressor volute fan blade; and 
 Each one of ample supply of the said compressor volute fan blade has a convergent inlet the wide end and divergent outlet the smallest end; with each one having a channel with hollow core having a curve parallel sides, circular cross-section being hollow at the nozzle throat, is where the cross-sectional area is the smallest; and 
 Each one of the said compressor volute fan blade is configured to and communicate transporting downstream the gas as the said gas accelerating being channeled permitting the gas downstream exiting. 
 
     
     
         30 . The apparatus of claim  1  wherein: The apparatus is suitable as a one, two, or an ample supply of units. 
     
     
         31 . The apparatus of claim  1  wherein: The larger and more complex unit also includes; the compressor velocity tube; the compressor supersonic tube; the inlet connection; the counter flow vortex tube; the casing tube that is attached to the said counter flow vortex tube.