A) Heat the Emulsified Air and Atomized liquid gasoline fragments together to initiate a "Phase Change" from a liquid form into a completely gaseous state, .................................
B) Further emulsify the now heated gaseous Gasoline vapor with the now heated Ambient Air in the 30 Heat Exchanger Tubes, to create a completely Homogenous Air / Fuel Mixture flowing at a high velocity,
8) Final Heating, the Homogenous Hot Air and Gasoline Vapor mixture then comes into contact with the even HOTER Combustion Chamber components, which have been tested by S.A.E. to be 478 +/- degrees Fahrenheit.
I MUST GET PDF IS COMING SOON 23/03/2020 today or tomorrow
Here is the Gasoline Vaporization process in sequence :......
1) Carburetor..............................................................................
A) Induct and Meter the incoming Ambient Air,
B) Meter and Atomize Liquid gasoline into tiny liquid fragments,
C) Emulsify the tiny gasoline fragments with Ambient Air at a high velocity,
2) Heat Exchanger.......................................................................
A) Heat the Emulsified Air and Atomized liquid gasoline fragments together to initiate a "Phase Change" from a liquid form into a completely gaseous state, .................................
B) Further emulsify the now heated gaseous Gasoline vapor with the now heated Ambient Air in the 30 Heat Exchanger Tubes, to create a completely Homogenous Air / Fuel Mixture flowing at a high velocity,
3) Turbocharger.........................................................................
A) Compress the Heated and Expanded Hot Homogenous Gasoline Vapor mixture to increase the Vapor Density,
4) Heated Intake Manifold.........................................................
A) Keep the Vapor mixture HOT so no Condensation will occur prior to induction into the Engines Combustion Chamber.
5) Combustion Chamber............................................................
8) Final Heating, the Homogenous Hot Air and Gasoline Vapor mixture then comes into contact with the even HOTER Combustion Chamber components, which have been tested by S.A.E. to be 478 +/- degrees Fahrenheit.