Vanes in an air duct, independently controlled, one by the engine operator and others by environmental factors, generate vortices determining the speed of a turbine and thereby the flow of fuel through a fuel meter and fuel valves into prechambers for vaporization and mixing with spiraling air.
In a low-pressure fuel control system increments of fuel and air flow from a vented receptacle sequentially into multiple fuel valves which are either actuated or responding to air pressure differentials and the latter can also be used for spark ignition.
Fuel Control And Injection System For I.c. Engines
Intake air flowing through a controlling device turns a spring constrained rotor and an attached metering valve to control the fuel flow. The aerodynamically computed turn angle depends on air velocity and density and on vortices generated with vanes actuated with device-integral means responding to operational needs. The fuel is delivered to intake ports or to cylinders.