Fuel injection control system for a turbine engine
AssigneeAffordable Turbine Power Company, Inc.
InventorsCharles F. Nearhoof, Sr., Charles F. Nearhoof, Jr., Kevin P. Pearce
Life of this patent
Estimating the term…
Loading patent…
AssigneeAffordable Turbine Power Company, Inc.
InventorsCharles F. Nearhoof, Sr., Charles F. Nearhoof, Jr., Kevin P. Pearce
Estimating the term…
This invention is a fuel injection control system for a turbine engine. The invention uses at least one fuel injector, having means for injecting fuel in pulses to the combustion chamber of a turbine engine, and an electronic control unit to receive and interpret input sensor signals from selected operating functions of the engine and to generate and direct fuel injection signals to modify the pulse duration and/or frequency of fuel injection in response to a deviation from a selected operating function, such as the desired operating speed, caused by variable operating loads encountered by the turbine engine. This configuration provides significantly greater fuel efficiency, better operational control and response time, and a lighter weight than is currently available in turbine engines. The invention may be used in many applications such as commercial, private, experimental and military aviation, power plant turbines, and other industrial, military and mining applications.
An apparatus for delivering fuel in pulses directly into the combustion chamber of a turbine engine, said apparatus comprising:
An apparatus for delivering fuel in pulses directly into the combustion chamber of a turbine engine, said apparatus comprising:
A method for delivering fuel in pulses directly into the combustion chamber of a turbine engine and having at least one fuel injector and at least one sensor for sensing operating signals from said engine, said method comprising the steps of:
Dependencies are inferred from the claim text.