Start fuel supply control method and system for micro gas turbine
A micro gas turbine and fuel supply control technology, which is applied in the starting of the engine, the starting of the turbine/propulsion device, and the fuel delivery system of the turbine/propulsion, etc., can solve the problems of damaged ignition performance, ignition failure, and reduced fuel supply, etc. Achieve the effect of improving oil-gas ratio, avoiding over-temperature, and enhancing atomization performance
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[0049] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in many different ways defined and covered by the claims.
[0050] The invention is used to expand the geographical application range of the micro gas turbine. Ground micro gas turbines generally work at altitudes below 3,000 meters. If they are directly applied to plateau application scenarios, it will directly lead to a decrease in the performance of micro gas turbines in terms of safety, reliability, maintainability, and service life, and the requirements for ignition energy As the temperature rises, the ignition reliability decreases, and the air density decreases due to high altitude. If the fuel supply law remains unchanged, the fuel-air ratio in the combustion chamber will increase significantly, and the fuel concentration will increase, resulting in deviation from the optimal design ignition range. I...
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