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FUEL INJECTOR FOR REDUCING COMBUSTION INSTABILITY, FLIGHT VEHICLE HAVING THE SAME AND CONTROL METHOD OF FUEL INJECTION
FUEL INJECTOR FOR REDUCING COMBUSTION INSTABILITY, FLIGHT VEHICLE HAVING THE SAME AND CONTROL METHOD OF FUEL INJECTION
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机译:减少燃烧不稳定性的燃油喷射器,具有相同功能的飞行器及燃油喷射的控制方法
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摘要
This invention is a fuel injection device , and relates to a vehicle provided with a fuel injection control method for this purpose, the fuel a mixture of a fuel injector in the air entering the air- fuel mixture and generates the fuel injection portion is formed so as to inject the air- fuel mixture , the injection path of said air fuel mixture so as to stabilize the combustion flame of the air- fuel mixture are arranged to form a recirculation zone to stabilize the flame of the air- fuel mixture portion , and the fuel injecting apparatus including a secondary fuel injection that is formed so as to inject the secondary fuel into the recirculation region so as to reduce the vibration of the combustion flame provided . Thereby, the present invention is to stabilize the combustion flame jet engines , etc. , thereby reducing the pressure oscillations in the combustion chamber . ; 展开▼