发明名称 FUEL INJECTOR FOR REDUCING COMBUSTION INSTABILITY, FLIGHT VEHICLE HAVING THE SAME AND CONTROL METHOD OF FUEL INJECTION
摘要 PURPOSE: A fuel injection device for reducing instable combustion, an aerial vehicle having the same, and a fuel injection control method are provided to stabilize combustion in a recirculation area and to relieve or prevent the vibration of a combustion flame. CONSTITUTION: A fuel injection device for reducing instable combustion comprises: a fuel injection unit(141) producing an air fuel mixture(151) by mixing fuel with influent air, and injecting the air fuel mixture; a flame stabilization unit(142) arranged on an injection path of the air fuel mixture to form a recirculation area of the air fuel mixture to stabilize a combustion flame of the air fuel mixture; and a secondary fuel injection unit injecting secondary fuel to the recirculation area to reduce the vibration of the combustion flame.
申请公布号 KR20110082701(A) 申请公布日期 2011.07.20
申请号 KR20100002563 申请日期 2010.01.12
申请人 AGENCY FOR DEFENSE DEVELOPMENT 发明人 HWANG, YONG SEOK;CHOI, JONG HO;CHOI, HO JIN;YOON, HYUN GULL;LIM, JIN SHIK
分类号 F02C7/232;F02K1/46;F23R3/20;F23R3/34 主分类号 F02C7/232
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