发明名称 METHOD OF DETECTING FAILURE OF AEROPLANE ENGINE AND APPARATUS FOR DETECTING FAILURE OF AEROPLANE ENGINE PERFORMING THE SAME
摘要 PURPOSE: A failure detect method of an airplane engine and a detect device using the same are provided to accurately detect the failure of an airplane engine based on the boundary value by varying a failure detect boundary value according to the mission profile of an airplane. CONSTITUTION: A failure detect method of an airplane engine comprises the following steps. The mission profile of the airplane is discriminated. The failure detect boundary value is determined according to the mission profile(110,120). The failure of the airplane engine is determined based on the failure detect boundary value(130). The mission profile comprises one among gliding, take-off, cruise, descending and landing. The failure detect boundary value is based on a predetermined signal generated in the airplane engine.
申请公布号 KR20110130292(A) 申请公布日期 2011.12.05
申请号 KR20100049865 申请日期 2010.05.27
申请人 IUCF-HYU (INDUSTRY-UNIVERSITY COOPERATION FOUNDATION HANYANG UNIVERSITY);DANAM SYSTEMS CORPORATION 发明人 LEE, HYEONG CHEOL;KIM, JI HWAN;CHO, BUM REA;PARK, HOON;YI, HYE WON
分类号 B64D31/00;B64D47/00;F02D41/22;G01M15/00 主分类号 B64D31/00
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