作者: Jerome Henri Noel Lacaille , Aurelie Gouby
DOI:
关键词:
摘要: A method and a system for monitoring an aircraft engine (2), including: acquisition processing part (11) configured to collect time signal of the exhaust gas temperature residual margin smooth thus forming first curve representing margin, identify decreasing pieces in curve, construct second by concatenation pieces, being continuous while restricted prediction model from determine at least one failure forecast indicator.