| 摘要 |
<p>According to the invention, the detection method includes the following steps: detecting (E40) an abnormal acceleration of the turbine engine or of a operating line of the compressor that is characteristic of a fault in the turbine engine; storing (E50) a reference temperature (EGTref) measured at the outlet of a turbine of the turbine engine at the moment of the detection; comparing (E60) a difference between a routine temperature (EGT), measured after the detection at the outlet of the turbine, and the reference temperature (EGTref) with a predetermined temperature threshold (SEGT); and identifying (E70) the presence of a rotational separation in the event the threshold is exceeded.</p> |
