SOUNDNESS MONITORING AND PROFILING OF MODEL BASE OF AERONAUTICAL DIVERTED GAS TURBINE PROTECTING AGAINST FAILURE OF SENSOR

摘要

PROBLEM TO BE SOLVED: To provide a method for monitoring soundness of a turbine coping even with a failure state of a turbine performance measuring device.;SOLUTION: This method includes a step of determining one or a plurality of soundness evaluations including tendency data on one or a plurality of engine modules based on a plurality of engine parameters by monitoring a turbine engine having the plurality of engine modules. This method also includes a step of determining and transmitting a proper report of displaying restoration performed on the turbine engine.;COPYRIGHT: (C)2011,JPO&INPIT