Method of monitoring gas turbine engine operation

Details Method of monitoring gas turbine engine operation Method of monitoring gas turbine engine operation

G - Physics

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G01M 15/00 (2006.01) F01D 19/02 (2006.01) F02C 9/00 (2006.01) F02C 9/28 (2006.01) F02D 28/00 (2006.01) G07C 5/08 (2006.01)

Patent

CA 2565147

A system, method and apparatus for monitoring the performance of a gas turbine engine. A counter value indicative of the comparison between the engine condition and the threshold condition is adjusted. The aircraft operator is warned of an impending maintenance condition based on the counter value and determines an appropriate course of action.

Cette invention se rapporte à un système, à un procédé et à un appareil qui permettent de suivre les performances d'une turbine à gaz. A cet effet, on règle une valeur compteur indiquant la comparaison entre la condition de la turbine à gaz et la condition seuil. L'opérateur de l'avion est averti d'une condition de maintenance imminente sur la base de cette valeur de compteur et il détermine une suite d'actions appropriée.

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