Method of measuring blade tip clearance

G - Physics – 01 – B

Patent

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G01B 21/16 (2006.01)

Patent

CA 2709935

A method for measuring blade tip clearance for a gas turbine engine having a fan case assembly and a rotor having a plurality of blades may include the steps of removably attaching a measurement tool to the fan case assembly, the measurement tool having a sensor, rotating the rotor, and measuring blade tip clearance for the plurality of blades during the rotation of the rotor.

L'invention porte sur un procédé de mesure de jeu radial d'aube pour un moteur à turbine à gaz ayant un ensemble carter de ventilateur et un rotor ayant une pluralité d'aubes, lequel procédé peut comprendre les étapes de fixation de façon détachable d'un outil de mesure à l'ensemble carter de ventilateur, l'outil de mesure ayant un capteur, de rotation du rotor et de mesure du jeu radial d'aube pour la pluralité d'aubes pendant la rotation du rotor.

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