Method and system for inductive sensing of blades in a...

G - Physics – 01 – D

Patent

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G01D 5/20 (2006.01) F01D 21/00 (2006.01)

Patent

CA 2740108

A method is provided for determining timing points indicative of the passage of a blade in a turbine engine. The method comprises the steps of: providing a first sensing coil proximate to a path of the blade, providing a second sensing coil proximate to the path of the blade, the second sensing coil spaced from the first sensing coil in a direction parallel to the path of the blade, and comparing a signal generated in the first sensing coil with a signal generated in the second sensing coil to derive a timing point indicative of the passage of the blade.

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