G - Physics – 01 – D
Patent
G - Physics
01
D
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.
Allen Leslie William
Clifton-Welker Matthew
Palmer Anthony
Fetherstonhaugh & Co.
Weston Aerospace Limited
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