Turbine blade radial position gage

G - Physics – 01 – B

Patent

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G01B 5/25 (2006.01) G01B 5/20 (2006.01) G01B 5/24 (2006.01)

Patent

CA 1283532

53521 -12- ABSTRACT A gage for determining alignment of a turbine rotor blade in an assembly position on a turbine rotor. The gage includes a precision base for positioning on the rotor surface adjacent a blade to establish a tangent line perpendicular to a rotor radial line through the center of a slot in which a blade is disposed. A standard extends from the base and carries a first contact for positioning against a low portion of the blade and a second measuring contact for positioning against an upper portion of the blade. The measuring contact provides an indication of blade misalignment.

547165

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