Method and apparatus for inspecting turbine nozzle segments

Measuring and testing – Instrument proving or calibrating – Displacement – motion – distance – or position

Reexamination Certificate

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Details

C073S865800, C033S549000, C415S118000

Reexamination Certificate

active

07578164

ABSTRACT:
A method for inspecting a turbine nozzle segment includes positioning the turbine nozzle segment on a base of a tool, with the outer forward face and the inner forward face of the turbine nozzle segment contacting a surface of the base. The outer wall is positioned between a first pedestal outer stand and a second pedestal outer stand of the tool, and the inner wall is positioned between a first pedestal inner stand and a second pedestal inner stand of the tool. At least one of a position, a depth and a width of a seal slot formed in a side edge of the outer wall and/or the inner wall is measured. At least one axial dimension of the turbine nozzle segment and at least one radial dimension of the turbine nozzle segment are measured.

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EP Search Report, App. No. 06254888.8 (Jan. 9, 2007).

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