G01B7/142

Turbomachine stage and method for detecting a sealing gap of such a turbomachine stage

A turbomachine stage, in particular a turbine stage or compressor stage of a gas turbine, is disclosed. The turbomachine stage has a, in particular conical, housing in which a rotor blade arrangement having a plurality of rotor blades is disposed which have an outer shroud having at least one radial sealing flange. The sealing flange has a recess arrangement having at least one radial recess in which a radial projection is disposed, in particular centrally. A sensor arrangement having at least one capacitive sensor for detecting a radial distance from a circumferential surface of the sealing flange is disposed on the housing.

SYSTEM AND METHOD FOR USING EDDY CURRENT EDGE EFFECT TO MEASURE A GAP BETWEEN TWO CONDUCTIVE PARTS
20200333294 · 2020-10-22 · ·

There is provided a system for using eddy current edge effect to measure a gap between two conductive parts. The system includes the two conductive parts, each having predetermined properties. The system includes a probe having a housing with a coil, and includes a reference gap standard, based on one or more reference gap measurements taken between at least two reference conductive parts separated by a gap distance, as specified by predetermined engineering requirements. The system includes an inspection instrument assembly coupled to the probe and having an inspection apparatus calibrated to the probe and the reference gap standard. The probe with the coil uses the eddy current edge effect to take the gap measurement and measure the gap. The gap measurement is compared to the reference gap standard, to determine whether the gap measurement is an acceptable result or an unacceptable result, based on the predetermined engineering requirements.

Turbomachine stage and method for determining a seal gap and/or an axial position of such a turbomachine stage

A turbomachine stage, particularly a turbine stage or a compressor stage of a gas turbine, is disclosed. The turbomachine stage has a, conical in particular, housing in which is arranged a moving vane arrangement with multiple moving vanes which have an exterior shroud band with at least one radial sealing flange. The sealing flange has a recess arrangement with at least one radial recess in which, centrally in particular, a radial projection is arranged. There is arranged on the housing a sensor arrangement with at least one capacitive sensor for detecting a radial clearance to a peripheral surface of the sealing flange.