Turbine blade-mounted sensor fixture for tip gap measurement
AssigneeSiemens Energy, Inc.
InventorsMahmood K. Silieti, Kevin L. Hines, Abdullatif M. Chehab
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AssigneeSiemens Energy, Inc.
InventorsMahmood K. Silieti, Kevin L. Hines, Abdullatif M. Chehab
Estimating the term…
Turbine blade tip clearance is measured in a fully assembled turbine casing by mounting a non-contact displacement probe or sensor on a turbine blade that generates data indicative of sensor distance from the turbine casing that circumferentially surrounds the blade. The sensor is mounted on the blade with a sensor fixture, which includes a clamping mechanism and a sensor retention mechanism that retains and calibrates the sensor by selective movement of the sensor relative to the retention mechanism. Variations in sensor distance data are recorded when the turbine is operated in turning gear mode. Blade rotational position data are collected by a rotational position sensor. A data processing system correlates the distance and rotational position data with localized blade tip gap at angular positions about the turbine casing circumference. This method and apparatus facilitate assessment of turbine casing deformation impact on blade tip clearance and rotor/casing alignment.
A method for measuring gas turbine blade tip and turbine casing radial clearance gap, comprising:
A system for measuring gas turbine blade tip and turbine casing radial clearance gap in a gas turbine having a rotatable rotor, a turbine blade coupled to the rotor with a radially outwardly projecting tip in opposed spaced relationship with a circumscribing turbine casing, defining a gap there between, the system comprising:
A sensor fixture for coupling a sensor to a turbine blade, comprising:
Dependencies are inferred from the claim text.