Contactless, blade-tip clearance measurement for turbines

Patent metadata

Field	Value
Publication number	US-10222200-B2
Application number	US-201715593354-A
Country	US
Kind code	B2
Filing date	May 12, 2017
Priority date	May 12, 2017
Publication date	Mar 5, 2019
Grant date	Mar 5, 2019

Abstract

Turbine blade-tip clearance is measured in a fully assembled turbine casing by mounting a probe tip of a non-contact displacement probe in an inspection port of a vane cavity at a known distance relative to the inner circumferential surface of the corresponding ring segment. The displacement probe generates displacement samples that are indicative of probe tip distance from the turbine blade tip. Variations in probe distance data are recorded as the blade circumferentially sweeps the turbine casing. A data processing system correlates the distance data with localized blade-tip clearance gap. In some embodiments, blade rotational position data are collected by a rotational position sensor. In those embodiments, the data processing system correlates the distance and rotational position data with localized blade tip gap at angular positions about the turbine casing circumference.

First claim

What is claimed is:

1. A method for measuring radial clearance gap between one or more blade tips and an opposing, inner circumferential surface of a ring seal within a turbine casing of a turbine engine, comprising:
providing a turbine engine with an engine outer casing and ring seal, which circumscribe an in situ, rotatable rotor having a row of turbine blades, each blade respectively having an airfoil and a blade tip in opposed spaced relationship with an inner circumferential surface of the ring seal, defining a tip gap there between; the ring seal having a necked, cylindrical-profile inspection port that is accessible from outside the engine outer casing, the inspection port defining a central axis that is axially and radially aligned with tangential swept path of the blade tips, and including: an upper cylindrical portion having a first diameter, which is contiguous with an outer diameter of an inspection port shoulder, an inner diameter of the inspection port shoulder contiguous with smaller second diameter, inspection port aperture; the inspection port aperture terminating and coextensive with the inner circumferential surface of the ring seal, and defining female threads on an outer circumference thereof;
providing a tip-gap inspection system, including:
a tip-gap inspection fixture having: an outer tube for insertion of a distal end thereof into the inspection port of the ring seal; a probe carrier coupled to the distal end of the outer tube, defining a probe carrier shoulder and male threads for engagement with the female threads of the inspection port aperture; a non-contact, absolute-displacement sensor probe, coupled to the probe carrier, the probe having a probe tip, for generating a displacement data set, indicative of absolute relative distance between the probe tip and any one of the respective blade tips that is aligned therewith, without rotor rotation or reference to relative, differential displacement data of any other blade tip;
a data acquisition system, coupled to the sensor probe, for converting the displacement data to actual absolute distance between the probe tip and the respective blade tips that are aligned therewith; and
a data analyzer system, coupled to the data acquisition system, for determining absolute radial clearance gap between any one or more of the respective, individual blade tips and the inner circumferential surface of the ring seal by:
determining actual absolute distance between the probe tip and each respective blade tip with the displacement data provided by the data acquisition system; and
thereafter subtracting from the determined absolute distance between the probe tip and the respective blade tip, a known distance between the probe tip and the inner circumferential surface of the ring seal that is contiguous with the probe aperture;
inserting and rigidly coupling the outer tube of the tip-gap inspection fixture into the inspection port, in fixed alignment with the inspection port aperture, by engaging and screwing together the respective threads of the probe carrier and the inspection port aperture, until the respective shoulders thereof are in abutting contact with each other, so that the probe tip of the displacement probe is radially aligned, in fixed, opposed, spaced relationship with the swept path of the blade tips;
rotating the rotor so that the blade tips of one or more respective blades sweeps the inspection port aperture and the probe tip of the non-contact, absolute-displacement sensor probe, while generating the displacement data set, inclusive of data for each individual sweeping blade;
acquiring the displacement data set with the data acquisition system; and
determining, with the displacement data set and the data analyzer, tip-gap between each respective blade tip and the ring seal at the inspection port aperture, by:
obtaining from the data acquisition system, a displacement data sample that is indicative of actual absolute distance between the probe tip and the respective blade tip; and
thereafter, subtracting from the obtained absolute distance between the probe tip and the respective blade tip, a previously known distance between the probe tip and the inner circumferential surface of the ring seal that is contiguous with the probe aperture.

2. The method of claim 1 , further comprising:
aligning a first blade in the blade row of the rotor with the displacement sensor probe and obtaining a first displacement sample with the data acquisition system;
rotating the rotor, so that other blades in the blade row are sequentially aligned with the displacement sensor probe and obtaining a respective displacement sample for each subsequent blade with the data acquisition system;
associating, with the data analyzer, each obtained respective displacement sample with its corresponding blade, by matching order sequence of the respective collected displacement samples with order sequence of blade alignment with the displacement sensor probe; and
determining with the data analyzer, tip-gap of each blade in the rotor's rotation sequence.

3. The method of claim 1 , further comprising the data analyzer system determining absolute radial clearance gap by:
determining actual absolute distance between the probe tip and each respective blade tip with the displacement data provided by the data acquisition system;
thereafter subtracting from the determined absolute distance between the probe tip and the respective blade tip, a known distance between the probe tip and the inner circumferential surface of the ring seal that is contiguous with the probe aperture and thickness of any bond and/or thermal barrier coating layers that are applied over the inner circumferential surface of the ring seal.

4. The method of claim 1 , the provided tip-gap inspection fixture further comprising:
the probe carrier defining a probe carrier tip projecting distal the probe carrier shoulder and incorporating the probe carrier's male threads, for engagement with the corresponding female threads within the inspection port aperture, the probe carrier tip having an internal cavity that defines a carrier tip shoulder and a carrier tip aperture, facilitating communication between the internal cavity and the inspection port aperture;
the probe tip of the displacement sensor probe retained in fixed position within the probe carrier's internal cavity, in abutting engagement with the carrier tip shoulder, and in communication with the inspection port aperture through the carrier tip aperture.

5. The method of claim 4 , the provided tip-gap inspection fixture further comprising:
a biasing element in the probe carrier, for biasing the probe tip in abutting engagement with the carrier tip shoulder.

6. The method of claim 5 , the biasing element comprising:
a lower spring retainer rigidly coupled to the probe and slidably engaged within the probe tip cavity;
an upper spring retainer rigidly coupled to the tip-gap inspection fixture; and
a spring captured between the upper and lower spring retainers.

7. A method for measuring radial clearance gap between one or more blade tips and an opposing, inner circumferential surface of a ring seal within a turbine casing of a turbine engine, comprising:
providing a turbine engine with an engine outer casing and ring seal, which circumscribe an in situ, rotatable rotor having a row of turbine blades, each blade respectively: oriented at a known angular position about the rotor circumference, having an airfoil and a blade tip in opposed spaced relationship with an inner circumferential surface of the ring seal, defining a tip gap there between; the ring seal having a necked, cylindrical-profile inspection port that is accessible from outside the engine outer casing, the inspection port defining a central ax

Assignees

• Siemens Energy Inc

Inventors

• Hatcher Jr Clifford
• Williams James P
• Silieti Mahmood K

Classifications

• F05D2230/72

  Maintenance · CPC title

• F05D2220/31

  in steam turbines · CPC title

• F05D2270/80

  Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges · CPC title

• G01B11/14 Primary

  for measuring distance or clearance between spaced objects or spaced apertures (G01B11/26 takes precedence; rangefinders G01C3/00) · CPC title

• F01D11/08

  for sealing space between rotor blade tips and stator (specially-shaped blade tips therefor F01D5/20) · CPC title