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Measurement of Cooling Holes in Gas Turbine Blades using Computed Tomography … · 2016-05-27 ·...

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Measurement of Cooling Holes in Gas Turbine Blades using Computed Tomography Greg Robinson SURVICE Metrology You created this PDF from an application that is not licensed to print to novaPDF printer (http://www.novapdf.com)
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Measurement of Cooling Holes in Gas Turbine Blades using Computed Tomography

Greg RobinsonSURVICE Metrology

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Cooling Hole Measurement

• Background to Project• Selected Approach• Selection of Measurement Techniques

– Surface – Subsurface

• Geometric Analysis– Combining Surface and Subsurface Data– Hole Parameter Extraction

• Cooling Film Effectiveness Assessment– APOLLOTM Computational Fluid Dynamics

• Summary and Comment

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Project Background

GoalAccurately measure small cooling holes in gas turbine blades.

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Project Background

Cooling Holes•Effect of high temperatures•Methods of cooling•Need to maintain effectiveness from blade to blade•Current measurement techniques

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Selected Approach

Surface Measurement

Meshing& CFD

Validation

Subsurface Measurement

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Technique Selection - Surface

SurveyLooked at number of very capable systems:•Laser scanners•Optical profilers

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Technique Selection - Surface

White Light ScannerSelected because:•Accuracy (< 0.001”)•Speed (few seconds)

But:•Problems with shiny objects (like turbine blades)•Cannot see very far into cooling holes

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Technique Selection - Surface

Tests

1.SURVICE Metrology(OptoTOP HE 125 mm FOV)2.ACCUREX Measurement, Inc.(Breuckmann StereoSCAN 60mm FOV)3.Breuckmann 30mm FOV

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Technique Selection - Surface

WLS results 60 mm FOV

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Technique Selection - Subsurface

Computed Topography - Panel Detector

X-ray Source

Inspection Envelope

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Technique Selection - Subsurface

Computed Tomography – Linear Detector

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Technique Selection - Subsurface

Computed Topography – Linear Detector

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Geometric Analysis

Alignment of WLS and CT scans

•PolyWorks Modeler

•Alignment to 0.002”

•CT scan data replaced by WLS data

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Geometric Analysis

Hole parameters extracted manually

•Diameter•Orientation•Location, etc.

Planning to automate this process in future.

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Cooling Film Effectiveness Analysis

APOLLOTM

Computational Fluid Dynamics

Developed for Office of Naval Research

May be adapted to predict airflow over the “as-built” blade

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Summary

• WLS scanning provided high accuracy, low noise surface data.

• CT scanning provides inner dimensions of holes but data can be noisier.

• Data was aligned and the relatively noisy CT scan data discarded.

• Using resulting hole parameters, cooling effectiveness sample holes computed using APOLLOTM.

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Comments

Via Partnership with Chesapeake Testing, SURVICE Metrology will have access to a state-of-the-art Nikon Metrology 225-450kV microfocus Computed Tomography system. Will be operational in the Fall of 2011.

Leveling the pad for thenew scanner.

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