Gas Turbine Combustor Cooling Hole Inspection

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Solution Overview

Problem

Existing inspection methods for cooling features in gas turbine combustors are time-consuming and costly, particularly when assessing the dimensional accuracy and cooling effectiveness of effusion holes, which can affect the performance and reliability of the engine.

Innovation Solution

A method and apparatus for inspecting cooling features, such as effusion holes in a combustor wall, using a system that directs pressurized ambient air through the holes while heating the wall, allowing for simultaneous measurement of flow rate and cooling effectiveness using pressure and thermal imaging techniques, thereby reducing the need for detailed geometric measurements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If dimensional inspection methods are used to inspect cooling holes, then manufacturing precision can be assessed, but inspection time increases and productivity decreases

Engineering Contradiction:
Improvecooling hole dimensional accuracyVSAvoidinspection speed
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The patent replaces traditional mechanical dimensional inspection methods with a functional inspection method that measures flow rate and cooling effectiveness. Instead of using mechanical measurement tools to assess hole dimensions, the system uses fluid flow measurements and thermal imaging to evaluate whether the cooling holes perform their intended function, thereby eliminating time-consuming geometric measurements while ensuring operational adequacy.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent changes the inspection parameters from geometric dimensions (diameter, length, shape) to functional parameters (flow rate, temperature distribution, cooling effectiveness). By measuring the actual performance of the cooling holes rather than their physical dimensions, the inspection process becomes faster while still providing assurance of manufacturing quality through functional performance validation.

Inventive Principle:
Principle #35Parameter changes

2Manufacturing precision

If detailed geometric measurements are performed on cooling holes, then manufacturing precision is verified, but inspection cost increases

Engineering Contradiction:
Improvecooling hole dimensional accuracyVSAvoidinspection system complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent replaces complex mechanical measurement systems with a simpler functional testing system. Instead of requiring sophisticated coordinate measuring machines or optical scanners to map hole geometries, the invention uses relatively simple flow rate measurement devices and thermal imaging cameras to assess cooling performance, thereby reducing inspection system complexity while maintaining verification of manufacturing quality.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent creates a functional copy of the cooling hole's intended performance rather than physically measuring the holes themselves. By measuring the flow rate and temperature distribution that the cooling holes produce, the system evaluates manufacturing precision through the holes' functional output rather than their physical dimensions, simplifying the inspection apparatus required.

Inventive Principle:
Principle #26Copying

3Measurement precision

If separate inspections for flow rate and cooling effectiveness are conducted, then measurement precision is improved, but inspection time increases

Engineering Contradiction:
Improveflow rate and cooling effectiveness measurement accuracyVSAvoidinspection duration
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The patent merges the inspection of flow rate and cooling effectiveness into a single integrated test procedure. Rather than conducting separate experiments to measure each parameter, the system simultaneously measures both the flow rate of coolant through the holes and the resulting temperature distribution on the surface, using thermal imaging to capture both pieces of information during the same operational test, thereby maintaining measurement precision while halving the inspection time.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The patent ensures continuous measurement of both flow rate and cooling effectiveness during a single uninterrupted test sequence. The thermal imaging system continuously monitors temperature distribution while the flow rate is measured, allowing both parameters to be captured in real-time during the same operational period, eliminating the need to stop and reset between separate measurements.

Inventive Principle:
Principle #20Continuity of useful action

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach enables efficient and cost-effective inspection of cooling features by directly measuring flow rate and cooling effectiveness during the same procedure, potentially reducing inspection time and eliminating the need for costly geometric measurements, ensuring the holes meet operational requirements.

Implementation Method 1

directing a flow of cooling fluid through the one or more cooling holes of the part while the part is being heated

Methodology Applied
Scientific EffectHeat transfer: Conduction (thermal)

Implementation Method 2

heating the wall

Methodology Applied
Scientific EffectHeating: Heating

Data Source

PatentEP2833071B1Methods for inspecting cooling holes
Publication Date: 2019.05.15 PRATT & WHITNEY CANADA CORP
  • EP2833071B1 patent drawingFigure 1
  • EP2833071B1 patent drawingFigure 2
  • EP2833071B1 patent drawingFigure 3

AI summary

Methods and apparatus for inspecting cooling holes (22) in a wall (24) of a combustor (16) of a gas turbine engine (10) are disclosed. A method may comprise heating the wall (24) of the combustor (16), directing a flow of cooling fluid through the cooling holes (22) while the wall (24) is being heated, acquiring a first measurement indicative of a flow rate of the cooling fluid through the cooling holes (22) and acquiring a second measurement indicative of a cooling effectiveness provided by the cooling fluid flowing through the cooling holes (22) at the flow rate.