Laser Drill Hole Completion Control for Turbine Airfoils

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Solution Overview

Problem

Current methods for laser drilling of cooling passages in turbine airfoils often result in incomplete holes due to premature cessation of the laser drill upon breakthrough, leading to reduced fluid flow and increased maintenance costs.

Innovation Solution

A method involving the use of a laser drill to create holes in airfoils, where the breakthrough is detected and the drill continues operation based on calculated time durations between breakthroughs, ensuring complete hole formation without damaging the airfoil.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If the laser drill continues operation after breakthrough, then the hole becomes complete with improved fluid flow, but the airfoil may be damaged

Engineering Contradiction:
Improvehole completionVSAvoidairfoil damage
Core Design Contradiction:
Manufacturing precisionVSObject-affected harmful factors

Solution Approach 1:

The system uses sensors to detect breakthrough events and provides feedback to the controller, which then adjusts the laser drill operation accordingly. This closed-loop control enables the system to continue drilling after breakthrough to complete the hole while monitoring for damage conditions, resolving the contradiction between hole completion and airfoil damage prevention.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The laser drill operation is made dynamic by allowing it to continue after breakthrough rather than stopping immediately. The system dynamically adjusts drilling parameters and timing based on real-time conditions, enabling complete hole formation while preventing damage through controlled dynamic operation.

Inventive Principle:
Principle #15Dynamics

2Object-affected harmful factors

If the laser drill stops immediately upon breakthrough, then the airfoil is protected from damage, but the hole remains incomplete reducing fluid flow

Engineering Contradiction:
Improveairfoil damage preventionVSAvoidcooling passage effectiveness
Core Design Contradiction:
Object-affected harmful factorsVSProductivity

Solution Approach 1:

The feedback mechanism allows the system to detect breakthrough and make an informed decision about continued operation. By monitoring breakthrough events and using this information to control drilling duration, the system achieves both airfoil protection and complete hole formation for optimal cooling passage effectiveness.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system changes operational parameters (drilling duration, laser power, pulse frequency) based on breakthrough detection. By adjusting these parameters dynamically, the system prevents airfoil damage while ensuring complete hole formation, thereby maintaining both protection and productivity.

Inventive Principle:
Principle #35Parameter changes

3Measurement precision

If multiple sensors are used to detect breakthrough, then detection accuracy improves, but device complexity increases

Engineering Contradiction:
Improvebreakthrough detection accuracyVSAvoidsensor system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The detection system is segmented into multiple sensors positioned at different locations (inside and outside the airfoil). Each sensor monitors specific aspects of the breakthrough event, and their combined information provides accurate detection without requiring a single complex sensor system.

Inventive Principle:
Principle #1Segmentation

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 allows for the completion of holes in airfoils, enhancing fluid flow and reducing maintenance needs by accurately determining the completion of drilling through precise timing and patterned drilling techniques.

Implementation Method 1

A laser drill may also be used to create the cooling passages through the airfoil

Methodology Applied
Scientific EffectLaser ablation: Laser Ablation

Implementation Method 2

determining that the laser drill has broken through the near wall of the airfoil

Methodology Applied
Scientific EffectBreakthrough detection:

Data Source

PatentUS9468991B2Method determining hole completion
Publication Date: 2016.10.18 SYNOVA SA
  • US9468991B2 patent drawing
  • US9468991B2 patent drawing
  • US9468991B2 patent drawing

AI summary

The present disclosure provides a method for determining a hole completing in laser drilling of a hole in a near wall of an airfoil. The method includes drilling a hole in the near wall of the airfoil using a laser drill. The laser drill may move in a pattern relative to the airfoil. The method also includes determining when the drilling of the hole is complete based on a calculated time duration between successive breakthroughs of a laser from the laser drill through the near wall of the airfoil, or based on a calculated time duration since the latest breakthrough of the laser from the laser drill through the near wall of the airfoil.