Braze Joint Strain Shift Detection for Turbomachinery Fatigue Monitoring

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Solution Overview

Problem

Turbomachinery instrumentation, such as inlet rakes, face undetected fatigue failure due to vibratory stresses, leading to costly shutdowns and potential damage to downstream components, as existing methods fail to detect stress/strain levels below the fatigue failure threshold.

Innovation Solution

Incorporating a braze joint in high-stress areas of the instrumentation, designed to accommodate stress/strain up to a predetermined threshold, with strain gauges monitoring shifts indicative of joint failure, allowing for early detection and informed decision-making on repair, replacement, or remaining service life.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If sophisticated instrumentation is used to monitor operating conditions in turbomachinery, then measurement precision is improved, but device complexity and cost increase

Engineering Contradiction:
Improvestress/strain detection precisionVSAvoidinstrumentation complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The instrumentation system is segmented into modular components: strain gauges attached to the beam, wiring connected to measurement devices, and data processing systems. This modular approach allows for precise stress/strain monitoring while simplifying installation and maintenance of individual components.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Strain gauges serve as intermediary sensors that convert mechanical stress/strain into electrical signals that can be measured and processed. This intermediary mechanism enables precise detection of structural conditions without requiring direct observation of the beam's internal state.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If instrumentation is monitored continuously for fatigue failure, then reliability is improved, but loss of time for shutdowns and repairs increases

Engineering Contradiction:
Improveinstrumentation reliabilityVSAvoidshutdown time for repair
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The strain gauges and monitoring system are installed and calibrated in advance during routine maintenance periods. Baseline stress/strain levels are established before the turbine enters operation, enabling continuous monitoring without requiring shutdowns for measurement setup.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The monitoring system provides continuous feedback on beam stress/strain levels and fatigue condition. When thresholds are approached or failure is detected, alerts are generated allowing operators to plan maintenance during scheduled outages rather than experiencing unexpected failures.

Inventive Principle:
Principle #23Feedback

3Strength

If the beam is designed to withstand high vibratory stresses, then strength is improved, but weight and cost increase

Engineering Contradiction:
Improvebeam strengthVSAvoidbeam weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The beam's material properties and geometric parameters are optimized to achieve the required strength-to-weight ratio. Finite element analysis is used to identify critical stress zones, allowing reinforcement only where necessary while maintaining lightweight construction in less critical areas.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The beam utilizes composite material construction combining materials with different properties to achieve optimal strength and weight characteristics. This allows the beam to withstand high vibratory stresses while minimizing weight compared to solid metal construction.

Inventive Principle:
Principle #40Composite materials

4Measurement precision

If strain gauges are attached to the beam surface, then measurement precision is improved, but the beam's strength and durability worsen

Engineering Contradiction:
Improvestrain measurement precisionVSAvoidbeam strength
Core Design Contradiction:
Measurement precisionVSStrength

Solution Approach 1:

Strain gauges are strategically positioned in high-stress regions where measurement is most critical for fatigue detection. The gauges are attached only to the surface in these specific locations rather than covering the entire beam, minimizing the impact on overall beam strength while maintaining measurement precision where it matters most.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The strain gauge attachment process uses specialized adhesives and preparation techniques that create a thin, compliant interface between the gauge and beam surface. This interface copies the beam's deformation accurately for measurement while adding minimal mass and having negligible effect on the beam's structural integrity.

Inventive Principle:
Principle #26Copying

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

Enables early warning and safe operation by detecting stress/strain levels below fatigue failure, preventing catastrophic failures and allowing for timely maintenance, effectively extending the service life of turbomachinery components.

Implementation Method 1

measuring strain at the braze joint

Methodology Applied
Scientific EffectStrain gauge measurement: Piezoresistive Effect

Implementation Method 2

the braze joint designed to accommodate stress/strain up to the predetermined threshold level

Methodology Applied
Scientific EffectPlastic deformation: Plasticity

Data Source

PatentUS8671770B2Brazed joint strain shift detection method for monitoring instrument high cycle fatigue life
Publication Date: 2014.03.18 GE INFRASTRUCTURE TECH LLC
  • US8671770B2 patent drawing
  • US8671770B2 patent drawing
  • US8671770B2 patent drawing

AI summary

A method of determining when a component exceeds a predetermined stress level that is less than a fatigue failure level for the component comprising providing a braze joint in a high stress area of a target component, the braze joint designed to accommodate stress/strain up to the predetermined threshold level; measuring strain at the braze joint; observing a shift in strain indicative of a failed brazed joint; utilizing information obtained to repair, replace or set a remaining service life for the target component.