Real-Time Turbine Life Prediction via Physics-Based Prognostics

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Solution Overview

Problem

Current systems fail to accurately predict the life consumption and residual life of turbine engine components in real-time, relying on predetermined safe-life limits and empirical models, which lead to inefficient maintenance and potential unexpected failures, as they do not account for actual usage-based thermal-mechanical loads and microstructural damage mechanisms.

Innovation Solution

A physics-based prognostics system that continuously monitors and analyzes engine operating parameters and thermal-mechanical loads to predict life consumption and residual life, using real-time combustor modeling, thermodynamic analysis, and non-linear finite element analysis to identify variability in damage accumulation and fracture mechanisms, enabling proactive maintenance decisions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If predetermined safe-life limits and empirical models are used for life prediction, then maintenance scheduling is simplified, but prediction accuracy and reliability deteriorate due to inability to account for actual usage-based thermal-mechanical loads and microstructural damage mechanisms

Engineering Contradiction:
Improvelife prediction accuracyVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system segments the life prediction process into distinct computational modules: thermodynamic analysis for temperature profiles, structural analysis for stress distributions, and damage accumulation models for different failure modes. Each module processes specific parameters independently, allowing complex physics-based analysis to be broken down into manageable computational tasks that can be executed in real-time

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system performs preliminary computational work by pre-processing material properties, geometric models, and boundary conditions before actual engine operation. This allows the real-time prediction system to focus only on processing actual operating data through the physics-based models, significantly reducing computational complexity during runtime while maintaining high prediction accuracy

Inventive Principle:
Principle #10Preliminary action

2Reliability

If real-time physics-based prognostics analysis is performed for multiple engine components, then residual life prediction accuracy improves, but computational time and processing requirements increase

Engineering Contradiction:
Improveresidual life prediction reliabilityVSAvoidcomputational time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system implements periodic updating of damage accumulation states at defined intervals during engine operation rather than continuous computation. This allows the physics-based models to be applied at strategic moments when component state changes significantly, maintaining prediction reliability while avoiding unnecessary computational overhead during transient periods when damage accumulation is minimal

Inventive Principle:
Principle #19Periodic action

Solution Approach 2:

The system dynamically adjusts the level of analysis detail and computational intensity based on operating conditions. During normal operation, simplified models are used for quick assessments, while more comprehensive physics-based analysis is activated only when operating conditions indicate potential damage risks or when prediction uncertainty exceeds thresholds, optimizing the balance between reliability and computational time

Inventive Principle:
Principle #15Dynamics

3Loss of information

If traditional monitoring methods are used without further processing, then data collection is simple, but component life computation and damage mechanism identification are not achieved

Engineering Contradiction:
Improvedamage mechanism informationVSAvoidsystem implementation ease
Core Design Contradiction:
Loss of informationVSEase of manufacture

Solution Approach 1:

The system introduces intermediate processing layers between traditional monitoring sensors and final life prediction outputs. These intermediate models include thermodynamic analyses that convert temperature measurements into component thermal states, structural analyses that translate vibration data into stress distributions, and damage models that accumulate effects over time. These intermediaries transform raw monitoring data into meaningful damage mechanism information without requiring complete system redesign

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system replaces traditional mechanical life prediction methods with physics-based computational models. Instead of relying on empirical wear models or simple cycle counting, the system uses thermodynamic equations, structural mechanics models, and material science principles to compute damage accumulation. This substitution enables identification of damage mechanisms while maintaining computational efficiency through modern numerical methods

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

4Productivity

If usage-based life assessment is implemented, then maintenance cost-effectiveness improves, but requirement for real-time operating data and computational resources increases

Engineering Contradiction:
Improvemaintenance efficiencyVSAvoiddata processing requirements
Core Design Contradiction:
ProductivityVSQuantity of substance

Solution Approach 1:

The system extracts only the essential operating parameters needed for life prediction from the full set of available sensor data. Rather than processing all monitoring data, the system identifies and processes specifically thermodynamic parameters for temperature-related damage, mechanical parameters for fatigue, and operational parameters for usage-based wear. This extraction approach maintains maintenance efficiency while significantly reducing data processing requirements

Inventive Principle:
Principle #2Taking out (Extraction)

Data Source

PatentUS8116990B2Method and system for real-time prognosis analysis and usage based residual life assessment of turbine engine components and display
Publication Date: 2012.02.14 KOUL ASHOK
  • US8116990B2 patent drawing
  • US8116990B2 patent drawing
  • US8116990B2 patent drawing

AI summary

A method and system for performing continuous (real-time) physics based prognostics analysis as a function of actual engine usage and changing operating environment. A rule-based mission profile analysis is conducted to determine the mission variability which yields variability in the type of thermal-mechanical loads that an engine is subjected to during use. This is followed by combustor modeling to predict combustion liner temperatures and combustion nozzle plane temperature distributions as a function of engine usage which is followed by off-design engine modeling to determine the pitch-line temperatures in hot gas path components and thermodynamic modeling to compute the component temperature profiles of the components for different stages of the turbine. This is automatically followed by finite element (FE) based non-linear stress-strain analysis using an real-time FE solver and physics based damage accumulation, life consumption and residual life prediction analyses using microstructural modeling based damage and fracture analysis techniques.