Method and system for real-time prognosis analysis and usage based residual life assessment of turbine engine components and display
First Claim
1. A physics based prognostics system for real-time prediction of remaining life prior to crack or flaw nucleation and prediction of residual life of engine components in the presence of a flaw or distortion, the system comprising:
- a graphical user input interface for inputting in-service machine operating data collected from sensors and signal processing modules installed in a machine under investigation, finite element model and quantitative microstructural and internal state variable material parameters of a component of the machine, temperature dependent physical and mechanical properties of the component material including creep, low cycle fatigue, thermal mechanical fatigue, high cycle fatigue, creep crack growth rate, fatigue crack growth rate oxidation, hot corrosion, corrosion fatigue, into a prognostics software database,a prognostics processor that contains materials engineering based damage rules and material microstructure and internal state variables based damage accumulation and fracture models for receiving the data from the database and for processing the data to provide output information indicative of remaining life prior to flaw or crack nucleation and residual life of engine components in the presence of a flaw or distortion, andan output interface for displaying the output information from the processor, indicative of the remaining life prior to flaw or crack nucleation, life consumed and residual life in the presence of a flaw in engine components.
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Abstract
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.
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Citations
20 Claims
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1. A physics based prognostics system for real-time prediction of remaining life prior to crack or flaw nucleation and prediction of residual life of engine components in the presence of a flaw or distortion, the system comprising:
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a graphical user input interface for inputting in-service machine operating data collected from sensors and signal processing modules installed in a machine under investigation, finite element model and quantitative microstructural and internal state variable material parameters of a component of the machine, temperature dependent physical and mechanical properties of the component material including creep, low cycle fatigue, thermal mechanical fatigue, high cycle fatigue, creep crack growth rate, fatigue crack growth rate oxidation, hot corrosion, corrosion fatigue, into a prognostics software database, a prognostics processor that contains materials engineering based damage rules and material microstructure and internal state variables based damage accumulation and fracture models for receiving the data from the database and for processing the data to provide output information indicative of remaining life prior to flaw or crack nucleation and residual life of engine components in the presence of a flaw or distortion, and an output interface for displaying the output information from the processor, indicative of the remaining life prior to flaw or crack nucleation, life consumed and residual life in the presence of a flaw in engine components. - View Dependent Claims (2, 3)
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4. A method for real-time assessment and prediction of remaining life prior to flaw nucleation and residual life in the presence of flaw or distortion of machine components, the method comprising the steps of:
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a) continuously monitoring variability of engine operating parameters and engine operating environment, b) performing the usage and operating environment based flaw or crack nucleation, crack propagation, distortion, corrosion or erosion analysis for life consumption, remaining life prior to crack nucleation and residual life prediction in the presence of flaws of multiple structural components of a turbine engine, c) predicting the development of the intrinsic as well as extrinsic state of damage in these structural components before the development of any discernable flaws, faults or damage in these components that may be manufactured out of metallic, ceramic or a combination of both types of materials using standard data acquired from engine monitoring interfaces. - View Dependent Claims (5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification