Updating the failure probability of miter

Slides:



Advertisements
Similar presentations
Brief introduction on Logistic Regression
Advertisements

Managerial Economics Estimation of Demand
Modelling unknown errors as random variables Thomas Svensson, SP Technical Research Institute of Sweden, a statistician working with Chalmers and FCC in.
Crack Management – Part II Feedback From In-Service Inspections Based upon OTC “FPSO Fatigue Assessment: Feedback From In-Service Inspections” Clemens.
Phase II Total Fatigue Life (Crack Initiation + Crack Propagation) SAE FD&E Current Effort 30 October 2012 at Peoria, IL.
Sections 7-1 and 7-2 Review and Preview and Estimating a Population Proportion.
Structural Reliability Theory
Propagation of Error Ch En 475 Unit Operations. Quantifying variables (i.e. answering a question with a number) 1. Directly measure the variable. - referred.
Chapter 5 Fatigue.
Fatigue Failure Through Bending David Burnette ME 498.
Development of Empirical Models From Process Data
Statistics and Probability Theory Prof. Dr. Michael Havbro Faber
A new assessment method for masonry arch bridges (SMART) Clive Melbourne, Adrienn Tomor School of Computing, Science and Engineering, University of.
Distribution of Defects in Wind Turbine Blades & Reliability Assessment of Blades Containing Defects Authors: Henrik Stensgaard Toft, Aalborg University.
RBI Intro & some activities at DNV
Chapter 6 Random Error The Nature of Random Errors
Critical Plane Approach in Stage I and Stage II of Fatigue Under Multiaxial Loading A. KAROLCZUK E. MACHA Opole University of Technology, Department of.
Engineering Doctorate – Nuclear Materials Development of Advanced Defect Assessment Methods Involving Weld Residual Stresses If using an image in the.
GOLD Guaranteed Operation and Low DMC SEAMLESS AIRCRAFT HEALTH MANAGEMENT FOR A PERMANENT SERVICEABLE FLEET Birmingham (UK) December 05, 2007.
Sections 6-1 and 6-2 Overview Estimating a Population Proportion.
Population All members of a set which have a given characteristic. Population Data Data associated with a certain population. Population Parameter A measure.
Chapter 7 Estimates and Sample Sizes
Application of the Direct Optimized Probabilistic Calculation Martin Krejsa Department of Structural Mechanics Faculty of Civil Engineering VSB - Technical.
High strength materials are being increasingly used in designing critical components to save weight or meet difficult service conditions. Unfortunately.
Chapter 7 Fatigue Failure Resulting from Variable Loading
Application of SRA for Pipeline Design Operation & Maintenance Andrew Francis Advantica Technologies ASRANeT, 2 nd Annual Colloquium, 9 th July 2001.
Pressure Cycling of Type 1 Pressure Vessels with Gaseous Hydrogen
FRACTURE MECHANICS AND FATIGUE DESIGN HANS MF PANJAITAN Marinteknisk Senter Otto Nielsens Veg Trondheim Norway Mobile:
Structural Engineering Lab 3.1 kind of fatigue design. (1) Safe life design (2)Fail safe design (3) Damage tolerance design (4) Fracture controlled design.
Preparing for the Hydrogen Economy by Using the Existing Natural Gas System as a Catalyst // Project Contract No.: SES6/CT/2004/ NATURALHY is an.
Sections 7-1 and 7-2 Review and Preview and Estimating a Population Proportion.
Propagation of Error Ch En 475 Unit Operations. Quantifying variables (i.e. answering a question with a number) 1. Directly measure the variable. - referred.
New Mexico Department of Transportation Research Bureau Expanding the Use of Weigh-In-Motion Data.
Reliability-Based Design Methods of Structures
Chapter 7 Fatigue Failure Resulting from Variable Loading
IX. Transient Model Nonlinear Regression and Statistical Analysis.
Teaching Modules for Steel Instruction
1 EXAKT SKF Phase 1, Session 2 Principles. 2 The CBM Decision supported by EXAKT Given the condition today, the asset mgr. takes one of three decisions:
Copyright © Cengage Learning. All rights reserved. 12 Analysis of Variance.
I. M. DMYTRAKH and V. V. PANASYUK Karpenko Physico-Mechanical Institute, National Academy of Sciences of Ukraine 5 Naukova Street, Lviv, 79601, UKRAINE.
Conference on Quality in Space & Defense Industries CQSDI ‘08 Probabilistic Technology Panel: What Is Probabilistic Technology? Mohammad Khalessi, Ph.D.
1 Chi-square Test Dr. T. T. Kachwala. Using the Chi-Square Test 2 The following are the two Applications: 1. Chi square as a test of Independence 2.Chi.
Reducing Uncertainty in Fatigue Life Estimates Design, Analysis, and Simulation 1-77-Nastran A Probabilistic Approach To Modeling Fatigue.
IAEA Training Course on Safety Assessment of NPPs to Assist Decision Making PSA Quantification. Analysis of Results Workshop Information IAEA Workshop.
William Prosser April 15, Introduction to Probability of Detection (POD) for Nondestructive Evaluation (NDE) This briefing is for status only and.
IDENTIFICATION OF FATIGUE FRACTURE PLANE POSITIONS WITH THE EXPECTED PRINCIPAL STRESS DIRECTION Aleksander KAROLCZUK Ewald MACHA Technical University of.
Chalmers University of Technology Advanced NDT Mathematical modelling of the ultrasonic phased array technique within the project Quantification of the.
Quantification of the reliability of flaw detection (NDT) using probability of detection (POD) based on synthetic data - Validation of the ultrasonic.
IS:800 Section 13 FATIGUE. Introduction Mechanism of Fatigue Fracture Factors Affecting Fatigue Strength Design Strength & Cumulative Fatigue Damage IS:800.
Ch 1. Introduction Pattern Recognition and Machine Learning, C. M. Bishop, Updated by J.-H. Eom (2 nd round revision) Summarized by K.-I.
Elasto - plastic behavior of beam-to- column connections with fillets of steel bridge frame piers.
Best in Market Pricing. What is Best in Market Pricing ? An extension of parametric modeling for negotiating lowest pricing for a statement of work consisting.
Define risk in AUDITING
RELIABILITY-BASED CAPACITY ASSESSMENT OF WATER STORAGE SYSTEM
Structural Reliability Aspects in Design of Wind Turbines
JCSS Model Code Fatigue, inspection and reliability
On the Assessment of Robustness: A General Framework
Turbo Power Life Prediction- Overview
Orynyak I.V., Borodii M.V., Batura A.S.
Product reliability Measuring
Applying the damage tolerance methodology on a railway component
Assessing uncertainties on production forecasting based on production Profile reconstruction from a few Dynamic simulations Gaétan Bardy – PhD Student.
SR 1 and 2 Hay Point Fatigue Damage Structural Risk
MATH 2140 Numerical Methods
YuankaiGao,XiaogangLi
MEMS Finite Element Analysis
INTERCONNECTED SYSTEM GENERATING CAPACITY RELIABILITY EVALUATION
Ch 3. Linear Models for Regression (2/2) Pattern Recognition and Machine Learning, C. M. Bishop, Previously summarized by Yung-Kyun Noh Updated.
Lab8: Fatigue Testing Machine
Lab8: Fatigue Testing Machine
Presentation transcript:

Updating the failure probability of miter gates based on observation of water levels Thuong Van DANG, Quang Anh MAI, Pablo G. MORATO, Philippe RIGO dangvanthuong@doct.uliege.be +32 488 613309 PARTNERS ABSTRACT Hydraulic steel structures, especially lock gates play a significant role in keeping navigation traffic uninterrupted. After a few decades of operation, many of the welded joints may suffer various degrees of deterioration, primarily due to fatigue. To economically combining crack inspection with a scheduled maintenance of the movable parts of the gate, it is valuable to predict inspection time of the welded joints using the observed water levels of the operational history. The updating of the failure probability is done for three inspection techniques, considering annual probability and repair decisions. 1. INTRODUCTION Basically, miter gates are inspected at approximately 5-10 years intervals. The results of the inspection provides data to update failure probability. This study introduces another technique that updates failure probability based on critical annual probability, considering probability of detection and repair decisions. 2. EQUIVALENT STRESS RANGE 4. UPDATING FAILURE PROBABILITY The simulation method is used to update the failure probability (Pf), considering POD and repair policies. It is assumed that all detected cracks are repaired. The maximum allowable annual probability of failure Pf =1.4x10-3 (equivalent to a target reliability index after 50 years is 1.5 in EN1990) and 90% POD in three inspection techniques A, B, C are used. The POD curves are represented by the Log-Odds-Log scale model: POD a = 𝛼 𝑎 𝛾 1+𝛼 𝑎 𝛾 (4) where a (mm) is the detectable crack and α, γ are regression parameters of A, B, C. For practical fatigue design with the use of nominal stress S-N curves, welded joints are divided into several classes, each with a corresponding design S-N curve. In this study, stresses are calculated for each observed water level by using analytical formulas. The properties of welded joint can be found in the detail category state ∆𝜎 = 40 N/mm2 with slop m = 3 in Eurocode NEN EN 1993.1.9 C2, Table 8.3. The different stress-ranges occurs during the year are represented by an equivalent stress-range value, as follows Eq. (1). ∆𝜎= 𝑚 𝐷 𝑡𝑜𝑡 𝐶 𝑛𝑇 (1) Where 𝐷 𝑡𝑜𝑡 is total accumulated damage, C is material parameter, n = 7048 is the number of levelling per year and T = 50 years is the time of observations. Fig. 1. Updating procedure Fig. 4. Updating failure probability Pf 3. CALIBRATING FRACTURE MECHANIC MODEL To incorporate the crack inspection results into assessing failure probability, a fracture mechanic (FM) model is used for crack propagation. The most widely used model is the Paris-Erdogan law: 𝑑𝑎 𝑑𝑁 = 𝐶(𝑌∆𝜎 𝜋𝑎 ) 𝑚 (2) where da/dN is the rate of crack growth, C and m are material parameters, Y is geometry function, Δσ is the equivalent stress-range. The calibration algorithm is carried out by a least-squares fitting in cumulative failure probability space (Pc), as shown in Eq. (3). 𝑚𝑖𝑛 𝑡=1 𝑇 ( 𝑃𝑐 𝑆𝑁 𝑡 − 𝑃𝑐 𝐹𝑀 𝑡; 𝑥 1 … 𝑥 𝑁 ) 2 (3) where 𝑃𝑐 𝑆𝑁 𝑡 is the cumulative failure probability at time t, evaluated using the S-N model; 𝑃𝑐 𝐹𝑀 𝑡; 𝑥 1 … 𝑥 𝑁 is the cumulative failure probability at time t, evaluated using FM model with a set of parameters 𝑥 1 … 𝑥 𝑁 representing initial crack size, C, uncertainty of geometry function. T is the service life of the considered structures. Fig. 5. Updating cumulative failure probability Pc CONCLUSIONS Fig. 2. Crack propagation Different stress-ranges occuring during the year are represented by an equivalent stress-range value. The calibration algorithm is carried out by a least-squares fitting in cumulative probability space. This study presented efforts to update probability of failure for a miter gate based on critical annual probability and inspection techniques. 1 2 3 Fig. 3. Calibrated result