Effect of Sweet CO2 Environments on Fracture Toughness (FT) and Fatigue Crack Growth Rate (FCGR) by J.R. Gordon and H. Yin Microalloying International Presented at AWS PIPELINES CONFERENCE HOUSTON, TEXAS MARCH 2014 1 Presentation Outline • Overview of Engineering Critical Assessment (ECA) • Flaw Acceptance Criteria for Girth Welds • Offshore pipeline Sweet CO2 and Sour H2S Service conditions • Fracture Mechanics based Testings of X65/X70 in environments • Fracture Toughness in sweet CO2 environments • Fatigue Crack Growth Rate (FCGR) in sweet CO2 environments • On‐going research program 2 Overview of ECA • Most pipeline codes include flaw acceptance criteria to ensure that flaws introduced during fabrication do not impact the performance of the pipeline during installation or operation. • Historically the flaw acceptance criteria in pipeline codes have been based on a combination of good workmanship principles in conjunction with RT (radiography) inspection. • Over the last 20 years there has been an increasing trend to adopt alternative fitness‐for‐service concepts for critical pipeline applications. • The concept of fitness‐for‐service has led to the development of alternative flaw acceptance criteria that are determined by performing an Engineering Critical Assessment (ECA) of the pipeline. • Codes: BS7910; API 579; DnV OS F101 Appendix A; API 1104 Appendix A; CSA Z662 Annex K; etc. 3 Overview of ECA (cont.) • It is now standard practice to perform an Engineering Critical Assessment (ECA) for fracture and fatigue analyses of onshore and offshore pipelines. • The adoption of ECA methods is ideally suited to modern construction methods that use mechanized welding in combination with automated ultrasonic testing (AUT). • Although the adoption of ECA concepts for pipelines may result in relaxed flaw acceptance criteria it will lead to improved integrity since the emphasis is placed on the most important aspects of overall quality: – Material Selection – Procedure Qualification – Improved Inspection Technology 4 Pipeline Construction/Inspection The combination of Mechanized Welding and Automated Ultrasonic Testing (AUT) Inspection is ideally suited for ECA Analysis. (AUT has the ability to size flaw height and Length) 5 Pipeline Construction/Inspection Stress Pipeline Stress Analysis Flaw Acceptance Criteria for AUT Correct for NDE Sizing Inaccuracy Calculate using ECA Procedure Flaw Size Fracture Mechanics Toughness WPQ CTOD Tests 6 Pipeline Construction/Inspection (cont.) • If you know 2 of the 3 parameters you can calculate the limiting value of the 3rd parameter: – Determine limiting flaw size – Determine maximum allowable stress – Develop minimum required toughness • Alternatively if you know all three parameters you can determine overall structural integrity and the margin of safety. • In general, pipeline ECAs determine limiting flaw size based on Applied Stress (calculated) and Material Toughness (measured). 7 BENEFITS of ECA / FFS • Ensure sound pipeline integrity (with reliable NDE inspection) • Reduce construction cost by minimizing unnecessary repairs • Required by code and standards for new constructions • Acceptance by regulatory agencies 8 Example of ECA Result: On‐Shore Pipeline API 1104 Appendix A ECA Flaw Acceptance Criteria 36" OD 8 Tolerable Flaw Plot API 1104 0.625 inch wall 7 Tolerable Flaw Plot 0.625 inch wall Fatigue and Fracture Proposed Flaw Acceptance Criteria Flaw Height (mm) 6 5 4 3 Fracture Limit State (Kmat) 2 Fatigue Limit (FCGR) 1 0 0 50 100 150 200 250 300 350 400 450 Flaw Length (mm) 9 Offshore risers and flowlines • • A number of fields in offshore development are initially sweet (Region 0), souring (pH2S greater than 0.05psia) occurs late in life. Both sweet and sour environments affect material properties (Kmat and FCGR laws) 10 Kmat and FCGR Testing in Sweet CO2 Environments • Pipe Grade : API X70 / X65 • Pipe Size: 12.75” OD x 1.377” WT (35mm) • Test Environments: – Solution = 5% NaCl – CO2 > 14.7 psia – pH = 4 – 6 (buffered with NaHCO3) 11 Fracture Toughness Specimen – B x 2B SENB B = 0.72” (18.3 mm), W = 1.44”, a/W = 0.5 In air testing, Load rate: dK/dt = 16 N.mm^‐1.5 (a test takes minutes) In CO2 environment testing, load rate : dK/dt = 0.05 N.mm^‐1.5 (a test takes days) (Slow rate rising displacement J‐integral or CTOD testing) 12 In‐Air, CO2 and H2S J R‐curve Results 1800 -3/2 1500 In‐Air K-rate:0.05Nmm 5wt% NaCl RT CO2 J (N/mm) 1200 /s CO2 J R‐curve results are intermediate to in‐air and H2S results PP - Air HAZ - Air WCL - Air PP - pH = 6, pH2S = 0.46psia PP - pH = 6, pH2S = 1.1psia 900 PP - pH = 5.5, pH2S = 1.1psia WCL - pH = 6, pH2S = 1.1psia H2S WCL - pH = 6, pH2S = 0.46psia WCL - pH = 5.5, pH2S = 1.1psia HAZ - pH = 6, pH2S = 1.1psia 600 HAZ - pH = 6, pH2S = 0.4psia HAZ - pH = 5.5, pH2S = 1.1psia PP pH = 6, pH2S = 0psia PP pH = 5, pH2S = 0psia 300 PP pH = 6, pH2S = 0psia, 140F 0 0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 a (mm) 13 Fracture toughness in sweet CO2 environments Notch Location Parent Pipe HAZ WCL • Air x x x pH pH2S pCO2 Temp ( C ) 20 20 20 PP Fracture toughness influenced by pH and temperature in pure CO2. Reduction is over 50% of in‐air values Toughness properties at RT are lower than that at 140F. • At RT and 140F minimum toughness properties are at pH = 4. • At pH = 4, the Jmaxload is 200 N/mm and 350N/mm at RT and 140F respectively. /s) 16 16 16 Jm axload (N/mm) J1m m (N/mm) J0.2 (N/mm) 1319 861 622 1006 942 705 500 PP in CO2 5wt% NaCl -3/2 K-rate: 0.05Nmm /s 400 J1mm - RT Jmaxload - RT J0.2mm - RT 300 J1mm - 140F Jmaxload - 140F J0.2mm - 140F 200 100 0 3 4 5 pH 14 215 225 166 600 J (N/mm) • -3/2 K-rate (Nmm Environment 6 Fracture Toughness Comparison: Sweet CO2 vs. Mild H2S, for pH = 5 ‐ 6 In‐Air J_max Load = 622 N/mm WCL 861 N/mm HAZ 1319 N/mm PP J Values (N/mm) 600 J @ max load ‐ All data J @ 1.0mm crack growth J @ 0.2mm crack growth 500 400 300 200 100 0 0 0.2 0.4 0.6 pH2S (psia) 0.8 1 1.2 15 FCGR Specimen – CT, 1/2T B = 0.75” (19 mm), W = 2”, a/W = 0.45 * FCGR Testing: frequency scan da/dN testing, load frequency effect on da/dN * Knockdown Factor (KDF) = FCGRenv / FCGRin‐air 16 FCGR in Sweet CO2 Environments Kmax = 1150Nmm3/2 3/2 K = 1000Nmm Karl, pH = 5, RT, -3/2 1000Nmm R = 0.13 5wt% NaCl OMAE 2008 -3/2 pH = 4.0, RT, 800Nmm KDF BS7910-Mean Increase in FCGR 10 DNV - Internal -3/2 pH = 6.5, RT, 1000Nmm pH = 6.1, No H2S,w/ Inhibitor - 140F, WCL pH = 6.1, No H2S,w/ Inhibitor - 140F, PP OMAE 2008 Corrosion 2005 DNV - Internal 1 17 1E-3 0.01 f (Hz) 0.1 1 • Frequency scan behaviour is similar to sour service behaviour i.e. increasing FCGR with decreasing frequency and reaching a plateau. • Data available in literature has mainly focused on riser frequencies of ~0.1Hz. • Limited data available on FCGR as a function of frequency. KDF vs Test Frequency for X65 and X70 (Literature + DnV Data) 1000 H2S Mean with +/‐ SD Error Bar H2S Mean+2SD H2S Literature Data DnV Data ‐ Thunder Horse CO2 Sweet Env. KDF (BS7910 in‐air mean, R<0.5) 100 10 1 0.1 0.0001 ΔK = 1000 ‐ 1150 N/mm^3/2, pH = 5 ‐ 6, pH2S = 0.12 ‐ 1.46 psia (Region 1); pCO2 = 14.48 ‐ 13.14 psia Temp = RT to 60 C 0.001 0.01 Frequency (Hz) 0.1 1 18 FCGR Comparisons: CO2 vs. H2S & f = 0.001Hz vs. 0.1 Hz 1.00E+00 Flowline, 0.001Hz, CO2 Flowline, 0.001Hz, H2S 1.00E‐01 SCR, 0.1 Hz, CO2 SCR, 0.1 Hz, H2S BS7910 in‐air, Mean, R < 0.5 1.00E‐02 BS7910 in‐air, Mean+2SD, R<0.5 FCGR ‐ da/dN (mm/cycle) BS7910 in‐air, Mean, R>0.5 STAGE B BS7910 in‐air, Mean+2D, R>0.5 1.00E‐03 1.00E‐04 1.00E‐05 STAGE A 1.00E‐06 1.00E‐07 1.00E‐08 10 100 1000 ΔK (N.mm^‐3/2) 19 Summary • Sweet CO2 fracture toughness (FT) tests show CO2 environments degraded fracture toughness significantly. • FCGR in sweet CO2 run faster than in air (i.e., KDF greater than 1.0). – KDF increases with decrease of loading frequency – KDF for sweet CO2 is lower than KDF for sour H2S • Operation ECA analyses of pipelines in Sweet CO2 services should consider the negative effects of CO2 environments on fracture toughness and FCGR laws. • JIP testing is on‐going to research on key variables: 20 Summary cont. • • • • Environmental Variables on FT and FCGR – pH – pCO2 – Temperature – Inhibitors Loading Variables on FCGR – ΔK, R‐ratio – f, fatigue loading frequency – S‐N fatigue Behaviour Sample Geometry – Shallow notch vs. Deep notch Microstructure – Parent Pipe/HAZ/WCL 21
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