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Prognostic and Determistic Analysis of
thinning rate due to Flow Accelerated
Corrosion
Presented By : Akshay Murkute
Instructor : Dr. Yongming Liu
Outline
 Objectives
 Introduction
 Mathematical Model
 Validation and Verification
 Erosion simulation
 Maintenance Scheduling
 Future scope
Objectives
 Develop a mechanistic model and methodology to
predict the thinning rate of pipelines in Nuclear power
plant (CANDU) due to FAC
 Develop State Space model
 Compare the results with the experimental data
 Perform CFD simulations
 Time interval for Maintenance Scheduling
Flow Accelerated Corrosion
 Corrosion mechanism in which a normally protective
oxide layer on a metal surface dissolves in a fast
flowing water.[1]
 Rate of protective oxide layer (magnetite) dissolution
is greater than the rate of protective oxide formation,
when exposed to flowing water or wet steam.
 Causes wall thinning and pipe rupture over time.
[1] https://en.wikipedia.org/wiki/Flow-accelerated_corrosion
Spalling / pitting
Mechanism
Fe = Fe2+ + 2e–
2H2O + 2e– = 2 OH– + H2
Fe2+ + OH– = Fe(OH)+
2Fe(OH)+ + 2 H2O = 2 Fe(OH)2 + H2
Fe(OH)+ + 2 Fe(OH)2+ 3 OH– = Fe3O4 + 4 H2O
[1] “Guidelines for Controlling Flow-Accelerated Corrosion in Fossil and Combined Cycle Plants “ by EPRI
Hydrodynamics
 Flow Velocity (V)
 Reynolds Number (R)
 Mass transfer co-efficient (K)
 Turbulence intensity (TI)
 Surface shear stress (Ʈ)
 Increases turbulence
 Particle hitting pitting of
oxide layer
 Velocity
 Affects the solubility of the surface
Fe3O4
 Higher pH will reduce the amount of
corrosion and FAC
 pH
Mass transfer co-efficient
 Mass Transfer is the process of transporting material
(essentially magnetite) from the surface to the bulk of the
flowing water or water-steam flow
 The local mass transfer coefficient depends in a complex
manner on fluid velocity, fluid viscosity, flow geometry,
pipe/tube surface roughness and temperature
 Mass transfer is usually described by the dimensionless
parameters: Reynolds, Schmidt and Sherwood numbers
Temperature
 Affects:
o pH of the water or wet steam
o Solubility of the oxide
o The variables related to mass
transfer (Reynolds, Schmidt
and Sherwood numbers)
 FAC tends to peak at
temperatures in the range of
150–180°C (300–350°F
Reference: Corrosion 98 – paper 721 flow accelerated corrosion, R. D port Nalco Chemical Company
Geometry
 Locates where FAC will occur.
 Certain geometries affect mass transfer due to changes in local velocity
and turbulence.
 Eg: elbows, tight bends, reducer tees, locations downstream of flow
control orifices and valves
 Geometric enhancement factors are related to the turbulence created by
the particular geometry or fitting.
 Larger values denote a greater propensity for flow disturbance and
which increases the mass transfer coefficients.
 Regression equation for FAC resistance
R = 0.61 + 2.43 Cr + 1.64 Cu + 0.3 Mo , No FAC failure if R > 1
Mathematical Model

FAC = K ∆C
K = Mass transfer coefficient
∆C = Solubility driving force
𝐹𝐴𝐶 = 𝑓 T 𝑓 V 𝑓 pH 𝑓 𝑂 𝑓 ἀ 𝑓 𝐶𝑟 𝑓(𝐺)
K - calculation

D = Diffusivity
𝛾 = Kinematic viscosity
𝑑 = diameter of pipe
ε = Roughness
Mass transfer Sherwood number (Sh) = 𝐾(𝑑/𝐷)
Reynolds number(Re) = 𝑉(𝑑/𝛾)
Schmitt number (Sc) = 𝛾/𝐷.
Component enhancement factor = 16.73*(Re)-0.19
∆C (solubility driving force)
 Depends on temperature, pH and water chemistry
 Defined within specific range
 ∆C = 0.0026*T2 - 1.3973*T + 195.09………(pH=9.5-11)
 ∆C = -5e-06*T3 + 0.006*T2 - 2.3307*T + 314.33……..(pH < 9.5)
Reference: F. H. Sweeton and C. F. Baes Jr., “The solubility of magnetite and hydrolysis of ferrous ion in aqueous solutions at elevated
temperatures,”The Journal of ChemicalThermodynamics, vol. 2, no. 4, pp. 479–500, 1970
0
20
40
60
80
100
120
140
0 50 100 150 200 250 300 350
Solubilityppb
Temperature (C)
Solubility vs temp
CANDU Reactor
 Outlet feeder Input data
Temperature= 310 ˚C
pH = 10.6
Velocity (V)= 8-16.5 m/s
Dissolved O2 ̴ 0 ppb
Diameter (d) = 2.5 in
Reference : A Mechanistic Model for Predicting Flow-assisted and General Corrosion of Carbon Steel in Reactor Primary Coolants D. H. Lister* and
L. C. Lang**
Node Diagram for CANDU circuit
Comparison
Diameter (cm) Bend Angle Coolant Velocity (m/s) Experimental FAC(um/a) Calculated
FAC(um/a)
6.4 42 10.5 50.2 50.43
6.4 73 10.4 59.0 63.5
6.4 73 12.3 75.6 75.9
6.4 73 15.6 105.9 96
6.4 73 16.2 110.0 99.4
6.4 73 17.5 123.1 107
5.0 42 15.8 94.9 90.7
5.0 73 11.9 74.8 89.2
Comparison
0
20
40
60
80
100
120
140
0 2 4 6 8 10 12 14 16 18 20
FACrate(um/a)
Velocity (m/s)
FAC rate vs Velocity
 Experimental
 Calculated
CANDU Reactor
FAC (mm) vs Time (years) Mass transfer vs Temp
Erosion Simulation
CFD Set up
Geometry and Meshing
Inflation at the interface of Wall-fluid
Convergence plot
Mass transfer co-efficient
Erosion Particle tracking
Verification
Validation with Velocity
0
0.02
0.04
0.06
0.08
0.1
0.12
0.14
0 2 4 6 8 10 12 14 16 18
Thinningrate
Velocity
Thinning rate vs Velocity
0.0005
0.00055
0.0006
0.00065
0.0007
0.00075
0.0008
0.00085
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
MTC
Velocity
MTC vs Velocity
Experimental data Calculated data
Reference: “A Mechanistic Model for Predicting Flow-assisted and General Corrosion of Carbon Steel in Reactor Primary Coolants by D. H. Lister and L. C. Lang”
25Reference: “A Mechanistic Model for Predicting Flow-assisted and General Corrosion of Carbon Steel in Reactor Primary Coolants by D. H. Lister and
L. C. Lang”
Maintenance Scheduling
Node Diagram of Nuclear primary circuit
26
Mathematical Model for Flow Accelerated Corrosion
FACrate = (1000*K*∆C +4.85)*10^3
I
II
III
Condition Stages
Stage 1 : >= 6.7
Stage 2 : 6.7< T <=6.4
Stage 3 : 6.4 < T <=6.1
Failure condition
27
5.8
5.9
6
6.1
6.2
6.3
6.4
6.5
6.6
6.7
6.8
6.9
7
0 1 2 3 4 5 6 7 8 9 10 11
Thicknessinmm
Time in years
Thickness vs Time
Maintenance Scheduling Interval
Assumptions:
1. 10% randomness in the variables
2. Initial Condition is 6.7 mm
3. Do nothing maintenance alternative
4. 10% failure probability
5. Both variables of line are randomized
Result:
Time interval of Maintenace
= 8.5 – 3
= 5.5 years
Time interval
Thank you!

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FAC_Akshay Murkute

  • 1. Prognostic and Determistic Analysis of thinning rate due to Flow Accelerated Corrosion Presented By : Akshay Murkute Instructor : Dr. Yongming Liu
  • 2. Outline  Objectives  Introduction  Mathematical Model  Validation and Verification  Erosion simulation  Maintenance Scheduling  Future scope
  • 3. Objectives  Develop a mechanistic model and methodology to predict the thinning rate of pipelines in Nuclear power plant (CANDU) due to FAC  Develop State Space model  Compare the results with the experimental data  Perform CFD simulations  Time interval for Maintenance Scheduling
  • 4. Flow Accelerated Corrosion  Corrosion mechanism in which a normally protective oxide layer on a metal surface dissolves in a fast flowing water.[1]  Rate of protective oxide layer (magnetite) dissolution is greater than the rate of protective oxide formation, when exposed to flowing water or wet steam.  Causes wall thinning and pipe rupture over time. [1] https://en.wikipedia.org/wiki/Flow-accelerated_corrosion
  • 6. Mechanism Fe = Fe2+ + 2e– 2H2O + 2e– = 2 OH– + H2 Fe2+ + OH– = Fe(OH)+ 2Fe(OH)+ + 2 H2O = 2 Fe(OH)2 + H2 Fe(OH)+ + 2 Fe(OH)2+ 3 OH– = Fe3O4 + 4 H2O [1] “Guidelines for Controlling Flow-Accelerated Corrosion in Fossil and Combined Cycle Plants “ by EPRI
  • 7. Hydrodynamics  Flow Velocity (V)  Reynolds Number (R)  Mass transfer co-efficient (K)  Turbulence intensity (TI)  Surface shear stress (Ʈ)
  • 8.  Increases turbulence  Particle hitting pitting of oxide layer  Velocity  Affects the solubility of the surface Fe3O4  Higher pH will reduce the amount of corrosion and FAC  pH
  • 9. Mass transfer co-efficient  Mass Transfer is the process of transporting material (essentially magnetite) from the surface to the bulk of the flowing water or water-steam flow  The local mass transfer coefficient depends in a complex manner on fluid velocity, fluid viscosity, flow geometry, pipe/tube surface roughness and temperature  Mass transfer is usually described by the dimensionless parameters: Reynolds, Schmidt and Sherwood numbers
  • 10. Temperature  Affects: o pH of the water or wet steam o Solubility of the oxide o The variables related to mass transfer (Reynolds, Schmidt and Sherwood numbers)  FAC tends to peak at temperatures in the range of 150–180°C (300–350°F Reference: Corrosion 98 – paper 721 flow accelerated corrosion, R. D port Nalco Chemical Company
  • 11. Geometry  Locates where FAC will occur.  Certain geometries affect mass transfer due to changes in local velocity and turbulence.  Eg: elbows, tight bends, reducer tees, locations downstream of flow control orifices and valves  Geometric enhancement factors are related to the turbulence created by the particular geometry or fitting.  Larger values denote a greater propensity for flow disturbance and which increases the mass transfer coefficients.  Regression equation for FAC resistance R = 0.61 + 2.43 Cr + 1.64 Cu + 0.3 Mo , No FAC failure if R > 1
  • 12. Mathematical Model  FAC = K ∆C K = Mass transfer coefficient ∆C = Solubility driving force 𝐹𝐴𝐶 = 𝑓 T 𝑓 V 𝑓 pH 𝑓 𝑂 𝑓 ἀ 𝑓 𝐶𝑟 𝑓(𝐺)
  • 13. K - calculation  D = Diffusivity 𝛾 = Kinematic viscosity 𝑑 = diameter of pipe ε = Roughness Mass transfer Sherwood number (Sh) = 𝐾(𝑑/𝐷) Reynolds number(Re) = 𝑉(𝑑/𝛾) Schmitt number (Sc) = 𝛾/𝐷. Component enhancement factor = 16.73*(Re)-0.19
  • 14. ∆C (solubility driving force)  Depends on temperature, pH and water chemistry  Defined within specific range  ∆C = 0.0026*T2 - 1.3973*T + 195.09………(pH=9.5-11)  ∆C = -5e-06*T3 + 0.006*T2 - 2.3307*T + 314.33……..(pH < 9.5) Reference: F. H. Sweeton and C. F. Baes Jr., “The solubility of magnetite and hydrolysis of ferrous ion in aqueous solutions at elevated temperatures,”The Journal of ChemicalThermodynamics, vol. 2, no. 4, pp. 479–500, 1970 0 20 40 60 80 100 120 140 0 50 100 150 200 250 300 350 Solubilityppb Temperature (C) Solubility vs temp
  • 15. CANDU Reactor  Outlet feeder Input data Temperature= 310 ˚C pH = 10.6 Velocity (V)= 8-16.5 m/s Dissolved O2 ̴ 0 ppb Diameter (d) = 2.5 in Reference : A Mechanistic Model for Predicting Flow-assisted and General Corrosion of Carbon Steel in Reactor Primary Coolants D. H. Lister* and L. C. Lang** Node Diagram for CANDU circuit
  • 16. Comparison Diameter (cm) Bend Angle Coolant Velocity (m/s) Experimental FAC(um/a) Calculated FAC(um/a) 6.4 42 10.5 50.2 50.43 6.4 73 10.4 59.0 63.5 6.4 73 12.3 75.6 75.9 6.4 73 15.6 105.9 96 6.4 73 16.2 110.0 99.4 6.4 73 17.5 123.1 107 5.0 42 15.8 94.9 90.7 5.0 73 11.9 74.8 89.2
  • 17. Comparison 0 20 40 60 80 100 120 140 0 2 4 6 8 10 12 14 16 18 20 FACrate(um/a) Velocity (m/s) FAC rate vs Velocity  Experimental  Calculated
  • 18. CANDU Reactor FAC (mm) vs Time (years) Mass transfer vs Temp
  • 20. Geometry and Meshing Inflation at the interface of Wall-fluid
  • 24. Validation with Velocity 0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0 2 4 6 8 10 12 14 16 18 Thinningrate Velocity Thinning rate vs Velocity 0.0005 0.00055 0.0006 0.00065 0.0007 0.00075 0.0008 0.00085 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 MTC Velocity MTC vs Velocity Experimental data Calculated data Reference: “A Mechanistic Model for Predicting Flow-assisted and General Corrosion of Carbon Steel in Reactor Primary Coolants by D. H. Lister and L. C. Lang”
  • 25. 25Reference: “A Mechanistic Model for Predicting Flow-assisted and General Corrosion of Carbon Steel in Reactor Primary Coolants by D. H. Lister and L. C. Lang” Maintenance Scheduling Node Diagram of Nuclear primary circuit
  • 26. 26 Mathematical Model for Flow Accelerated Corrosion FACrate = (1000*K*∆C +4.85)*10^3 I II III Condition Stages Stage 1 : >= 6.7 Stage 2 : 6.7< T <=6.4 Stage 3 : 6.4 < T <=6.1 Failure condition
  • 27. 27 5.8 5.9 6 6.1 6.2 6.3 6.4 6.5 6.6 6.7 6.8 6.9 7 0 1 2 3 4 5 6 7 8 9 10 11 Thicknessinmm Time in years Thickness vs Time Maintenance Scheduling Interval Assumptions: 1. 10% randomness in the variables 2. Initial Condition is 6.7 mm 3. Do nothing maintenance alternative 4. 10% failure probability 5. Both variables of line are randomized Result: Time interval of Maintenace = 8.5 – 3 = 5.5 years Time interval