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Pipeline Research Council International, Inc. Advances in Pipeline Fitness-for-Service A PRCI Webinar SEIKOWAVE

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Page 1: Pipeline Research Council International, Inc. - Seikowaveenergy.seikowave.com/.../Seikowave_Pipeline_FFS_v4.pdf · Pipeline Research Council International, Inc. ... 3DSL Rhino 3D

Pipeline Research Council International,

Inc.

Advances in Pipeline Fitness-for-Service

A PRCI Webinar

SEIKOWAVE

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We will cover

A brief review of corrosion damage assessment methods

Determination of burst pressure – two examples

Integration with NDT tools

3D surface measurements

UT

What’s next?

Pit gage data entry interface

ASME B31G (2012), DNV RP-F101, Kastner

Q&A

2

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A BRIEF HISTORY OF CORROSION

DAMAGE ASSESSMENT METHODS FOR

PIPELINES

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Barlow’s Formula

Barlow's formula calculated the

maximum internal pressure that a pipe

can withstand using the dimensions

and material properties of the pipe

𝑃 =𝜎𝑜2𝑡

𝐷 Where

P = burst pressure

so = allowable stress

t = pipe wall thickness

D = outside diameter of the pipe

t

D

D

direction of flow

t

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Maxey’s Surface Flaw Equation

Developed in the 1960’s to describe the impact of flaws on reducing the maximum pressure of a pipe; modifies the stress based on the surface flaw geometry

𝜎 = 𝜎𝑜

1 −𝐴𝐴𝑜

1 −𝐴

𝐴𝑜𝑀 Where

𝐴 = 𝐿𝑑

𝑑 = 𝑑𝑒𝑝𝑡ℎ 𝑜𝑓 𝑎 𝑟𝑒𝑐𝑡𝑎𝑛𝑔𝑢𝑙𝑎𝑟 𝑑𝑒𝑓𝑒𝑐𝑡

𝐴𝑜 = 𝐿𝑡

𝑀 = 1 +0.8𝐿2

𝐷𝑡

t

D

D

direction of flow

t

d

L

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Corrosion Assessment Failure Prediction

Based on concepts pioneered by Maxey and Kiefner

Modifications to Barlow’s formula to account for surface flaws

First ASME B31G standard in 1991

Subsequent revisions in 2009, and 2012

RSTRENG

Based on a more detailed assessment of the shape of the corrosion damage

Incorporates more accurate Folias factors

Original development by John F. Kiefner while at Battelle Memorial Institute

Ongoing development and advancement supported by PRCI

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Original B31G

𝑃𝑏𝑢𝑟𝑠𝑡 =𝜎𝑓𝑙𝑜𝑤2𝑡

𝐷

1 −2𝑑3𝑡

1 −2𝑑3𝑡𝑀

Where

𝐴 =2

3𝑑𝐿

𝜎𝑓𝑙𝑜𝑤 = 1.1𝑆𝑀𝑌𝑆

𝑀 = 1 +0.8𝐿2

𝐷𝑡L = defect lengthd = maximum defect depthD = pipe diametert = pipe wall thicknessSMYS = Specified Minimum Yield Strength

For defects defined as 𝐿 ≤ 20𝐷𝑡

t

D

D

direction of flow

t

d

L

Parabolic defect model for defects

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Original B31G

𝑃𝑏𝑢𝑟𝑠𝑡 =𝜎𝑓𝑙𝑜𝑤2𝑡

𝐷1 −

𝑑

𝑡Where

𝐴 = 𝐿𝑑

𝜎𝑓𝑙𝑜𝑤 = 1.1𝑆𝑀𝑌𝑆

L = defect length

d = maximum defect depth

D = pipe diameter

t = pipe wall thickness

SMYS = Specified Minimum Yield Strength

For defects defined as 𝐿 > 20𝐷𝑡

t

D

D

direction of flow

t

d

L

Rectangular defect model for long defects

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0.85dL Method

𝑃𝑏𝑢𝑟𝑠𝑡 =𝜎𝑓𝑙𝑜𝑤2𝑡

𝐷

1 − 0.85𝑑𝑡

1 − 0.85𝑑𝑡𝑀

Where

𝐴 = 0.85𝑑𝐿

𝜎𝑓𝑙𝑜𝑤 = 𝑆𝑀𝑌𝑆 + 10,000𝑝𝑠𝑖

𝑀 = 1 + 0.6275𝐿2

𝐷𝑡− 0.003375

𝐿2

𝐷𝑡

2

L = defect lengthd = maximum defect depthD = pipe diametert = pipe wall thicknessSMYS = Specified Minimum Yield Strength

For defects defined as 𝐿 ≤ 50𝐷𝑡

t

D

D

direction of flow

t

d

L

Bulging stress magnification factor

(Folias factor) depends on defect length

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0.85dL Method

𝑃𝑏𝑢𝑟𝑠𝑡 =𝜎𝑓𝑙𝑜𝑤2𝑡

𝐷

1 − 0.85𝑑𝑡

1 − 0.85𝑑𝑡𝑀

Where

𝐴 = 0.85𝑑𝐿

𝜎𝑓𝑙𝑜𝑤 = 𝑆𝑀𝑌𝑆 + 10,000𝑝𝑠𝑖

𝑀 = 0.032𝐿2

𝐷𝑡+ 3.3

L = defect lengthd = maximum defect depthD = pipe diametert = pipe wall thicknessSMYS = Specified Minimum Yield StrengthFor defects defined as 𝐿 > 50𝐷𝑡

t

D

D

direction of flow

t

d

L

Bulging stress magnification factor

(Folias factor) depends on defect length

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Comparison

Criterion Original B31G 0.85dL Method Effective Area

Flow stress 1.1SMYS SMYS + 10,000psi SMYS + 10,000psi

Defect area𝑑𝐿 𝑜𝑟

2

3𝑑𝐿

0.85𝑑𝐿 Effective Area

Transition length 20𝐷𝑡 50𝐷𝑡 50𝐷𝑡

Folias factors 1 2 2

Defect model 2 1 Corrosion Profile

Pressure model 2 1 1

• Improved performance achieved by adjusting the bulging stress magnification factor (Folias factor) for the length of the defect

and maintaining a single failure stress (pressure) model

• Effective area is the best method for estimating the remaining strength of the pipe (hence the term rstreng)

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0

2

4

6

8

10

12

0 10 20 30 40 50 60 70 80 90 100 110 120

ASME B31G Folias Factor Comparison

𝑀0.85𝑑𝐿 = 1 + 0.6275𝐿2

𝐷𝑡− 0.003375

𝐿2

𝐷𝑡

2

𝑀0.85𝑑𝐿 = 0.032𝐿2

𝐷𝑡+ 3.3

𝐿2

𝐷𝑡

𝑀𝐵31𝐺 = 1 +0.8𝐿2

𝐷𝑡

𝐿2

𝐷𝑡≤ 50

𝐿2

𝐷𝑡> 50

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Maxey’s Surface Flaw Equation

A second look

𝜎 = 𝜎𝑜

1 −𝐴𝐴𝑜

1 −𝐴

𝐴𝑜𝑀

𝐴 = 𝐴𝑟𝑒𝑎 𝑜𝑓 𝑑𝑎𝑚𝑎𝑔𝑒

𝑑 = 𝑑𝑒𝑝𝑡ℎ 𝑜𝑓 𝑎 𝑑𝑒𝑓𝑒𝑐𝑡

𝐴𝑜 = 𝐿𝑡

𝑀 = Bulging stress magnification factor (Folias factor)

t

D

D

direction of flow

t

d

L

What’s the best

method to

estimate the area

of damage, A?

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Effective Area

Better calculation of the area of damage

Does not depend on a specific defect model

Parabolic, rectangular, or otherwise

Requires detailed data regarding the shape of the infrastructure damage

One step closer to a FEA (finite element analysis) for damage assessment

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DETERMINATION OF BURST PRESSURE

– TWO EXAMPLES

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• Broad area

corrosion

• Data collected

using a 3D surface

measurement tool

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• Corrosion damage

analyzed to

determine depth

and extent of metal

loss

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ASME B31G-2012 Revision

Fitness for Service Determination

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Defect length = 12.389”

𝐿 ≤ 20𝐷𝑡 = 17.321“

Area model for ASME B31G (1991)

𝐴𝐵31𝐺 =2

3𝐿𝑑 = 1.148 𝑖𝑛2

Area model of 0.85dL

𝐴0.85𝑑𝐿 = 0.85𝑑𝐿 = 1.464 𝑖𝑛2

Area model Effective Area

𝐴𝐸𝐴 = 0.860 𝑖𝑛2

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Effective Area

Area Estimate Comparison

Defines Original ASME B31G

boundary for area estimation

Defines 0.85dL boundary

for area estimation

Area model for ASME B31G (1991)

𝐴𝐵31𝐺 =2

3𝐿𝑑 = 1.148 𝑖𝑛2

Area model of 0.85dL

𝐴0.85𝑑𝐿 = 0.85𝑑𝐿 = 1.464 𝑖𝑛2

Area model Effective Area

𝐴𝐸𝐴 = 0.860 𝑖𝑛2

Corrosion (River bottom) Profile

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• Isolated pits that

likely interact to

form a single

defect

• Data collected

using a 3D surface

measurement tool

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• Isolated pits that

likely interact to

form a single

defect

• Data collected

using a 3D surface

measurement tool

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Defect length = 141mm

𝐿 ≤ 20𝐷𝑡 = 225𝑚𝑚

Area model for ASME B31G (1991)

𝐴𝐵31𝐺 =2

3𝐿𝑑 = 408 𝑚𝑚2

Area model of 0.85dL

𝐴0.85𝑑𝐿 = 0.85𝑑𝐿 = 520 𝑚𝑚2

Area model Effective Area

𝐴𝐸𝐴 = 263 𝑚𝑚2

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Defines Original ASME

B31G boundary for area

estimation

Defines 0.85dL boundary

for area estimation

Corrosion (River bottom) Profile

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INTEGRATION WITH NDT TOOLS

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Integration with NDT tools

Seikowave Tools

3DSL Rhino

3D Toolbox

Ultrasound

Olympus

Other 3D surface measurement tools

Handyscan 700

Coordinate Measurement Machines (e.g. Mitutoyo)

27

Need 3D data in

ply or stl format

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WHAT’S NEXT?

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• Complexity

• Difficult to acquire the

data

• Difficult to perform the

calculation

• Conservatism

• More conservative

generally means more

cost to maintain

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ASME B31G-2012 includes

• Expanded definition of flow stress

• Applicability to metal loss in field bends,

induction bends and elbows

ASMEB31G-2012 does not include

• Preferential corrosion affecting pipe

seams or girth welds

• Metal loss in fittings other than bends

and elbows

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ASME B31G (2012) Flow Stress

Material SMYS Temperature Flow Stress

Carbon Steel T < 250F (120C) sflow = 1.1 X SMYS

sflow < SMTS

Carbon Steel

and low-alloy

Steel

T < 250F (120C) sflow = SMYS + 10kpsi (69MPa)

sflow < SMTS

Carbon Steel

and low-alloy

Steel

sflow = (sYT + sUT)/2

sYT and sUT are specified at the

operating temperature (YT is

the yield strength and UT is the

ultimate strength in tension)

ASME B31G-2012 Revision

𝑆𝑀𝑌𝑆 ≤ 70𝑘𝑝𝑠𝑖 (483MPa)

𝑆𝑀𝑌𝑆 ≤ 80𝑘𝑝𝑠𝑖 (551MPa)

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Flow Stress Examples

SMYS SMTS 1.1 SMYS

SMYS + 10kpsi

(69MPa) (SMYS+SMTS)/2

ksi Mpa ksi Mpa ksi Mpa ksi Mpa ksi Mpa

X65 65 448 77 531 71.5 493 75 517 71 490

X80 80 551 90 621 88 607 90 621 85 587

X100 100 690 110 759 110 759 110 759 105 725

𝑃𝑏𝑢𝑟𝑠𝑡 =𝜎𝑓𝑙𝑜𝑤2𝑡

𝐷

1 −2𝑑3𝑡

1 −2𝑑3𝑡𝑀

• For X65, Pburst is higher when using SMYS + 10kpsi

• For X80, SMYS + 10kpsi equals SMTS

• For X100, 1.1SMYS and SMYS + 10kpsi = SMTS

• Average of SMYS and SMTS is more conservative but

• ASME B31G-2012 does not cover pipe with SMYS > 80kpsi

Subject of ongoing PRCI studies

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Remaining Strength Assessment

What’s Available Now

Original ASME B31G

Modified 0.85dL

Effective Area

API 579

Level 1 and Level 2

What’s Next (Q2 2016)

Pit Gage Data Entry

Robotic Collection

Additional Capabilities

Expanded definition of flow stress

DNV RP-F101

• Per DNV RP-F101, applicable for corrosion in girth welds and seam welds

• Applicable for temperatures above 250F (120C)

Kastner (Circumferential corrosion analysis)

• Better solution for examining extensive circumferential corrosion

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Pit Gage Data Entry

Data from NDT tools is not always available

Sometimes a pit gage is all you have

Data entry in a grid format that matches the grid drawn on the pipeline

Integrates with existing database

Integrates with existing flaw detection and interaction rule software

Integrates with Pipeline FFS for fitness for service calculations

0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

0.000 0.000 0.000 0.034 0.037 0.035 0.000 0.000 0.000

0.000 0.000 0.036 0.050 0.058 0.056 0.038 0.000 0.000

0.034 0.034 0.039 0.052 0.060 0.059 0.048 0.000 0.000

0.037 0.037 0.040 0.052 0.054 0.221 0.049 0.042 0.041

0.036 0.037 0.037 0.035 0.041 0.043 0.041 0.044 0.048

0.000 0.033 0.035 0.039 0.040 0.038 0.139 0.111 0.045

0.000 0.000 0.045 0.090 0.122 0.038 0.037 0.041 0.041

0.000 0.000 0.036 0.037 0.036 0.036 0.038 0.041 0.041

0.000 0.000 0.000 0.000 0.037 0.038 0.041 0.041 0.039

0.000 0.000 0.000 0.035 0.039 0.038 0.039 0.039 0.034

0.000 0.000 0.000 0.034 0.034 0.000 0.000 0.000 0.000

0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

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Robotic data collection

Seikowave robotic systems can move omni-directionally over surfaces and can be operated remotely enabling collection of3D inspection data

Other inspection data (e.g. UT, eddy current)

UntetheredAble to operate as far as 300

meters from the base station

36

Seikowave systems

navigating and

measuring inside and

outside of pipes (1)

(1) Photos courtesy of Asahi and ExxonMobil

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FEA – Under Development

𝑃𝑐𝑜𝑚𝑝𝑢𝑡𝑒𝑑

𝑃𝑏𝑢𝑟𝑠𝑡 𝑡𝑒𝑠𝑡< 1 𝑡ℎ𝑒𝑛 𝑐𝑜𝑚𝑝𝑢𝑡𝑎𝑡𝑖𝑜𝑛 𝑖𝑠 𝑐𝑜𝑛𝑠𝑒𝑟𝑣𝑎𝑡𝑖𝑣𝑒

More work still needed but shows promise

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COME TO THE PRCI RESEARCH

EXCHANGE TO LEARN MORE

February 2-4, 2016 at the Omni San Diego Hotel in San Diego, CA