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Test IV Test IV Test IV Test IV The TownsendTest The TownsendTest Herb Townsend Herb Townsend The Townsend Test The Townsend Test Townsend Corrosion Consultants Townsend Corrosion Consultants 1 1 Townsend Corrosion Consultants
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Test IV The “Townsend” Test The Townsend Test

Jan 01, 2017

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  • Test IVTest IVTest IV Test IV The Townsend TestThe Townsend Test

    Herb TownsendHerb Townsend

    The Townsend TestThe Townsend TestTownsend Corrosion ConsultantsTownsend Corrosion Consultants

    11 Townsend Corrosion Consultants

  • ScopeScopepp

    Fundamental definitions and concepts Fundamental definitions and concepts

    Review of previous studiesReview of previous studies

    Test IV description and purposep p p

    Current status of testing

    22 Townsend Corrosion Consultants

  • Specific RequirementsSpecific RequirementsFor Hydrogen EmbrittlementFor Hydrogen Embrittlementy gy g

    33 Townsend Corrosion Consultants

  • Sustained, HighSustained, High--Tensile LoadTensile Load, g, g

    Hydrogen embrittlement requires a sustained, high tensile loadhigh tensile load.

    Cracking is a slow process Cracking is a slow process

    Time needed for hydrogen to diffuseTime needed for hydrogen to diffuse to crack site

    Not detected at normal test speeds

    44 Townsend Corrosion Consultants

  • Sources Of HydrogenSources Of Hydrogeny gy g

    Process HydrogenAcid cleaning Acid cleaning

    Galvanizing Phosphatingp g Electroplating

    Corrosion HydrogenCorrosion Hydrogen Cathodic protection Galvanic corrosion of zinc

    55 Townsend Corrosion Consultants

  • Fundamental ConceptsFundamental Conceptspp

    There is a critical threshold load for SCC

    In terms of fracture mechanics, the critical value is Kis KIscc

    KI decreases with increasing hardnessKIscc decreases with increasing hardness

    KIscc decreases with decreasing electrochemical Iscc gpotential

    66 Townsend Corrosion Consultants

  • Key DefinitionsKey Definitionsyy

    Hydrogen embrittlement (HE) loss of cohesion between atoms caused by H in steelbetween atoms caused by H in steel

    Internal hydrogen embrittlement (IHE) HE caused by H entering the steel during processing also calledH entering the steel during processing, also called process hydrogen

    External hydrogen embrittlement (EHE) HE caused External hydrogen embrittlement (EHE) HE caused by H entering from the environment

    In the case of exposure to water EHE is often called In the case of exposure to water, EHE is often called corrosion hydrogen embrittlement, or stress corrosion cracking (SCC)

    77 Townsend Corrosion Consultants

  • Electrochemical ReactionsElectrochemical ReactionsOn Galvanized SteelOn Galvanized Steel

    Galvanized coatingZn Zn+2 + 2eZn Zn+2 + 2e-

    Exposed steel2e- + 2H2O 2OH

    - + H2

    In solutionZn+2 + 2OH- Zn(OH)2 (white rust)

    Overall reactionOverall reactionZn + 2H2O Zn(OH)2 + H2

    99 Townsend Corrosion Consultants

  • Results of Results of Previous StudiesPrevious StudiesPrevious StudiesPrevious Studies

    1973 1973 Large research program conducted by Large research program conducted by BattelleBattelleg p g yg p g yfor the Research Council on Structural Connectionsfor the Research Council on Structural Connections

    1010 Townsend Corrosion Consultants

  • Battelle Bolt Study Battelle Bolt Study 19731973yy

    A325 (HRC 25-34) bolts

    A490 (HRC 33-39) bolts

    Black, ungalvanized

    Galvanized

    Laboratory and outdoor tests

    1111 Townsend Corrosion Consultants

  • Battelle Bolt Study Battelle Bolt Study 1973 Results1973 Results

    Bare and galvanized A325 bolts no failures

    Bare A490 bolts no failures

    Galvanized A490 numerous failures

    Battelle suggested that failures were due to EHE caused by galvanic activity of galvanized y g y gcoatings

    1212 Townsend Corrosion Consultants

  • 1975 1975 Fracture Mechanics TestsFracture Mechanics TestsPrecrackedPrecracked 11--in SQ Bars (ASTM E 1681)in SQ Bars (ASTM E 1681)( )( )

    1313 Townsend Corrosion Consultants

  • 19751975Fracture Mechanics TestsFracture Mechanics Tests

    4140 1-in. bars, HRC 32 to 48

    Notched cantilever-beam specimens

    Fatigue precracked Fatigue precracked

    Bare and zinc-coated

    Rapid-load tests in air for baseline toughness

    Sl l d t t i i f IHE Slow-load tests in air for IHE

    Slow-load tests in 3.5% salt solution for EHE

    1414 Townsend Corrosion Consultants

  • FpcFpc Specimen and Specimen and the the KiesKies EquationEquationqq

    The stress intensity factor, K1, is calculated from Equation 1, the Kies equation as given by Brown [8, 13] and modified to account for side grooves:

    2/32/1

    2/13

    3

    1

    112.4

    WBB

    MK

    (1)

    In equation 1, M is the applied moment, W is the overall specimen height, B is the overall

    WBB n

    the overall specimen height, B is the overall specimen width, Bn is the net specimen width

    at the side grooves, and is defined:

    a1

    Where a is the overall crack length, notch depth included.

    w1

    1515 Townsend Corrosion Consultants

    g , p

  • Dry, SlowDry, Slow--Load Tests Galvanized Load Tests Galvanized Bars In Air For IHEBars In Air For IHE

    1616 Townsend Corrosion Consultants

  • Greater Susceptibility to EHEGreater Susceptibility to EHEp yp y

    1717 Townsend Corrosion Consultants

  • Effect of HardnessEffect of Hardnesson EHE Thresholdon EHE Threshold

    70Kscc vs Hardness

    dKscc/dHRC = -3.8 50

    60

    KSI

    in^0

    .5

    30

    40

    y Fa

    ctor

    , K

    20

    30

    ss In

    tens

    ity

    0

    10

    30 35 40

    Stre

    s

    H d HRC

    1818 Townsend Corrosion Consultants

    Hardness, HRC

  • Effect of Electrochemical Effect of Electrochemical Potential on EHE ThresholdPotential on EHE Threshold

    100

    Kscc vs E (HRC=35)

    80

    90

    100

    SI in

    ^0.5

    Steel

    dK/dE = - 0.134 Ksi-in0.5/mv

    60

    70

    y Fa

    ctor

    , KS

    40

    50

    ss In

    tens

    ity

    Zi

    20

    30

    0.6 0.65 0.7 0.75 0.8 0.85 0.9 0.95 1 1.05 1.1

    Stre

    s Zinc

    1919 Townsend Corrosion Consultants

    Potential, -Vsce

  • Townsend 1975Townsend 1975Summary of ResultsSummary of Resultsyy

    Dry slow-step load Loss of strength due to hydrogen from galvanizing processhydrogen from galvanizing process

    Wet slow-step load Larger loss of strength Wet slow-step load Larger loss of strength due to hydrogen from galvanic corrosion of zinc coatingg

    Led to prohibition of galvanizing for A490 bolts and HRC 32 maximum for galvanized A325

    2020 Townsend Corrosion Consultants

  • Model for Hydrogen Embrittlement Model for Hydrogen Embrittlement of Highof High--Strength Galvanized BoltsStrength Galvanized Boltsgg gg

    1. Galvanized coatings crack at the thread roots of A490 bolts with high pretensionof A490 bolts with high pretension (using turn-of-the-nut or equivalent)

    2. Hydrogen is galvanically deposited on bare steel exposed at these cracks

    3. If the load is greater than the threshold for hydrogen embrittlement, slow crack growth begins

    4. The crack grows until a critical length is

    2121 Townsend Corrosion Consultants

    4. The crack grows until a critical length is reached, and the bolt breaks

  • Test IV ObjectivesTest IV Objectivesjj

    Determine the threshold load levels for Determine the threshold load levels for hydrogen embrittlement of full-size galvanized A354 BD rods exposed to salt waterA354 BD rods exposed to salt water

    Use the results as a guide to identifying safe g y gload levels and if necessary, suggest remedial action for galvanized fasteners on the SAS

    2222 Townsend Corrosion Consultants

  • Application of Application of PrecrackedPrecracked Results Results to Rods is a Significant Challengeto Rods is a Significant Challengeg gg g

    Fracture mechanics equations for threaded sections are approximationssections are approximations

    Uniform hardness for bars vs. hardness profiles for rods

    The 1975 analysis for bolts assumed turn-of-The 1975 analysis for bolts assumed turn ofthe-nut tightening, which generally leads to stresses greater than yield strength

    Rods on the SAS are tensioned by jacking to lower-than-yield stress levels

    2323 Townsend Corrosion Consultants

    lower than yield stress levels

  • BuecknerBueckner Equation Equation for Stress Intensity Factor, K, of a for Stress Intensity Factor, K, of a Circumferentially Notched Round BarCircumferentially Notched Round Baryy

    K= (D1/2) f(d/D)Where:

    d = diameter of notch = tensile stressD = diameter of barD = diameter of barf(d/D) is a constant

    K ( t t) 0 80(%F ) fK = x (constant) ~ 0.80(%Fu) for 3-inch rods

    2424 Townsend Corrosion Consultants

  • Differences Between Differences Between 1975 Lab Tests and Test IV1975 Lab Tests and Test IV

    Cantilever bending vs. tensioning for rods

    No fatigue precrack for Test IV

    K calculations for rods are approximations

    Uniform HRC vs. HRC gradients

    1 in bars vs 2 in to 4 in rods 1-in bars vs. 2-in to 4-in rods

    Low-iron vs. high-iron coatings for rods

    2525 Townsend Corrosion Consultants

    Low iron vs. high iron coatings for rods

  • Test IV Common Design FeaturesTest IV Common Design Featuresgg

    Slow-step, load increases to determine thresholdthreshold

    Exposure to 3 5% NaCl solution Exposure to 3.5% NaCl solution

    Measurement of electrochemical potentialMeasurement of electrochemical potential and pH

    2626 Townsend Corrosion Consultants

  • Test IV Design FeaturesTest IV Design Featuresgg

    Step load increases applied by hydraulic tensioningtensioning

    Displacement measurementDisplacement measurement

    2727 Townsend Corrosion Consultants

  • Test IV Additional Design Test IV Additional Design FeaturesFeatures

    Loads measured by strain gages

    Full-size rods

    Intentional coating holidays

    Continuous monitoring of temperatures

    Acoustic emission monitoring

    2828 Townsend Corrosion Consultants

  • Test IV Load ScheduleTest IV Load ScheduleLoad, % Fu K, KSI-in1/2 Hold time , days

    30 24 230 24 240 32 250 40 255 44 260 48 265 52 270 56 275 60 280 64 2

    2929 Townsend Corrosion Consultants

    85 68 6Fu = minimum specified ultimate strength

  • Test IV Average Load Rate Compared Test IV Average Load Rate Compared to 1975 Testing ksito 1975 Testing ksi--inin1/21/2 per Hourper Hourgg pp

    1975 Test IV

    0.2 ksi-in1/2/hr 0.1 ksi-in1/2/hr

    3030 Townsend Corrosion Consultants

  • Test IV Rig for FullTest IV Rig for Full--length length Bridge Rods Bridge Rods gg

    3131 Townsend Corrosion Consultants

  • Test IV Phase 1 (2010 E2 Rods)Test IV Phase 1 (2010 E2 Rods)( )( )

    2, Full-length 3-in dia shear key bottom anchor rodsanchor rods

    2 Full-length 3-in dia bearing bolts bottom 2, Full-length 3-in dia bearing bolts bottom housing rods

    Tests completed analysis in progress

    3232 Townsend Corrosion Consultants

  • Setting Up Test IV RigSetting Up Test IV Rigg p gg p g

    3333 Townsend Corrosion Consultants

  • Tent Enclosure During TestingTent Enclosure During Testingg gg g

    3434 Townsend Corrosion Consultants

  • After FractureAfter Fracture

    3535 Townsend Corrosion Consultants

  • Fracture SurfaceFracture Surface

    3636 Townsend Corrosion Consultants

  • Test IV Preliminary ResultTest IV Preliminary ResultHighlightsHighlightsg gg g

    4, 3-inch 2010 rods fractured at loads of,0.80 Fu, 0.85 Fu, 0.85 Fu, and >0.85 Fu

    3838 Townsend Corrosion Consultants

  • Test IV SlowTest IV Slow--Step Step Load ApplicationLoad Applicationpppp

    FRACTURE AT 0 80 FAT 0.80 Fu

    3939 Townsend Corrosion Consultants

  • Test IV Preliminary Results Test IV Preliminary Results yy

    Scanning electron microscopy shows evidence of intergranular cracking on the fracture facesof intergranular cracking on the fracture faces for 3 out of 4 rods

    This is consistent with failure by hydrogen embrittlement

    The fracture morphology was similar to that of the failed 2008 rods

    4040 Townsend Corrosion Consultants

  • Test IV Results to DateTest IV Results to DateIntergranularIntergranular Cracking X500Cracking X500gg gg

    4141 Townsend Corrosion Consultants

  • Test IV Test IV Results to DateResults to Date

    2 of 4 rods broke at end without coating holiday

    This suggests that coating defects are not critical in the mechanism of fracturecritical in the mechanism of fracture

    4242 Townsend Corrosion Consultants

  • Galvanized Coating CrackGalvanized Coating CrackRod 4 X500Rod 4 X500

    4343 Townsend Corrosion Consultants

  • Test IV Results to DateTest IV Results to Date

    Electrochemical potentials were 0.15 V to 0.20 V less negative than expected for typicalless negative than expected for typical galvanized

    Galvanized rod coatings were generally higher in iron content

    The high iron content accounts for the reduced galvanic activity of the Test IV rods

    4444 Townsend Corrosion Consultants

  • Test IV Results to DateTest IV Results to Date

    4545 Townsend Corrosion Consultants

  • Test IV Phase 2Test IV Phase 2

    2-in dia. Upper Bearing Rod

    3-in dia. Tower Base Anchor Rod

    4 in dia Tower Saddle Tie Rod 4-in dia. Tower Saddle Tie Rod

    3.5-in dia. Main Cable Anchor Rods with rolled threads

    3.5-in dia. Main Cable Anchor Rods with cut threads

    Tests completed analysis in progress

    4646 Townsend Corrosion Consultants

    Tests completed analysis in progress

  • Test IV Phase 3Test IV Phase 3

    3-in 2008 shear key bottom anchor rods (2 Samples)( p )

    Test set-up in progress

    4747 Townsend Corrosion Consultants

  • Test IV Phase 4 Test IV Phase 4 Planning PhasePlanning Phasegg

    Plan to Test:

    3-in dia. shear key anchor replacement rods (2013 upgrade)

    Black and galvanized

    Effect of Second Heat treatmentEffect of Second Heat treatment

    4848 Townsend Corrosion Consultants

  • Thank youThank youThank youThank you

    4949 Townsend Corrosion Consultants