Appendix No 1

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    Report by: 5 Camber Grove

    Metspect Sarel Cilliers Circle

    Pinetown

    4041

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    BACKGROUND

    We were told that the bolt failed on a building site in Mocambique. At the time of failure it

    had been mounted in a concrete plinth which had been allowed to cure. To align it with the

    mating girder it was necessary to straighten the bolt using a hand-held pipe as a lever. It wasduring this operation that the bolt snapped.

    EXPERIMENTAL

    The failed bolt was examined visually and with a stereo microscope. Sections were then

    removed for:

    a) The fracture face of the failed bolt was examined optically and on a SEM to

    determine the failure mode.

    b) Longitudinal and transverse sections were removed from both the failed and

    the new bolt. These were mounted, polished, etched in 2% nital and

    examined on an optical microscope to determine the microstructure. These

    samples were then used for Vickers hardness testing

    c) Tensile test pieces were machined from both the failed and the new bolt.

    Because of the size of the failed sample it was only not possible to obtain a

    full 50mm gauge length sample

    d) Spectroscopic chemical analysis was done on the sectional remains from the

    tensile test pieces.

    RESULTS

    Visual Examination

    Photo 2 Photo 3

    Initiation

    point

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    Photo 2 shows the failed bolt and the threaded portion of the new one. It can be seen that

    failure occurred on the last, or very near the last, thread. Due to bending moments this

    would have been the highest stress section during the straightening operation.

    Photo 3 shows the fracture face with the initiation point marked. The fracture is flat faced

    with no significant macro deformation, this is indicative of brittle fracture on a macro level.

    Microscopic Examination

    Photo 4 Photo 5

    Photo 4 and 5 show the microstructure of the failed bolt at 200x magnification. Photo 4 is a

    transverse section and photo 5 is a longitudinal direction. The samples have been etched in

    2% nital to reveal a microstructure of tempered martensite with some grain boundary

    bainite.

    There is some banding evident in the longitudinal direction. Banding occurs when there is

    non-uniform chemical composition across the section. This can cause variations in hardness

    between bands.

    Photo 6 Photo 7

    Photos 6 and 7 show the microstructure of the new bolt at x200 magnification. Photo 6 is a

    transverse section and photo 7 is a longitudinal direction. The samples have been etched in

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    2% nital to reveal a microstructure, which again was tempered martensite with some grain

    boundary bainite. Again there is some banding evident in the longitudinal direction.

    Scanning Electron Microscope Examination

    The fracture face of the broken bolt was examined on a scanning electron microscope (SEM)

    to determine the failure mode. Scale bars and magnification are shown on the photos.

    Photo 8 Photo 9

    Photo 8 was taken at 600x and photo 9 is the same location at 1200x magnification. The

    photographs are typical of cleavage failure. Decohesion or cracking can also be seen.

    Cleavage is a mechanism of brittle transgranular fracture, resulting in cleaving of the crystals

    along their crystallographic planes.

    Photo 10 Photo 11

    Dimple

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    Photo 9 shows more clearly the river patterns associated with brittle cleavage failure. More

    than 90% of the fracture face showed a cleavage or quasi-cleavage mode of failure. There

    were also small areas of dimple rupture, synonymous with a more ductile failure mode, as

    shown in photo 11.

    Chemical Analysis and Mechanical Properties

    Elements Failed Bolt New Bolta709M40 (En19)

    bPD970-709M40

    Carbon 0.38 0.40 0.35-0.45 0.36-0.44

    Manganese 0.82 0.87 0.50-0.80 0.70-1.00

    Sulphur

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    Sample

    Diameter

    mm

    Area

    mm2

    Gauge

    Length

    mm

    0.2%

    Proof

    Load

    kN

    Max

    Load

    kN

    Extension

    mm

    0.2%

    Proof

    Stress

    MPa

    Elongation

    %

    RA

    %

    UTS

    MPa

    Failed Bolt 10.21 81.87a36.26 66.44 78.49 7.07 812 19.5 54.1 959

    New Bolt 9.92 77.29 51.14 62.80 78.19 6.85 813 13.4 51.3 1012

    Specification665

    min

    13

    min

    850-

    1000

    Table 2: Tensile test data.

    Note that because of the size of the available sample it was not possible to get a standard

    tensile test piece on the failed bolt. The reduced gauge length could be expected to affect

    the % elongation result, causing it to be slightly high.

    Distance from surface(mm) 0.25 0.5 1.0 2.0 3.0 4.0 5.0

    Failed Bolt 322 304 310 317 317 322 303

    New Bolt 347 331 325 321 322 336 307

    Table 3: Vickers hardness readings (HV)

    Table 3 is a plot of Vickers hardnessreadings, using a 5kg load, against the distance from

    the surface of the bolt. It shows that there is variation in hardness across the section, due to

    banding. In fact when separate readings were taken in the light and dark bands variation

    between 288HV and 331Hv were found on the failed bolt. Similar readings on the new bolt

    varied between 307HV and 345 HV

    DISCUSSION

    Hydrogen Embrittlement

    Hydrogen Embrittlement (HE) is a form of embrittlement caused by the absorption of

    hydrogen ions (H+) into the structure of susceptible steels. The presence of hydrogen in

    concentrations of only a few parts per million (ppm) is sufficient to cause disastrous brittle

    failure.

    The susceptibility of a steel to hydrogen embrittlement is a function of its strength, not itschemical composition. Usually only steels with an Ultimate Tensile Strength (UTS) greater

    than 1000MPa are susceptible.

    The mode of failure with hydrogen embrittlement can be cleavage, quasi-cleavage, micro-

    void coalescence or intergranular, depending on the crack tip stress, temperature, the

    hydrogen concentration and its effects on its plasticity (reference: Professor M.N. James,

    University of Plymouth, England)

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    Hydrogen embrittlement is known to occur during the acid pickling process commonly used

    to clean components prior to hot-dip galvanizing.

    ASTM A143 (Standard Practice for Safeguarding against Embrittlement of Hot-Dip

    Galvanized Structural Steel Products)

    Section 3.2"Hydrogen embrittlement may also occur due to the possibility of atomic hydrogen being

    absorbed by the steel. The susceptibility to hydrogen embrittlement is influenced by the type of steel;

    it's previous heat treatment, and degree of previous cold work. In the case of galvanized steel, the acidpickling reaction prior to galvanizing presents a potential source of hydrogen. In practice hydrogenembrittlement of galvanized steel is usually of concern only if the steel exceeds approximately 150 ksi(1000 MPa) in ultimate tensile strength, approximately 310 HV

    CONCLUSIONS

    Although the bolts were found to be nominally to specification, the failed bolt failed in a

    brittle manner, both macroscopically (minimal distortion) and on a microstructural level

    (cleavage). The bolts were found to have a banded structure resulting in areas having ahardness of up to 347HV, equivalent to a UTS of 1100 MPa. There was evidence of

    decohesion present, (photos 8 & 9), which is common with hydrogen embrittlement.

    From these results our conclusion is that this bolt failed as a result of hydrogen

    embrittlement.

    RECOMMENDATIONS

    1) Those bolts presently mounted in concrete could be tested by affixing a

    mounting plate and tightening the bolts up to the correct torque and leaving

    them for 48hours. Hydrogen embrittlement is often a delayed failure but, in

    our experience, if they are going to fail they will usually do so within 48 hours.

    2) All future bolts might be mechanically cleaned, rather than acid pickled, prior

    to hot-dip galvanizing. Alternatively a hydrogen relieving heat treatment

    process might be instituted after galvanising.

    Signed:

    _____________________ ______________________ __12/06/2014_____

    Alan Blundell Dr. Clinton Bemont (Pr Eng) Date