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Martensite
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Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.bldgs.c0047694
EISBN: 978-1-62708-219-8
... martensite present in the weld area after the heat treatment. The test failures of the AISI 1080 steel wire butt-welded joints were due to martensite produced in cooling from the welding operation that was not tempered adequately in postweld heat treatment, and to poor wire-end preparation for welding...
Abstract
Extra high strength zinc-coated 1080 steel welded wire was wound into seven-wire cable strands for use in aerial cables and guy wires. The wires and cable strands failed tensile, elongation, and wrap tests, with wires fracturing near welds at 2.5 to 3.5% elongation and through the welded joints in wrap tests. The welded wire was annealed by resistance heating. The wire ends had a chisel shape, produced by the use of sidecutters. Tests of the heat treatment temperatures showed that the wire near the weld area exceeded 775 deg C (1425 deg F). Metallographic examination revealed martensite present in the weld area after the heat treatment. The test failures of the AISI 1080 steel wire butt-welded joints were due to martensite produced in cooling from the welding operation that was not tempered adequately in postweld heat treatment, and to poor wire-end preparation for welding that produced poorly formed weld burrs. The postweld heat treatment was standardized on the 760 deg C (1400 deg F) transformation treatment. The chisel shape of the wire ends was abandoned in favor of flat filed ends. The wrap test was improved by adopting a hand-cranked device. Under these conditions, the welded joints withstood the tensile and wrap tests.
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.process.c0047566
EISBN: 978-1-62708-235-8
... stainless steel filler metal to form a fillet between the handle and the cover. The structure was found to contain a zone of brittle martensite in the portion of the weld adjacent to the low-carbon steel handle; fracture had occurred in this zone. The brittle martensite layer in the weld was the result...
Abstract
Handles welded to the top cover plate of a chemical-plant downcomer broke at the welds when the handles were used to lift the cover. The handles were fabricated of low-carbon steel rod; the cover was of type 502 stainless steel plate. The attachment welds were made with type 347 stainless steel filler metal to form a fillet between the handle and the cover. The structure was found to contain a zone of brittle martensite in the portion of the weld adjacent to the low-carbon steel handle; fracture had occurred in this zone. The brittle martensite layer in the weld was the result of using too large a welding rod and too much heat input, melting of the low-carbon steel handle, which diluted the austenitic stainless steel filler metal and formed martensitic steel in the weld zone. Because it was impractical to preheat and postheat the type 502 stainless steel cover plate, the low-carbon steel handle was welded to low-carbon steel plate, using low-carbon steel electrodes. This plate was then welded to the type 502 stainless steel plate with type 310 stainless steel electrodes. This design produced a large weld section over which the load was distributed.
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in Cracked Eccentric Camshaft
> ASM Failure Analysis Case Histories: Machine Tools and Manufacturing Equipment
Published: 01 June 2019
Fig. 7 Cold deformation and grinding martensite at surface of cam lobe side. Etch: Nital. 200 ×
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in Failure of a Flange from a High Pressure Feeder Plant
> ASM Failure Analysis Case Histories: Improper Maintenance, Repair, and Operating Conditions
Published: 01 June 2019
Fig. 7 Martensite with unaltered ledeburite network. Etched (FeCl 3 + HCl + ethanol). 100 ×
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in Failure of a Flange from a High Pressure Feeder Plant
> ASM Failure Analysis Case Histories: Improper Maintenance, Repair, and Operating Conditions
Published: 01 June 2019
Fig. 8 Microstructure of heat affected zone. Left martensite (black) with ledeburite eutectic, right recrystallised structure. Etched (FeCl 3 + HCl + ethanol). 100 ×
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in Failure of a Flange from a High Pressure Feeder Plant
> ASM Failure Analysis Case Histories: Improper Maintenance, Repair, and Operating Conditions
Published: 01 June 2019
Fig. 14 Microstructure of metal smeared on flange: martensite and residual austenite. Large inclusions of scale are grey. Etched (FeCl 3 + HCl + ethanol). 500 ×
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in Problematic Failure Analysis of a Cast Steel Crankshaft[1]
> ASM Failure Analysis Case Histories: Improper Maintenance, Repair, and Operating Conditions
Published: 01 June 2019
Fig. 14 A band of martensite found at the woody textured fracture edge
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in Microstructural Manifestations of Fractured Z-Profile Steel Wires on the Outer Layer of a Failed Locked Coil Wire Rope
> ASM Failure Analysis Case Histories: Buildings, Bridges, and Infrastructure
Published: 01 June 2019
Fig. 2 Optical micrographs showing white/gray bands of surface martensite and dark underlying region of deformed pearlite in three different broken wire samples. (a) Surface martensite band approximately 65 µm thick. (b) Surface martensite band approximately 25 µm thick. (c) Surface martensite
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Published: 01 June 2019
Fig. 9 Ferrite/martensite microstructure near fracture surface in H.A.Z. 1000 ×
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in Failure Analysis of Cylinder Clamping Rods in Diesel Engines
> ASM Failure Analysis Case Histories: Design Flaws
Published: 01 June 2019
Fig. 8 Microstructure of the new cylinder clamping rod showing tempered martensite structure, 3000×
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in Failure Investigations of PH 13-8 Mo Aircraft Components
> ASM Failure Analysis Case Histories: Air and Spacecraft
Published: 01 June 2019
Fig. 12 Tempered martensite microstructure of the PH 13-8 Mo stainless steel and transgranular internal crack from the shrink link cylinder wall (Vilella's etchant, ×1000).
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in Failures in Airplane Engine Crankshafts
> ASM Failure Analysis Case Histories: Air and Spacecraft
Published: 01 June 2019
Fig. 3 Grinding burn area (hard, brittle white layer of untempered martensite; Rc 54 to 56) and microcracks (arrows) on fillet surface near fatigue origin. Magnification 75 times; 2 pct nital etch.
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in Failures in Airplane Engine Crankshafts
> ASM Failure Analysis Case Histories: Air and Spacecraft
Published: 01 June 2019
Fig. 7 Grinding burn zone consists of untempered martensite. Magnification 100 times; 2 pct nital.
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in Microstructural Features of Prematurely Failed Hot-Strip Mill Work Rolls: Some Studies in Spalling Propensity
> ASM Failure Analysis Case Histories: Steelmaking and Thermal Processing Equipment
Published: 01 June 2019
Fig. 3 Nital-etched microstructure of roll HSM #8 showing acicular martensite with retained austenite at needle interstices and white carbide phase exhibiting microcracking; magnification 500×
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in Microstructural Features of Prematurely Failed Hot-Strip Mill Work Rolls: Some Studies in Spalling Propensity
> ASM Failure Analysis Case Histories: Steelmaking and Thermal Processing Equipment
Published: 01 June 2019
Fig. 4 Nital-etched microstructure of roll HSM #14 showing acicular martensite with retained austenite at needle interstices, white carbide phase, and dark-gray graphite nodule; magnification 500×
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in Microstructural Features of Prematurely Failed Hot-Strip Mill Work Rolls: Some Studies in Spalling Propensity
> ASM Failure Analysis Case Histories: Steelmaking and Thermal Processing Equipment
Published: 01 June 2019
Fig. 5 Nital-etched microstructure of roll HSM #1 showing acicular martensite with retained austenite at needle interstices and white carbide phase exhibiting pronounced microcracking; magnification 500×
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Published: 01 June 2019
Fig. 11 SEM Micrograph showing martensite lath structure (8000×).
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in Rupture of Water Wall Tubes of a Boiler
> ASM Failure Analysis Case Histories: Power Generating Equipment
Published: 01 June 2019
Fig. 2 Martensite structure at edge of rupture. (×100).
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Published: 01 January 2002
Fig. 45 A typical example of freshly formed martensite at the tip of a failed shear blade. The hardness was 59 to 60 HRC. Etched with 3% nital. 50×
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Published: 01 January 2002
Fig. 21 Cross-sectional view of a white layer of martensite produced by fretting of a carbon steel connecting rod. Axial stress, 0 to 380 MPa (0 to 55 ksi); contact stress, 40 MPa (6 ksi); fretting cycles, 10 5 . Sample was nital etched and viewed with scanning electron microscopy (SEM).
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