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Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.steel.c9001238
EISBN: 978-1-62708-232-7
... Abstract Heating elements, consisting of strips, 40 mm x 2 mm, of the widely used 80Ni-20Cr resistance heating alloy, and designed to withstand a temperature of 1175 deg C, were rendered unusable by scaling after a few months service in a through-type annealing furnace, Although the temperature...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001104
EISBN: 978-1-62708-214-3
... the furnace at approximately 1 m/min (3 ft/min). The total length of the belt was 94 m (308 ft), with 23 m (75 ft) operating in the heating zone of the furnace. Circumstances Leading to Failure The sinter belt distorted in shape and stretched approximately 1.2 m (4 ft) over a period of 6 months. Normal...
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Published: 01 January 2002
Fig. 8 Heat-resistant alloy clamp for securing the hot air ducting system on fighter aircraft that failed by stress corrosion. (a) Configuration and dimensions (given in inches). (b) Section through the fracture area showing an intergranular crack. Electrolytically etched with oxalic acid. 540 More
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Published: 01 January 2002
Fig. 10 Surface residual-stress map of resistance welded, heat treated, and ground steel saw blade. Source: Ref 30 More
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Published: 01 January 2002
Fig. 27 Section through a heat-resistant alloy forging showing a central discontinuity that resulted from insufficient homogenization during conversion. Step machining was used to reveal the location of the rupture; original diameter is at right. More
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Published: 01 January 2002
Fig. 55 Cast heat-resistant alloy HH, type II, showing the effects of long-term exposure to temperatures between 705 and 925 °C (1300 and 1700 °F) More
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Published: 01 January 2002
Fig. 56 Cast heat-resistant alloy HH, type II, showing cracking through intergranular carbides More
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Published: 01 January 2002
Fig. 57 Sigma (σ) phase in cast heat-resistant alloy HH, type II. Intermetallic phases, such as σ, can greatly reduce the ductility of many high-temperature alloys in service at temperatures from 480 to 955 °C (900 to 1750 °F). More
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Published: 30 August 2021
Fig. 31 Cast heat-resistant alloy HH, type II, showing the effects of long-term exposure to temperatures between 705 and 925 °C (1300 and 1700 °F) More
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Published: 30 August 2021
Fig. 32 Cast heat-resistant alloy HH, type II, showing cracking through intergranular carbides More
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Published: 30 August 2021
Fig. 33 Sigma (σ) phase in cast heat-resistant alloy HH, type II. Intermetallic phases, such as σ, can greatly reduce the ductility of many high-temperature alloys in service at temperatures from 480 to 955 °C (900 to 1750 °F). More
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Published: 30 August 2021
Fig. 15 Section through a heat-resistant alloy forging showing a central discontinuity that resulted from insufficient homogenization during conversion. Step machining was used to reveal the location of the rupture; original diameter is at right. More
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Published: 01 June 2019
Fig. 1 Heat-resistant alloy clamp for securing the hot air ducting system on fighter aircraft that failed by stress corrosion. (a) Configuration and dimensions (given in inches). (b) Section through the fracture area showing an intergranular crack. Electrolytically etched with oxalic acid. 540 More
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Published: 15 January 2021
Fig. 10 Surface residual-stress map of resistance-welded, heat-treated, and ground steel saw blade. Source: Ref 39 More
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Published: 15 January 2021
Fig. 35 Heat-resistant alloy clamp for securing the hot air duct system on a fighter aircraft that failed by stress-corrosion cracking. (a) Configuration and dimensions of the clamp (given in inches). (b) Micrograph of an intergranular crack in a cross section prepared through the fracture More
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001107
EISBN: 978-1-62708-214-3
... based (Cr 23 C 7 and Cr 7 C 3 ). The sooty substance was identified as graphite. Discussion Metal dusting of heat-resistant alloys occurs in carbonaceous atmospheres at temperatures above 425 °C (800 °F), with very high activity in the range of 790 to 845 °C (1450 to 1550 °F)and above 925 °C...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.steel.c9001224
EISBN: 978-1-62708-232-7
... Abstract A recuperator for blast heating of a cupola furnace became unserviceable because of the brittle fracture of several finned tubes made of heat resistant cast steel containing 1.4C, 2.3Si and 28Cr. The service temperature was reported as 850 deg C. This led to the suspicion...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.steel.c9001225
EISBN: 978-1-62708-232-7
... strength of these steels proved inadequate, an alloy lower in chromium would have been preferable. Annealing furnaces Cracking (fracturing) Heat resistant steels Sheet metal Sigma phase Fe-0.06C-1.98Si-25.8Cr-35.8Ni (Other, general, or unspecified) fracture Three radially cracked disks...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.modes.c9001712
EISBN: 978-1-62708-234-1
... analysis indicated there was a strong possibility that the growth of the roll was a result of volumetric expansion due to nitrogen pickup. Therefore, an experiment was designed to quantify the expansion of heat resistant alloys as a function of increase in nitrogen content. Lai 1 , Smith and Bucklin...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.steel.c0046926
EISBN: 978-1-62708-232-7
... Abstract Over a period of about one year, three RA 330 alloy salt pots from a single heat-treating plant were submitted to failure analysis. All of the pots, which had 9.5 mm thick walls, were used primarily to contain neutral salts at temperatures from about 815 to 900 deg C (1500 to 1650 deg...