Volume 5: Marine; Microturbines and Small Turbomachinery; Oil and Gas Applications; Structures and Dynamics, Parts a and B 2006
DOI: 10.1115/gt2006-90195
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Creep Strength and Microstructure of AL20-25+Nb Alloy Sheets and Foils for Advanced Microturbine Recuperators

Abstract: The Oak Ridge National Laboratory (ORNL) and ATI Allegheny-Ludlum began a collaborative program in 2004 to produce a wide range of commercial sheets and foils of the new AL20-25+Nb stainless alloy, specifically designed for advanced microturbine recuperator applications. There is a need for cost-effective sheets/foils with more performance and reliability at 650–750°C than 347 stainless steel, particularly for larger 200–250 kW microturbines. Phase I of this collaborative program produced the sheets and foils … Show more

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“…foil form is much shorter than that of the tube specimen. Maziasz et al [2005Maziasz et al [ , 2006 also observed such rapid creep rupture in foils of other alloys such as Alloy 625, and HR120. Figure 3.79 clearly suggests that it is critical to evaluate the mechanical properties, especially fatigue, creep and creep-fatigue, of thin sections (of the thickness typically used in PCHEs) of Alloy 617 and other candidate materials and establish the performance envelope.…”
Section: Thin-section Mechanical Properties Of Metallic Alloysmentioning
confidence: 91%
“…foil form is much shorter than that of the tube specimen. Maziasz et al [2005Maziasz et al [ , 2006 also observed such rapid creep rupture in foils of other alloys such as Alloy 625, and HR120. Figure 3.79 clearly suggests that it is critical to evaluate the mechanical properties, especially fatigue, creep and creep-fatigue, of thin sections (of the thickness typically used in PCHEs) of Alloy 617 and other candidate materials and establish the performance envelope.…”
Section: Thin-section Mechanical Properties Of Metallic Alloysmentioning
confidence: 91%
“…Figure 8: LMP plot for 740H plate and tube specimens (aged for 16h at 800 °C in air) [37], 282 specimens (plate material) after aging for 4h at 800 °C in vacuum [30] and 625 sheet specimens (sheet material) in cold-rolled and annealed (1052 °C) condition for the Special Metals data, in as-received condition from ATI Allegheny Ludlum for ORNL data [38] and in solution annealed (1100°C) condition for the ANL data [39].…”
Section: Creep Datamentioning
confidence: 99%
“…Existing creep data for 625 sheet specimens generated at ORNL [38] and at ANL [39] was assimilated and the corresponding LMP plot for the data is shown in Figure 8. Additionally, data from the alloy manufacturer Special Metals was also included resulting in a dataset encompassing temperatures between 593-1000°C and stresses from 30-600 MPa.…”
Section: Creep Datamentioning
confidence: 99%