Recuperators are considered essential hardware to achieve the efficiencies desired for advanced microturbines. Compact recuperator technologies, including primary surface, plate and fin, and spiral, all require thin section materials that have high-temperature strength and corrosion resistance up to 750°C or above, and yet remain as low-cost as possible. The effects of processing and microstructure on creep-rupture resistance at 750°C and 100 MPa were determined for a range of austenitic stainless alloys made into 0.1 mm foils. Two groups of alloys were identified with regard to improved creep-resistance relative to type 347 stainless steel. Alloys with better creep-rupture resistance included alloys 120, 230, modified 803 and thermie-alloy, while alloy 214 and 625 exhibited much better creep strength. Alloys 120 and modified 803 appeared to have the most cost-effective improvements in creep-strength relative to type 347 stainless steel, and should be attractive for advanced microturbine recuperator applications.
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ASME Turbo Expo 2001: Power for Land, Sea, and Air
June 4–7, 2001
New Orleans, Louisiana, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7850-7
PROCEEDINGS PAPER
Selecting and Developing Advanced Alloys for Creep-Resistance for Microturbine Recuperator Applications
Philip J. Maziasz,
Philip J. Maziasz
Oak Ridge National Laboratory, Oak Ridge, TN
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Robert W. Swindeman
Robert W. Swindeman
Oak Ridge National Laboratory, Oak Ridge, TN
Search for other works by this author on:
Philip J. Maziasz
Oak Ridge National Laboratory, Oak Ridge, TN
Robert W. Swindeman
Oak Ridge National Laboratory, Oak Ridge, TN
Paper No:
2001-GT-0541, V001T04A005; 8 pages
Published Online:
July 30, 2014
Citation
Maziasz, PJ, & Swindeman, RW. "Selecting and Developing Advanced Alloys for Creep-Resistance for Microturbine Recuperator Applications." Proceedings of the ASME Turbo Expo 2001: Power for Land, Sea, and Air. Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. New Orleans, Louisiana, USA. June 4–7, 2001. V001T04A005. ASME. https://doi.org/10.1115/2001-GT-0541
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