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Creep-rupture behavior of candidate stirling engine cast iron-base superalloys

Conference · · TMS (The Metallurgical Society) Paper Selection; (USA)
OSTI ID:5250408
 [1]
  1. NASA Lewis Research Center, Cleveland, OH (USA)

The Stirling engine is under investigation jointly by the DOE and NASA as an alternate to the automotive internal combustion engine. Present design criteria require cast cylinder heads and regenerator housings to operate 3500 hours from ambient to 775 C while pressurized to 15 MPa with hydrogen. Creep-rupture tests in air and 15 MPa hydrogen were performed on candidate iron-base alloys XF-818, CRM-6D, and SA-F11 at 760, 815, and 870 C in the as cast condition and with a simulated vacuum braze cycle. The time to 1% strain, minimum creep rate and rupture life as a function of stress was statistically analyzed for each temperature. Multiple linear regression analysis of a temperature-compensated Sherby-Dorn type relationship yielded apparent activation energies and stress exponents. The 15 MPa hydrogen test environment did not significantly reduce the 3500 hour rupture life. The creep-rupture properties are compared to current design criteria for the automotive Stirling engine.

OSTI ID:
5250408
Report Number(s):
CONF-840909--
Journal Information:
TMS (The Metallurgical Society) Paper Selection; (USA), Journal Name: TMS (The Metallurgical Society) Paper Selection; (USA) Vol. 56; ISSN 0197-1689; ISSN TMPSA
Country of Publication:
United States
Language:
English