TY - JOUR
T1 - Stress relaxation of MCrAlY bond coat alloys as a function of temperature and strain
AU - Wereszczak, A. A.
AU - Hemrick, J. G.
AU - Kirkland, T. P.
AU - Haynes, J. A.
AU - Fitzgerald, T. J.
AU - Junkin, J. E.
PY - 1998
Y1 - 1998
N2 - The tensile stress relaxation behavior of two NiCoCrAlY bond coat alloys was examined at several temperatures between 25 and 899 °C (1650 °F) and at 0.1, 0.3, 0.5, and 0.8% strain. One alloy was made from Praxair's CO211 powder and served as the reference alloy, while the other was a Westinghouse-developed, oxide-dispersion-strengthened alloy. The specimens were loaded to the desired tensile strain at a constant strain rate, and the elastic modulus, yield strength, and yield strain were determined as a function of temperature for the two alloys using the stress/strain information from this loading segment. There was not a statistically significant difference in the high temperature elastic properties between the two alloys, although the oxide-dispersion-strengthened alloy tended to exhibit larger yield strengths. The relaxation data for both alloys were reduced into a form in which instantaneous stressing rate during relaxation was examined as a function of stress and temperature using an Arrhenius power-law model. The oxide-dispersion-strengthened alloy exhibited a larger stress exponent and activation energy than the reference alloy between 677-899 °C (1250-1650 °F), and was generally more creep resistant. The results from this study demonstrate that bond coat relaxation should occur during engine operation. Bond coatings fabricated from the oxide-dispersion-strengthened alloy have the potential to reduce residual stresses in the TBC ceramic top coating.
AB - The tensile stress relaxation behavior of two NiCoCrAlY bond coat alloys was examined at several temperatures between 25 and 899 °C (1650 °F) and at 0.1, 0.3, 0.5, and 0.8% strain. One alloy was made from Praxair's CO211 powder and served as the reference alloy, while the other was a Westinghouse-developed, oxide-dispersion-strengthened alloy. The specimens were loaded to the desired tensile strain at a constant strain rate, and the elastic modulus, yield strength, and yield strain were determined as a function of temperature for the two alloys using the stress/strain information from this loading segment. There was not a statistically significant difference in the high temperature elastic properties between the two alloys, although the oxide-dispersion-strengthened alloy tended to exhibit larger yield strengths. The relaxation data for both alloys were reduced into a form in which instantaneous stressing rate during relaxation was examined as a function of stress and temperature using an Arrhenius power-law model. The oxide-dispersion-strengthened alloy exhibited a larger stress exponent and activation energy than the reference alloy between 677-899 °C (1250-1650 °F), and was generally more creep resistant. The results from this study demonstrate that bond coat relaxation should occur during engine operation. Bond coatings fabricated from the oxide-dispersion-strengthened alloy have the potential to reduce residual stresses in the TBC ceramic top coating.
UR - http://www.scopus.com/inward/record.url?scp=0031649790&partnerID=8YFLogxK
M3 - Conference article
AN - SCOPUS:0031649790
SN - 0402-1215
JO - American Society of Mechanical Engineers (Paper)
JF - American Society of Mechanical Engineers (Paper)
IS - GT
T2 - Proceedings of the 1998 International Gas Turbine & Aeroengine Congress & Exhibition
Y2 - 2 June 1998 through 5 June 1998
ER -