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dc.contributor.otherTurbomachinery Symposium (27th : 1998)
dc.creatorYakuwa, Hiroshi
dc.creatorNarita, Toshio
dc.creatorKawasaki, Masamichi
dc.creatorMiyasaka, Matsuho
dc.creatorFang, Cheng
dc.creatorGo, Tetsu
dc.creatorNakahama, Shuhei
dc.date.accessioned2017-10-05T14:04:41Z
dc.date.available2017-10-05T14:04:41Z
dc.date.issued1998
dc.identifier.urihttps://hdl.handle.net/1969.1/163415
dc.descriptionLectureen
dc.descriptionPg. 49-54en
dc.description.abstractA nickel-base superalloy for FCC power recovery turbine rotors was developed, which shows excellent sulfidation-corrosion resistance, high temperature strengths, and hot workability. To investigate the influences of the alloying elements of AISI685 on the sulfidation behavior, nickel-base alloys containing each of chromium, cobalt, molybdenum, titanium, and aluminum (the major components of AISI685), and alloys containing multiple such elements were produced and corroded in sulfidizing gas atmospheres at 600°C. It was found that the sulfidation behavior, especially the penetrating behavior into the alloys, was greatly influenced by aluminum, and that the resistance could be improved by increasing the aluminum content in the alloys. Six types of alloys, in which aluminum had been increased to improve the sulfidation resistance of AISI685 and titanium decreased by the same proportion to maintain the high temperature strengths of AlSI685, were forged to test their sulfidation behavior and high temperature strengths. As a result, the alloy with 1.5 percent titanium and 3.0 percent aluminum showed only half the sulfidation depth of AISI685, for the tensile characteristics at 538°C, and at 850°C through 1100°C, equivalent or better than those of AISI685. This means that the alloy with 1.5 percent titanium and 3.0 percent aluminum has twice more sulfidationcorrosion resistance than AISI685, in addition to equal or higher high temperature strengths and hot workability. A simulation expander rotor disk of 500 mm in diameter was manufactured with the newly developed alloy. The disk was successfully produced without shear cracking or buckling problems. Furthermore, test specimens cut from the disk showed a rupture strength equal to that of AISI685 at 650°C to 750°C.en
dc.format.mediumElectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoen
dc.publisherTexas A&M University. Turbomachinery Laboratories
dc.relation.ispartofProceedings of the 27th Turbomachinery Symposiumen
dc.subject.lcshTurbomachinesen
dc.titleDevelopment Of A Sulfidation - Corrosion Resistant Nickel-Base Superalloy For FCC Power Recovery Turbine Rotors.en
dc.type.genrePresentationen
dc.type.materialTexten
dc.identifier.doihttps://doi.org/10.21423/R1B66Q


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