Turbine engine alloys and crystalline orientations
作者： Dilip M. Shah , Joseph G. Hillebrand , Daniel E. Kane
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摘要: A method is provided for engineering a single crystal cast gas turbine engine first component cooperating with second component. An at least local operational stress on the determined. The has direction. orientation within or physical configuration of selected so that produces desired engagement associated either negative Poisson's effect high in Single highly textured iron- and nickel-base alloys enable one to use such temperature and/or corrosive environments.
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