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Gas turbine engine with non-axisymmetric surface contoured rotor blade platform
Gas turbine engine with non-axisymmetric surface contoured rotor blade platform
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机译：具有非轴对称表面轮廓的转子叶片平台的燃气涡轮发动机
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摘要
A rotor blade for a gas turbine engine includes a platform section between a root section and an airfoil section, the platform section having a non-axisymmetric surface contour.
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