Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
作者： James Charles Gautreau , Chris A. Rickert , Nicholas Francis Martin
DOI:
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摘要: A blade of an axial compressor comprising: airfoil is disclosed that has a leading edge and root; platform attached to the root airfoil; dovetail side opposite neck adjacent platform, slot in generally parallel extends from front position beyond line formed by blade.
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