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Turbine has built method of the turbine blade, turbine blade, and the turbine blades

机译:涡轮已经建立了涡轮叶片,涡轮叶片和涡轮叶片的方法

摘要

PROBLEM TO BE SOLVED: To provide an incorporation method for a turbine rotor blade for incorporating a turbine rotor blade body at a narrow pitch, the turbine rotor blade and a turbine with the turbine rotor blade.;SOLUTION: In this incorporation method for the turbine rotor blade, the turbine rotor blade body including a blade root inserted in each of a plurality of grooves formed in the circumferential direction of a turbine disk and engaged therewith, and a blade imparting the energy of rotary motion to the turbine disk, and a platform supporting the blade root and the blade is incorporated in the turbine disk. The turbine rotor blade has a plurality of kinds of turbine rotor blade bodies having platforms having different shapes, and the blade root of the turbine rotor blade boy having a prescribed platform shape is inserted in the groove in a prescribed order to the turbine disk to perform incorporation.;COPYRIGHT: (C)2008,JPO&INPIT
机译:解决的问题:提供一种用于以窄节距组装涡轮转子叶片本体的涡轮转子叶片的组装方法,涡轮转子叶片和具有涡轮转子叶片的涡轮。;解决方案:在该涡轮组装方法中转子叶片,涡轮转子叶片主体包括:叶片根部;平台,该叶片根部插入在沿涡轮盘的圆周方向形成的多个槽中的每一个中并与其接合;以及叶片,其将旋转运动的能量赋予涡轮盘。支撑叶片根部并且叶片结合在涡轮盘中。涡轮动叶片具有具有不同形状的平台的多种涡轮动叶片主体,并且将具有预定平台形状的涡轮动叶片男孩的叶根以预定顺序插入到槽中,以执行涡轮盘的操作。版权:(C)2008,JPO&INPIT

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