Turbine disk is the heart of aero engine.
涡轮盘是航空发动机的心脏。
The LCF Ufe of the turbine disk is evaluated using the method provided by SPEY MK202 engine stress standard ( EGD - 3 ).
采用斯贝MK202发动机应力标准（EGD-3）提供的方法，对该涡轮盘的低循环疲劳寿命进行了估算。
The formation of vane-integrated disk used in high-pressure compressor of turbine engine is simulated and analyzed with the finite element method (FEM) on the platform of software DEFORM 3d.
在DEFORM 3d有限元分析软件平台上，对高压压气机整体叶盘的锻压成形过程进行了模拟与分析。
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