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DEFORM3d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。
The contra-rotating turbine disks of an aero-engine were simplified as a counter-rotating plan disk system.
将反向旋转的高低压涡轮盘简化成了几何形状相对简单的反转盘系统。
The contra-rotating turbine disks of an aero-engine were simplified as a counter-rotating plan disk system.
将反向旋转的高低压涡轮盘简化成了几何形状相对简单的反转盘系统。
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