1) Directionally solidified hollow blade
定向空心叶片
2) hollow blade
空心叶片
1.
The finite-element model of transient temperature field for hollow blade during laser rapid forming (LRF) process was developed.
建立了空心叶片激光快速成形过程温度场瞬态有限元数值模型,模拟了TC4钛合金空心叶片激光快速成形过程的温度场演变过程。
2.
A transient temperature/stress field finite-element model for the laser rapid forming(LRF) process of a hollow blade of aeroengine is developed.
采用随动强化及米塞斯屈服准则进行了热弹塑性分析,通过间接耦合模拟了TC4钛合金空心叶片激光快速成形的温度场/应力场演变过程。
3.
mprovement and the principle of a holding mechanism for complex ceramic core die of aero-engine hollow blades was described.
途述了某发动机空心叶片陶瓷型芯模具夹紧机构的改进及原理分析。
3) directional vane
定向叶片
4) hollow turbine blade
空心涡轮叶片
1.
Numerical simulation of solidification process of hollow turbine blade of the second generation single crystal superalloy;
第二代单晶高温合金空心涡轮叶片凝固过程数值模拟研究
6) Blade Directional Solidification
叶片定向凝固
补充资料：MS6001系列燃气轮机一级空心涡轮叶片
MS6001系列燃气轮机一级空心涡轮叶片
Ms6()()l系列燃气轮机一级空心涡轮叶片 中同科学院金属研究所供稿
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条