1) titanium-alloyed blade
钛合金叶片
1.
Study results may serve as a reference for optimizing the forging technology of titanium-alloyed blades.
利用热力耦合三维刚粘塑性有限元模拟技术对汽轮机钛合金叶片锻造过程进行了数值模拟,并以实际锻造工艺试验对其进行了验证。
2) Ti-Alloy rotor blades
钛合金动叶片
1.
This article describes how the wiser finalize the machining steps and tools considering the characteristies of 300MW unit LP-1 Ti-Alloy rotor blades,By using MasterCAM,Pro/E and RCS software,aiming at the characteristic of a five axis machine.
根据300MW机组低压次末级钛合金动叶片的特点,利用Master CAM、Pro/E和RCS联合造型,并针对五坐标机床特点,利用RCSSOFTWARE编制出合理高效的数控加工程序。
2.
This article describes how the wiser finalize the machining steps and tools considering the characteristies of 300MW unit LP-1 Ti-Alloy rotor blades,By using Mastercam,Pro/e and Rcs software,Aiming at the characteristic of a five axis machine.
根据300MW机组低压次末级钛合金动叶片的特点,利用MasterCAM、Pro/E、和RCS联合造型,并针对五坐标机床特点,利用RCSSOFTWARE编制出合理高效的数控加工程序。
3) TC11 titanium alloy blade
TC11钛合金叶片
1.
TC11 titanium alloy blade is one of aircraft engine important parts,its shape is complex and the quality requirement is high.
TC11钛合金叶片是航空发动机的重要部件之一,其型面复杂、质量要求高,在成形过程中常因锻造后的残余应力和温度应力的作用而发生翘曲变形,最终导致报废。
4) titanium alloy LP twisted blading
钛合金低压扭叶片
1.
This paper discusses the feasibility to raise maximum speed of industrial steam turbine with titanium alloy LP twisted blading.
论述了用钛合金低压扭叶片提高工业汽轮机极限转速的可行性。
6) superalloy turbine blade
高温合金叶片
1.
In this paper,a two-dimensional simulation method for grain structures of superalloy turbine blade in NDS solidification is discussed.
论述了几年来发展起来的非定向凝固高温合金叶片熔模铸造过程中晶粒组织形成的计算机二维模拟方法,包括凝固过程中晶粒组织形成的物理模型、模拟中所采用的二维胞状自动机(CA)技术。
补充资料：钛合金盘及叶片
钛合金盘及叶片
锄铁合金盘及叶片
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