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涡轮机固定部分
1、turbine blade───[动力]涡轮叶片，透平叶片
2、candent turbine───坎登特涡轮机
3、steam turbine───n.蒸汽轮机; 汽机；汽轮机；蒸汽轮机；蒸汽透平
4、sucked into turbine───吸入涡轮
5、stator coil───[电]定子线圈
6、pelton turbine───水戽式[冲击式]水轮机；水轮机；培尔顿水轮机；水斗式水轮机
7、wind turbine───[动力]风力涡轮机；风轮机，风力涡轮机
1、For the turbine stator cascade, the negative curving of blade can not improve the performance of the cascades as well, the total losses of straight cascade are the lowest.───栅中部和端部二次流均增强，总平均的二次流动能增大。对于该叶栅，叶片反弯曲亦不能提高叶栅流场的气动性能，直叶片叶栅总损失最小。
2、Experimental Investigation on Influence of Incidence on Performance of Turbine Stator Cascade───冲角对涡轮低压导向器气动特性影响的实验研究
3、Numerical Simulation of Flow Field in a Turbine Stator with Film Cooling───气膜冷却涡轮导向叶片流场数值模拟
4、combination of the slot with an optimized blade design significantly reduces the secondary flow losses compared to the original turbine stator, especially at large negative angles of incidence.───联合造型后的叶栅与原始叶栅相比在各个攻角下的流动损失均有大幅度降低，大负攻角下效果尤为明显。
5、Experimental investigation on effects of blade negative bowing in turbine stator cascades───透平静叶型叶片反弯曲作用的实验研究
6、Numerical Simulation of Flow Field in Turbine Stator by Aero-thermal Coupling Method───涡轮导向器内部流场气-热耦合数值计算
7、Numerical Simulation of the Impact of Leading-edge Gas-film Pores on Cooling Effectiveness in Turbine Stator Blades───前缘气膜孔对涡轮静叶冷却效果影响的数值模拟
8、cause of turbine stator blades was analyzed on the base of numerical simulation by means of air-thermal coupling for heat transfer and temperature distribution.───在内部流场气-热耦合数值模拟的基础上，研究了某涡轮导向器叶片烧蚀故障的原因。
9、Experimental investigation on the effects of positive blade bowing in turbine stator cascadeswith low aspect ratio───低展弦比涡轮静叶栅叶片正弯曲作用的试验研究