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1)  turbine wheel
涡轮叶轮
1.
Based on the principle of optimization design,structure optimization of JP60 turbine wheel was carriedout using optimization module of ANSY and APDL in order to obtain minimum turbine weight when retaining.
以车用增压器JP60涡轮叶轮为研究对象,基于最优化设计的原理,在不改变叶型及流道并保证涡轮叶轮结构强度的基础上,利用ANSYS优化设计模块及APDL语言编制用户程序,以涡轮叶轮重量最小为目标对增压器涡轮叶轮进行了减重结构优化。
2.
Taking into consideration the material nonlinearity of turbocharger compressor impellers and turbine wheels,we carry out elastoplasticity numerical analysis of their burst speed based on FEM software ANSYS.
基于ANSYS有限元分析软件,对车用涡轮增压器涡轮叶轮和压气机叶轮进行了材料非线性弹塑性有限元数值分析,计算了涡轮叶轮和压气机叶轮在离心载荷作用下的破裂转速,并与试验结果进行了对比。
3.
Considering material nonlinearity of turbocharger compressor impeller and turbine wheel, Elastoplasticity numerical analysis is carried out for burst speed based on FEM software ANSYS.
基于 ANSYS 有限元分析软件,对车用涡轮增压器涡轮叶轮和压气机叶轮进行了材料非线性弹塑性有限元数值分析,计算了涡轮叶轮和压气机叶轮在离心载荷作用下的破裂转速,并与试验结果进行了对比。
2)  turbine blades
涡轮叶片
1.
Parametric design of turbine blades based on feature modeling;
基于特征造型技术的涡轮叶片参数化设计
2.
Research on Fatigue Life of Large Gas Turbine Blades;
大型燃气轮机涡轮叶片疲劳寿命研究
3.
The single crystal Ni-base superalloys were widely used for manufacturing advance gas turbine blades,but the ignored weakness of these alloys to date is that the extent of primary creep at intermediate temperature is much higher than that at high temperature.
单晶镍基高温合金已广泛用于制造先进燃气涡轮叶片,但这种合金至今仍被忽视的薄弱环节是它的中温Ⅰ阶蠕变伸长量远高于高温蠕变,而且与高温蠕变相比,中温Ⅰ阶蠕变对取向偏离、合金成分和热处理组织的变化更为敏感。
3)  Turbine blade
涡轮叶片
1.
Error Analysis on Turbine Blade;
精铸涡轮叶片的误差分析技术
2.
Displacement transfer with the mesh deformation method in multidisciplinary optimization of turbine blades;
基于网格变形技术的涡轮叶片变形传递
3.
Turbine blade design and optimization based on the combination means of parametric-Bezier curve;
基于参数法和贝塞尔曲线的涡轮叶片造型及其优化
4)  turbine cascade
涡轮叶栅
1.
Upstream wake-passage vortex interaction in turbine cascade;
上游尾迹与涡轮叶栅通道涡相互作用研究
2.
Numerical simulation of the three-dimensional flow field of transonic turbine cascade;
跨声速涡轮叶栅三维流场的数值模拟
3.
Boundary layer transition detection on blade surface in low speed turbine cascade wind tunnel;
低速涡轮叶栅风洞中叶片表面边界层转捩图像捕捉
5)  turbine rotors
涡轮动叶
1.
Tip clearance flow is one of the most important resources of losses in turbine rotors.
叶顶间隙流动是导致涡轮动叶中产生流动损失的主要原因之一。
6)  turbo blade
涡轮叶片
1.
Research and Application of Parting Design for Turbo Blade Mould with the Case- based Reasoning (CBR);
基于事例推理技术的涡轮叶片精铸模分模设计研究与应用
2.
An integration system is set up to meet the need for information integration in the process of mold design and manufacture and detection of aero-engine turbo blade by investment casting.
为满足航空发动机涡轮叶片精铸模具设计、制造、叶片铸件检测流程对信息集成的需求,提出构建精铸模具集成设计系统平台。
3.
Seven stageⅠturbo blades fractured during working time of an engine.
某发动机在服役过程中,有7片Ⅰ级涡轮叶片连续发生断裂或开裂。
补充资料:半开式叶轮
分子式:
CAS号:

性质:没有轮盖的离心式叶轮。由整块锻件铣制成型,叶片和轮盘的一整体,且都做成径向直叶片。其结构强度高,叶轮的圆周速,度可达450~500m/s,单级压力比高,但叶道中气流速度和马赫数较高,泄漏损失较大,级效率此闭式叶轮低,工况稳定性差。广泛用于内燃机透平增压器和小功率燃气轮机的离心式压缩机,在固定式离心式压缩机上的应用也增多。

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