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1)  gan-xia
感匣
2)  sagger [英]['sægə]  [美]['sægɚ]
匣钵
1.
Thermoresistant saggers containing silicon carbide and granular filler were produced through slip casting in plaster mould.
用石膏模浇注法生产出了含碳化硅和粒状填料的耐热匣钵。
2.
New formula and new Process flow Of large pressed sagger have been laid down through analyzing old Process flow and operating condition of the sagger,and product quality and economic benefit were raised.
通过分析大件机压匣钵的旧工艺流程和使用情况,制定了新配方和新工艺流程,从而提高了产品质量和经济效益。
3)  Stator [英]['steitə]  [美]['stetɚ]
机匣
1.
Nonlinear dynamic response analysis of unbalance-rubbing coupling faults of rotor-ball bearing-stator coupling system;
转子-滚动轴承-机匣耦合系统的不平衡-碰摩耦合故障非线性动力学响应分析
2.
Nonlinear dynamic analysis and experiment verification of rubbing faults of rotor-ball bearing-support-stator coupling system for aero-engine;
航空发动机转子-滚动轴承-支承-机匣耦合系统的碰摩故障分析与验证
4)  case [英][keɪs]  [美][kes]
机匣
1.
Analysis of mechanical properties of composite case after impact;
复合材料机匣冲击后的力学性能分析
2.
Using the numerical method and fatigue damage theory, the buckling and fatigue on the composite materials and composites case are studied for aero-engine design.
目前我国正在研制碳纤维树脂基复合材料的发动机外涵道机匣。
5)  engine case
机匣
1.
Structure of aero-engine case under the effect of combined axial pressure and end twist;
轴向压力和端部转矩载荷联合作用下机匣结构稳定性的数值分析
2.
The integration of CAD parametric modeling,finite element method,classical strength calculation theory with modern optimal design techniques produces a complete and systematic design procedure for performing parametric optimal design of turbine disk,engine case and turbine shaft.
开发了基于大型有限元分析软件Ansys的燃气涡轮发动机辅助设计系统,该系统将CAD参数建模技术、工程有限元数值计算方法、经典强度计算理论与现代优化设计技术相结合,实现了涡轮盘、机匣和涡轮轴典型零件的参数优化设计的完整设计流程,建立了结构优化设计平台;并通过机匣的结构优化设计实例,验证了燃气涡轮发动机辅助设计系统的有效性。
6)  casing [英]['keɪsɪŋ]  [美]['kesɪŋ]
机匣
1.
Experimental study of real casing containment;
航空发动机真实机匣的包容性试验
2.
Using the finite element numerical method based on the impact dynamics theory,this paper simulates the process of an aero-engine casing containment test normally run with spinning test rig.
本文采用基于冲击动力学理论的有限元数值分析方法模拟了在旋转试验器上进行的某发动机机匣的包容性试验过程,反映了撞击过程中断叶和机匣的能量变化历程,较好地模拟了试验结果。
3.
The aero-engine casing containment is important for aero-engines to improve safety and reliability.
航空发动机机匣包容性是发动机工作的安全性和可靠性的一项重要技术指标。
补充资料:感感
1.感激。
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