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涡轮叶片是航空发动机中的关键部件之一。The turbine blade is one of the key components in aeroengine.

对某型发动机压气机第2级轮盘进行了结构可靠性分析。Structural reliability analysis of an aeroengine 2nd-stage compressor disk is presented.

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低循环多轴疲劳失效是航空发动机低压压气机轮盘的主要失效形式。Low cycle multiaxial fatigue failure is the main failure mode of aeroengine compressor disk.

最后将其应用到航空发动机的维修策略决策中。Finally, the proposed method was applied to the maintenance strategy decision making of aeroengine.

介绍了某型航空发动机冶金型号标准的编制情况及其尚存在的问题。The establishment and existing problems of metallurgy model standard for an aeroengine are introduced.

本文提供了现代航空发动机主燃烧室中三维两相燃烧流场的数值计算方法。A method is presented for computing 3-D two-phase combusting flow field in a modern aeroengine combustor.

本文将智能控制理论和方法引入到航空发动机多变量控制中。In this paper, the theory and method of intelligence control are used to aeroengine multivariable control.

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并提出了增广LQL控制方法，应用其设计了航空发动机控制系统。The augmented LQL method was proposed, then the aeroengine control system was designed by using the method.

为了对某型航空发动机涡轮转子叶片在900℃高温下进行动应力测试，研制了900℃动态应变计。A dynamic strain gage is developed for dynamic stress test at 900℃ of turbine rotor blades of an aeroengine.

航空发动机空心涡轮叶片的壁厚是保证叶片强度的一个关键参数。The wall thickness of the hollow aeroengine turbine blade is a critical parameter for ensuring its strength.

研究旨在为航空发动机构件的电子束焊接加工制造积累经验和性能数据。This research can accumulate experiences and properties data for manufacturing aeroengine components with EBW.

实验结果表明该智能位置控制器适用于航空发动机分布式控制系统。The result indicates that the smart position actuator can be applied to aeroengine distributed control systems.

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本文基于面向对象技术建立了某型双轴涡扇航空发动机的部件级气动热力模型。A component level aerothermodymamic model of a turbofan aeroengine is created in this thesis using OO technology.

该方法被用于某型双转子涡喷航空发动机稳态控制器的设计，并取得了良好效果。This method was applied to designing the steady state controller of a two spool turbojet aeroengine with success.

航空发动机主轴轴承保持架动平衡精度对轴承的性能至关重要。Dynamic balance accuracy of aeroengine main shaft bearing cage is of the utmost importance to bearing performance.

介绍了几种评定航空发动机润滑油高温氧化安定性的方法。It is introduced several evaluating methods of high temperature oxidative stability of aeroengine lubricating oil.

航空发动机是一种内燃机，其工作环境是非常恶劣的和复杂的。The aeroengine is a kind of internal -combustion engine working under very abominable and complicated environment.

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机匣是在研某型号航空发动机上的核心部件，采用铸造高温合金K423A无余量整体精密铸造而成。The case, which is cast in K423A superalloy by investment casting, is one of the core components of the aeroengine.

航空发动机重要零件如机匣、压气机风扇叶片等广泛采用钛、镍基合金等先进结构材料。Advanced aeroengine alloys such as titanium and nickel-based alloys are widely used for casing and compressor blades.

结合某型航空发动机的结构特点，创建了转子非包容顶层事件故障树。The fault tree of rotor uncontained top event was established combining the structure characteristics of an aeroengine.