中冷回热航空发动机,intercooled recuperated aero-engine(IRA)
1)intercooled recuperated aero-engine(IRA)中冷回热航空发动机
2)aero-engine hot end航空发动机热端
英文短句/例句
1.Microstructural Evolving and Failure Mechanism of 3D C/SiC in Environment Simulating Hot-Section Component Service in Aero-Engine;航空发动机热端部件模拟环境下3D C/SiC的微结构演变和失效机制
2.Preliminary analysis of thermodynamic cycle of an intercooled recuperated turbofan engine中冷回热航空涡扇发动机热力循环初步分析
3.Application and Development of Thermal Barrier Coatings on Aero Engines热障涂层技术在航空发动机上的应用与发展
4.Application of Zirconia Thermal Barrier Coating in Aeroengine二氧化锆热障涂层在航空发动机上的应用
5.Optics Measurement Method of Hot Deformation for Aeroengine Convergent/Divergent Exhaust Nozzle航空发动机收扩喷管热态变形的光学测量方法
6.Progress in Thermal Barrier Coatings for Advanced Aeroengines先进航空发动机热障涂层技术研究进展
7.Development of TBCs on Turbine Blade of Aero-engine热障涂层在航空发动机涡轮叶片上的应用
8.aero-gas turbine engine航空燃气轮机发动机
9.aero-engine aerodynamics航空发动机气体动力学
10.general aviation turbine engine通用航空涡轮发动机
11.engine ,piston, for aircraft活塞发动机,航空用
12.Investigation of Calculation Method of Fuel-Oil Radiator Performance Curve Cluster航空发动机燃-滑油散热器散热性能曲线簇计算方法研究
13.The Effects of Controlled Plasma by the External Magnetic Field on Fluid Flow and Heat Transfer of Aeroengine Nozzle;磁控等离子体对航空发动机尾喷管流动传热的影响
14.Aircraft Turbine Engine and the Specification of Engine Oil燃气涡轮航空发动机与发动机油规格
15.Research on Conjugate Heat Transfer Simulation of Aero Turbine Engine Air-Cooled Vane航空发动机气冷涡轮叶片的气热耦合数值模拟研究
16.The Coupled Thermo-mechanical Simulation on Precision Forging Process of Blade fo Aerogengine航空发动机叶片精锻成形过程的热力耦合数值模拟
17.Transient Thermal Analysis of Main Thrust Ball Bearing During Fuel Cut off for Aeroengine Oil System航空发动机滑油系统断油时主推力球轴承的瞬态热分析
18.Philips hot-air engine菲利浦斯热空气发动机
相关短句/例句
aero-engine hot end航空发动机热端
3)China National Aero-Engine Corporation (CAREC)中国航空发动机总公司
4)aeroengine航空发动机
1.Control method of time on wing for civilaeroengine;民用航空发动机在翼时间控制方法
2.Fault diagnosis and adaptive reconfiguration control for sensors inaeroengine based on improved least squares support vector;基于改进LS-SVM的航空发动机传感器故障诊断与自适应重构控制
3.Research on detection system ofaeroengine large wear particle based on microimage;基于显微图像的航空发动机大磨损颗粒检测系统研究
5)aero-engine[英]["??r?,end?in][美]["?r?,?nd??n]航空发动机
1.Establishment of Aero-engine s Model Based on SMI Identification Method;基于SMI辨识的航空发动机模型建立
bination forecasting model ofaero-engine maintenance costs based on statistic rough sets theory;基于状态的航空发动机维修成本组合预测
3.Research on Aerodynamic Detection of Aero-engine Blade;航空发动机叶片叶型无损检测气动试验研究
6)aircraft engines航空发动机
plicated nonlinear systems such asaircraft engines.对于像航空发动机这样复杂的非线性系统,基于对象精确数学模型的PID控制方法的自适应性较差,难以适应具有非线性、时变不确定性的被控对象。
2.The technology of surface modification was an efficient way to increase fatigue life of the mainshaft bearing of theaircraft engines.表面改性处理技术是一种提高航空发动机主轴轴承疲劳寿命的有效途径。
3.Considering the geometric features of the air cooled turbine blades of theaircraft engines, the methods to sort the features in the parametric modeling of the blades were advanced.针对航空发动机涡轮气冷叶片的结构特点 ,提出了叶片参数化建模的特征分类形式 。
延伸阅读
航空发动机推重比(见航空发动机推力)航空发动机推重比(见航空发动机推力)thrust to weight ratio of aeroenginehQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
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