涡轮发动机

基于微型涡轮发动机实现超高能量密度PowerMEMS的研究

Research on Power MEMS Based on Micro-Gas Turbine Engine with Ultra-High Specific Energy

航空燃气涡轮发动机燃烧室的NOx控制及预测

Control and Prediction of NOx Formation in Aircraft Gas Turbine Engine Combustor

GE飞机发动机集团在燃气涡轮发动机的设计、产及维修方面处于世界领先地位。

GE Aircraft Engines is a world leader in the design , manufacture and servicing of gas turbine engines .

基于ANFIS的涡轮发动机风车工况建模仿真

Turbojet modeling and simulation in wind milling based on ANFIS

基于环境保护的要求，对燃气涡轮发动机排放物（尤其是NOx）也提出了更为严格的限制。

On the other hand , based on the environmental requirements of gas turbine engine emissions ( especially NOx ), a more stringent restrictions are proposed .

因此，人们开始将多学科设计优化（MDO，Multidisciplinarydesignoptimization）引入涡轮发动机等复杂系统及零件的设计优化中。

At the same time , there are complex coupling relationships among these disciplines . Thus , the MDO ( Multidisciplinary Design Optimization ) theory was introduced into the design procedure of complex system or their parts like turbine blade .

笔者通过对校准箱中德国涡轮发动机动力模拟器（TPS）天平的研究，提出了外式组合天平校准方法及校准原理。

In this paper , a calibration method and principle of outer composed-balance are put forward for calibrating Germany Turbine Power Simulator ( TPS ) balance on calibration tank .

航空燃气涡轮发动机前后冷气导管是一薄壁（δ＝0.2mm）零件，材质为Inconel625高温合金。

The leading and trailing inserted tube for air coolant on an aeroengine is a thin wall component , it is made of Inconel 625 alloy sheet ( thickness 02mm ) .

根据航空涡轮发动机与电厂燃气涡轮机（UGT）在尺寸、运转环境和负载要求方面的重大差异，讨论了UGT叶片和导向叶片用单晶合金的成分、力学性能和抗氧化与热腐蚀性能。

In this paper , the composition , mechanical properties and corrosion / oxidation resistance of SC alloy for UGT blades and vanes are discussed according to the significant difference between aeroturbines and UGT in size , operating environment and duty requirements .

在此基础上，搭建单轴燃气涡轮发动机模型，并在Dymola平台上对其进行启动、加速和减速等动态过程仿真，得到合理的结果，证明了该方法的可行性，通用性。

On the base of the volume modeling method and simulation libraries , the single spool gas turbine is simulated on the platform & Dymola . The rational simulation results in the process of start-up , accelerating and decelerating are obtained and proved to be reasonable .

设计生产涡轮发动机测试单元和风洞。

Designs and manufactures turbine engine test cells and wind tunnels .

微型涡轮发动机设计与制造的若干关键技术

Key Techniques for Design and Manufacture of Micro Gas Turbine Engine

涡轮发动机复杂区域的结构化网格生成技术

Creating technology of structure grid for complex region at turbine engine

微型涡轮发动机中压气机部件设计仿真及加工实验

Simulation and Fabrication of the Micro Compressor for Micro Turbine Engine

超大航深涡轮发动机系统的闭环控制

Closed-loop control of turbine engine system in super deep operation condition

航空燃气涡轮发动机熄火后自动立即点火初步探讨

The Primary Discussion of Automatic Ignition in Time after Turbojet Blowout

航空涡轮发动机对润滑油的性能要求与发展趋势

Performances Demand and Developing Trends of Lubricants for Aviation Turbine Engine

航空燃气涡轮发动机高速圆柱滚子轴承

High speed cylindrical roller bearings used in aero gas tur-bine engine

自然吸气发动机和涡轮发动机拥有不同的活塞。

Naturally aspirated engines and turbo engines have different pistons .

燃气涡轮发动机试验数据确认概念研究

Conceptual Study on Data Validation of Gas Turbine Engine Test

涡轮发动机高温隔热涂层内的传热研究

Heat Transfer in Translucent Thermal Barrier Coatings of Turbine Engine

微型涡轮发动机控制系统仿真及台架试验

Control system simulation and bed test for micro turbine engine

这架飞机的价格通常与速度较慢的涡轮发动机飞机类似。

A jet at a price usually associated with slower turboprop-engined aircraft .

涡轮发动机喷管出口速度的估计方法

Estimation Method of Nozzle Exit Speed for Torpedo Turbine Engine

油雾润滑在微型航空涡轮发动机上的应用

Application of Oil Mist Lubrication Technology on Micro Turbo Engine

航空涡轮发动机状态监控经验谈

Some Experience on Monitoring the Condition of Aircraft Turbine Engines

航空燃气涡轮发动机气路故障诊断现状与展望

State-of-the-Art and Prospect of Aircraft Engine Fault Diagnosis Using Gas Path Parameters

涡轮发动机有一个高度旋转的压气机。

The turbine engine has a compressor which turns at high speed .

自然吸气发动机和涡轮发动机中的进气门是相同的。

Intake valves are identical in the naturally aspirated and turbo engines .

分析了航空燃气涡轮发动机主轴承产生滑蹭损伤的机理与危害。

The mechanism and impact of aero-engine bearing 's skidding damage are analyzed .