一种适用于燃气涡轮发动机的部件。
航空燃气涡轮发动机为了提高性能经常采用中介轴承。
Intershaft bearings are often used in gas turbine engines for better performance.
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.
本发明涉及用以增强燃气涡轮发动机中的过渡导管冷却的方法和装置。
The invention relates to a method and an apparatus to enhance transition duct cooling in a gas turbine engine.
“沃斯堡”号配置燃气涡轮发动机，并将横跨太平洋进行动力装置维修。
Powered by its gas turbine engines, the USS Fort Worth will make a crippled trek across the Pacific headed to port for repairs to its propulsion system.
针对微型燃气涡轮发动机喷嘴的雾化对燃烧室火焰稳定性、温度分布和燃烧效率的影响。
The nozzle spray characteristics of micro-turbine engines affect the stabilization of flame of the combustion chamber, the distribution of temperature, and the efficiency of combustion.
前言：随着燃气涡轮发动机进口工作温度的提高，热障涂层技术受到了广泛的关注。
With the elevation of inlet working temperature of gas turbine engine, thermal barrier coatings (TBCs)are receiving a great deal of attention.
涡轮导向器喉道面积值是燃气涡轮发动机设计和生产中的重要参数，必须加以严格的控制。
The throat area of turbine nozzle which is very important in gas turbine engine's design and manufacture must be controlled strictly.
压力和温度畸变对发动机稳定性影响的评定是当代航空燃气涡轮发动机适用性战术指标的重要内容之一。
The influence of the pressure and temperature distortion to the engine stability is one of important target to evaluate aircraft engine.
燃气涡轮发动机在航空、地面和舰船上有着广泛的应用，对其进行性能评估和故障诊断有着重大的现实意义。
Gas turbine engines are widely used in the fields of air, ground and ship, so it is much of importance to assess engine performance and diagnose its faults.
目前，尽管燃气涡轮发动机以其功率大、体积小的突出优点在航空动力和其他地面动力工程中得到了广泛的应用。
At present time, the turbine engine has been widely used in aeronautics and other power engineering due to its strength in power output and small size.
MaslingIndustries在库塔·曼德拉有11名员工，主要专门负责维修直升机和中型飞机的燃气涡轮发动机。
Masling Industries employs 11 people there, running a specialised component overhaul business mainly dealing with gas turbine engines in helicopters and medium-sized aircraft.
研究人员由法国航空航天供应商赛峰集团可能被拉开，并使用3D打印机复制提供了一个古老的辅助动力的燃气涡轮发动机。
Researchers were provided an old auxiliary powered gas turbine engine by French aerospace supplier Safran that could be pulled apart and copied using a 3D printer.
以带气膜冷却孔的航空燃气涡轮发动机涡轮叶片为研究背景，引入了等效概念对密布小孔结构进行了详细的应力-应变分析。
An equivalent no-perforated plate concept is introduced in the stress-strain analysis for densely-distributed film cooling holes on turbine blades of gas turbine engines.
以带气膜冷却孔的航空燃气涡轮发动机涡轮叶片为研究背景，引入了等效概念对密布小孔结构进行了详细的应力-应变分析。
An equivalent no-perforated plate concept is introduced in the stress-strain analysis for densely-distributed film cooling holes on turbine blades of gas turbine engines.
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