To most people a gas turbine engine is the huge cylinder bolted beneath the wing of a commercial airliner, although they are also widely used in stationary power plants.
对大多数人来说，燃气轮机是一个巨大的圆柱体型的东西，安装在商用飞机上，其实它们也被广泛应用在固定的发电设备中。
A small turbine engine in the airplane for supplying electrical and pneumatic power for systems operation on the ground or in flight.
辅助动力装置是飞机内的小涡轮发动机，在地面或空中给各系统提供电源和气源。
A component suitable for use in a gas turbine engine.
一种适用于燃气涡轮发动机的部件。
In one aspect, the present disclosure is directed to a turbine engine (10).
本发明一方面涉及一种涡轮发动机(10)。
The major new feature, however, was the fitting of a multi-fuel gas turbine engine.
无论如何，主要的新特性是一种可以适应多种燃料的涡轮发动机。
The invention relates to a method and an apparatus to enhance transition duct cooling in a gas turbine engine.
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。
A gas turbine engine assembly (8) includes a gas turbine engine (12) mounted on a three-point mounting frame (10).
本发明涉及一种气体涡轮发动机组件(8)，其包括安装在三点式安装框架(10)上的气体涡轮发动机(12)。
The invention relates to a combined cycle of a high-power diesel engine and a one-level turbine engine with one pump.
大功率柴油机与一泵一级涡轮发动机联合循环。
The invention relates to a combined cycle of a high-power diesel engine and a divided-flow two-level turbine engine with one pump.
大功率柴油机与分流式一泵两级涡轮发动机联合循环。
The invention relates to a combined cycle of a high-power diesel engine and a divided-flow two-level turbine engine with two pumps.
大功率柴油机与分流式两泵两级涡轮发动机联合循环。
So it is necessary to estimate quantitatively the radiation effect in the thermal analysis of turbine engine under high temperature.
氧化锆、陶瓷等涂层材料对热辐射是半透明的，因此，高温下涡轮发动机的热分析需要考虑涂层内辐射换热的影响。
The one-level turbine engine with one pump is composed of a turbine, a turbine shaft, a booster pump wheel and an expansion chamber shell.
一泵一级涡轮发动机由涡轮、涡轮轴、增压泵轮和膨胀室壳体组成。
With the elevation of inlet working temperature of gas turbine engine, thermal barrier coatings (TBCs)are receiving a great deal of attention.
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。
Aerospace OEMs and their suppliers require quality air flow measurements of passages in both aircraft and land based turbine engine components.
航空生产商和他们的供应商要求高质量的通道空气流量计量，用于航天和陆地涡轮发动机组件。
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.
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。
The mathematic model of gas turbine engine is important for the development of ship power and its control system. The key of modeling is the precision and convergence.
建立燃气轮机数学模型是船舶动力及其控制系统研制的重要手段，建模的关键在于提高精度和收敛速度。
The aerodynamic performance of turbomachinery for an gas turbine engine based on a semi-closed cycle employing carbon dioxide as the primary working fluid was analyzed.
本文对采用二氧化碳作为基本工作流体的半闭环燃气轮机循环的空气动力学特性进行了详尽的分析。
The divided-flow two-level turbine engine with one pump is composed of a turbine, a turbine shaft, a two-level booster pump wheel, a guide pulley and the expansion chamber shell.
分流式一泵两级涡轮发动机由涡轮、涡轮轴、两级增压泵轮、导轮和膨胀室壳体组成。
The formation of vane-integrated disk used in high-pressure compressor of turbine engine is simulated and analyzed with the finite element method (FEM) on the platform of software DEFORM 3d.
在DEFORM3d有限元分析软件平台上，对高压压气机整体叶盘的锻压成形过程进行了模拟与分析。
Turbine blade including guide blade and work blade is one of the crucial heated end components of gas turbine engine to convert heat energy of burning gas to revolving mechanism kinetic energy.
航空发动机涡轮叶片，包括导向叶片和工作叶片，是将燃气的热能转换为旋转的机械动能的重要的热端部件。
The problem of altering the rotating coordinate system to absolute coordinate system is often encountered when the frequency characteristics of unsteady vortex shedding in turbine engine is studied.
在研究叶轮机械转动部件非定常旋涡脱落频谱特性时，难以避免会遇到旋转坐标系向绝对坐标系转换的问题。
The problem of altering the rotating coordinate system to absolute coordinate system is often encountered when the frequency characteristics of unsteady vortex shedding in turbine engine is studied.
在研究叶轮机械转动部件非定常旋涡脱落频谱特性时，难以避免会遇到旋转坐标系向绝对坐标系转换的问题。
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