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turbine-driven相关的网络例句

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In 1989, Dr Mohana Rao, then a junior technician at the Gas Turbine Research Establishment, Bangalore, immersed himself in the ambitious Kaveri programme, which was designing a jet engine for the Tejas Light Combat Aircraft.

1989年,&莫喊啦。闹&博士那时还是位于班加罗尔的&印度涡轮燃气研究院&的一名初级技师。那时候,他正全心投入于雄心勃勃的&卡佛力项目&。该项目是LCA光辉战斗机的配套发动机。

The Grand Island plant would create more than 200 new jobs and produce lighter and stronger wind turbine blades using composite materials such as glass, carbon, resin, foam and balsa wood.

这项优惠政策的资金将用于包括智能电网、太阳能、风能以及能效管理技术等清洁能源领域创造1.7万个就业。该政策将惠及43个州的183个项目。

It takes a certain kind of man or woman to strap themselves down in what basically amounts to an over-sized arrowhead with a four-thousand horsepower helicopter turbine engine lodged in the back-end.

它在什么采取一某一男人或妇女束缚自己下来基本上共计有在这个支持者寄宿的四千马力直升机涡轮发动机的一个过大的箭头。

The traditional geothermal systems rely on the search for natural underground steam and hot spring area, and the EGS high temperature through the broken rock to form the water cycle access through the use of the traditional steam turbine power generation.

传统的地热系统依赖于寻找自然存在的地下蒸汽和温泉区,而EGS是通过破碎高温岩,形成水循环通道,利用产生的蒸汽通过传统的涡轮发电。

This will be a turbo-electric system based on proven water turbine systems used in landbased arresting gear, but with a lighter synthetic cable system and an electromagnetic motor to meet the USN's performance goals.

这是一个在验证过的陆基制动装置所使用的水轮机系统基础上发展而来的涡轮发电系统,它和一套更轻型的综合电缆系统还有一台电动机一起满足美国海军的性能要求。

Heat transfer in channel for trailing edge of turbine blade with pin-fin arrays is studied numerically.

对涡轮叶片尾缘针肋通道的换热进行了数值模拟研究。

In this paper, heat transfer and fluid flow in passage for trailing edge of turbine blade with pin-fin arrays is studied numerically.

本文应用湍流模型对涡轮叶片尾缘针肋通道的换热与流动进行了二维数值模拟研究。

With the development of aero turbine engines technology, it requires that ceramics for thermal barrier coatings have lower thermal conductivity and higher phase stability.

航空发动机技术的发展,要求热障涂层用陶瓷材料应具有更低的热导率和更高的相稳定性能。

The study of thermal barrier coatings is the sticking point of exploiting thermal barrier coating system, which is used in the next generation of high performance aero turbine engine.

热障涂层陶瓷材料的研究是开发适用于下一代高性能航空涡轮发动机热障涂层体系的关键,也是未来热障涂层技术发展的重要方向之一。

The computer simulation of ceramic thermal barrier coating on turbine engine blades during loading process has been conducted.

本文通过在计算机中建立航空发动机叶片的工作环境,进而模拟在飞行状态下叶片表面涂敷的陶瓷热障涂层的受力行为,获得了陶瓷涂层在热气动载荷作用下应力场分布,并得出应力场分布与涂层结构和叶片几何形状及与承受的载荷之间的关系,提出了进一步提高陶瓷热障涂层的使用寿命的途径。

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