TGT:涡轮燃气温度
涡轮燃气温度(Turbine Gas Temperature,简称TGT)是航空航天等综合领域中的常用专业术语,多用于描述发动机内部关键工作参数。为便于快速书写和实际应用,该术语常被缩写为TGT,既简洁又通用。
Turbine Gas Temperature具体释义
Turbine Gas Temperature的英文发音
例句
- Increasing turbine inlet gas temperature is one of important means to improve turbine efficiency and increase thrust-weight ratio.
- 提高涡轮前燃气温度是提高涡轮效率、增加推重比的重要手段之一。
- With the increase of the turbine inlet gas temperature, the study on the thermal control of turbine vane endwall has become more and more important.
- 随着涡轮进口燃气温度水平不断提高,涡轮叶栅端壁区域的热控制成为研究的热点问题。
- Hot components thermal protection is one of the core technologies of gas turbine, gas temperature before turbine has been improved constantly, and already exceeded the capacity of material, to ensure that the turbine normal work must use reasonable protection measures.
- 燃气轮机热端部件的热防护是燃气轮机核心技术之一,随着涡轮前燃气温度的不断提高,已远远超过了材料的可承受能力,必须采用合理的防护措施以保证涡轮正常工作。
- With the development of the aero-engine direction to the high thrust-weight ratio, and turbine inlet gas temperature continuously growing, the ability to endure temperature of existing high temperature alloys has been close to the limit.
- 随着航空发动机向高推重比方向发展,涡轮前燃气温度不断提高,现有高温合金材料的承温状况都己接近极限。
- In Wenzhou Power Plant, E type gas turbine from GE company is used and the inlet gas temperature is 1100 ℃ now. Therefore, the power generation and supply efficiencies are 48.39 % and 47.66 %, respectively.
- 以温州300MW燃气-蒸汽联合循环发电厂为例,选用的燃气轮机为GE公司的E型,燃气轮机进气温度为1100℃,目前其发电效率为48.39%,供电效率为47.66%。
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