1) temperature of tail gas
尾气温度
2) aircraft EGT index
发动机尾气温度指数
3) temperature at the rotary kiln terminal
窑尾温度
1.
By adjusting the back pressure at the terminal and the top of a rotary kiln, the temperature at the rotary kiln terminal as well as the lengths of the drying, preheating and calcining zone in the the rotary kiln have been controlled.
通过调整窑头窑尾负压,达到控制窑尾温度和干燥带、预热带、煅烧带长度的目的。
4) plume temperature
尾焰温度
1.
Plume temperature of the rocket is an important physics parameter that reflects the propellant’s combustion condition, the temperature measurement for SPRE plays a dominant role in the total diagraph.
应用神经网络技术研究固体火箭尾焰真温测量,对于提高我国火箭发动机尾焰温度诊断水平;对科学确定火箭的使用寿命有着重大的战略意义和现实巨大的经济价值。
5) JPT
尾喷管温度
6) gas temperature
煤气温度
1.
A series of technical measures such as adjustment of gas temperatures and amelioration of the quality of circulating oil were adopted,reaching the goals of reducing naphthalene content in gas after primary cooling and energy saving.
对横管式初冷器煤气脱萘生产状况进行深入研究,通过煤气温度的调整及循环油质量的改善等一系列技术措施,达到降低初冷后煤气含萘及节能的目的。
2.
Reasons and harm of higher gas temperature at the final cooling stage are analyzed and solutions are proposed.
分析了终冷段煤气温度偏高的危害及原因，并提出了处理办法。
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条