| 1. | Brief introduction for gas turbine inlet air cooling system
浅述燃气轮机的进气冷却技术 |
| 2. | turbine inlet temperature
涡轮机入口温度 |
| 3. | Tit turbine inlet temperature
机进气温度 |
| 4. | turbine inlet pressure
涡轮机入口压力 |
| 5. | Temperature analysis on gas turbine inlet air by water spray evaporative cooling
燃气轮机进气采用喷雾蒸发冷却方式的温度分析 |
| 6. | The economic beneficail demonstration for combustion turbine inlet evaporative cooling installation
燃气轮机进气蒸发冷却装置经济效益的论证 |
| 7. | A two-dimensional navier-stokes equation was solved to predict the unsteady, multipassage flow and temperature fields with hot streak in turbine inlet
摘要通过求解二维n-s方程对多通道涡轮级进口有温度畸变时的流场和温度场进行了非定常数值模拟。 |
| 8. | The structure and the aerodynamics performance of marine gas turbine inlet system is one of the important aspects when the gas turbine is installed on the naval vessels
船用燃气轮机进气系统的结构和气动性能是燃气轮机装舰技术研究的一个重要组成部分。 |
| 9. | Experimental studies on s1a-02 gas turbine with water injection into compressor interstage / inlet as well as that on turbocharger self-loop test rig with inlet water injection are introduced . test results are in good accordance with simulation results, wet compression can lower compression work and increase engine power output so engine performance is enhanced, if engine power output is not changed, efficiencies of compressor and this engine become higher and turbine inlet temperature and fuel consumption become lower and if keeping t4 the same as that before wet compression is used, efficiencies become furthermore higher and engine power output increases greatly
实验结果和计算结果同样表明：湿压缩减少了压气机所消耗的压缩功，增加了燃气轮机的输出功率，提高了燃气轮机性能，如果保持发动机输出功率恒定，湿压缩可以提高压气机和整个燃气轮机机组的效率，与此同时，涡轮进口温度t_3~*和燃油消耗率下降；如果保持涡轮排气温度t_4~*恒定，压气机和燃气轮机机组效率进一步提高，燃气轮机输出功率增加。 |
