This paper shows the effect of excess air on combustion gas temperature at turbine inlet, and how it determines power and thermal efficiency of a gas turbine at different pressure ratios and excess air. In such a way ...This paper shows the effect of excess air on combustion gas temperature at turbine inlet, and how it determines power and thermal efficiency of a gas turbine at different pressure ratios and excess air. In such a way an analytic Equation that allows calculating the turbine inlet temperature as a function of excess air, pressure ratio and relative humidity is given. Humidity Impact on excess air calculation is also analyzed and presented. Likewise it is demonstrated that dry air calculations determine a higher level for calculations that can be performed on wet air.展开更多
This paper briefly introduced the structure and compo- sition of gas turbine inlet air filtration system, and analyzed the reason why inlet air titration system cannot adapt to bad weather. Meanwhile, some optimized t...This paper briefly introduced the structure and compo- sition of gas turbine inlet air filtration system, and analyzed the reason why inlet air titration system cannot adapt to bad weather. Meanwhile, some optimized transformation plans are proposed in this paper, such as arranging the coarse filter G3 in the anti- freeze warehouse and adding medium efficiency filter M5 etc. Furthermore, the net benefit in the first year after the optimized transformation is calculated. These optimized transformation plans could effectively decrease the rising velocity of air inlet system＇s total pressure differences, reduce the workload and costs of maintenancing air inlet system, extent the lifespan of fine cartridge, enhance the adaptability against bad weather of unit, improve the security and stability of unit operation and in- crease the economic benefit of unit, which is worth of populari- zation and application in the optimized transformation of similar gas turbine inlet system.展开更多
A novel adjusting method for improving gas turbine(GT)efficiency and surge margin(SM)under partload conditions is proposed.This method adopts the inlet air heating technology,which uses the waste heat of lowgrade heat...A novel adjusting method for improving gas turbine(GT)efficiency and surge margin(SM)under partload conditions is proposed.This method adopts the inlet air heating technology,which uses the waste heat of lowgrade heat source and the inlet guide vane(IGV)opening adjustment.Moreover,the regulation rules of the compressor inlet air temperature and the IGV opening are studied comprehensively to optimize GT performance.A model and calculation method for an equilibrium running line is adopted based on the characteristic curves of the compressor and turbine.The equilibrium running lines calculated through the calculation method involve three part-load conditions and three IGVopenings with different inlet air temperatures.The results show that there is an optimal matching relationship between IGV opening and inlet air temperature.For the best GT performance of a given load,the IGV could be adjusted according to inlet air temperature.In addition,inlet air heating has a considerable potential for the improvement of part-load performance of GT due to the increase in compressor efficiency,combustion efficiency,and turbine efficiency as well as turbine inlet temperature,when inlet air temperature is lower than the optimal value with different IGV openings.Further,when the IGV is in a full opening state and an optimal inlet air temperature is achieved by using the inlet air heating technology,GT efficiency and SM can be obviously higher than other IGVopenings.The IGV can be left unadjusted,even when the load is as low as 50%.These findings indicate that inlet air heating has a great potential to replace the IGV to regulate load because GT efficiency and SM can be remarkably improved,which is different from the traditional viewpoints.展开更多
文摘This paper shows the effect of excess air on combustion gas temperature at turbine inlet, and how it determines power and thermal efficiency of a gas turbine at different pressure ratios and excess air. In such a way an analytic Equation that allows calculating the turbine inlet temperature as a function of excess air, pressure ratio and relative humidity is given. Humidity Impact on excess air calculation is also analyzed and presented. Likewise it is demonstrated that dry air calculations determine a higher level for calculations that can be performed on wet air.
文摘This paper briefly introduced the structure and compo- sition of gas turbine inlet air filtration system, and analyzed the reason why inlet air titration system cannot adapt to bad weather. Meanwhile, some optimized transformation plans are proposed in this paper, such as arranging the coarse filter G3 in the anti- freeze warehouse and adding medium efficiency filter M5 etc. Furthermore, the net benefit in the first year after the optimized transformation is calculated. These optimized transformation plans could effectively decrease the rising velocity of air inlet system＇s total pressure differences, reduce the workload and costs of maintenancing air inlet system, extent the lifespan of fine cartridge, enhance the adaptability against bad weather of unit, improve the security and stability of unit operation and in- crease the economic benefit of unit, which is worth of populari- zation and application in the optimized transformation of similar gas turbine inlet system.
基金supported by Project 2017-II-0007-0021 of the National Science and Technology Major Project of China.
文摘A novel adjusting method for improving gas turbine(GT)efficiency and surge margin(SM)under partload conditions is proposed.This method adopts the inlet air heating technology,which uses the waste heat of lowgrade heat source and the inlet guide vane(IGV)opening adjustment.Moreover,the regulation rules of the compressor inlet air temperature and the IGV opening are studied comprehensively to optimize GT performance.A model and calculation method for an equilibrium running line is adopted based on the characteristic curves of the compressor and turbine.The equilibrium running lines calculated through the calculation method involve three part-load conditions and three IGVopenings with different inlet air temperatures.The results show that there is an optimal matching relationship between IGV opening and inlet air temperature.For the best GT performance of a given load,the IGV could be adjusted according to inlet air temperature.In addition,inlet air heating has a considerable potential for the improvement of part-load performance of GT due to the increase in compressor efficiency,combustion efficiency,and turbine efficiency as well as turbine inlet temperature,when inlet air temperature is lower than the optimal value with different IGV openings.Further,when the IGV is in a full opening state and an optimal inlet air temperature is achieved by using the inlet air heating technology,GT efficiency and SM can be obviously higher than other IGVopenings.The IGV can be left unadjusted,even when the load is as low as 50%.These findings indicate that inlet air heating has a great potential to replace the IGV to regulate load because GT efficiency and SM can be remarkably improved,which is different from the traditional viewpoints.
