中国电力 ›› 2021, Vol. 54 ›› Issue (3): 177-184.DOI: 10.11930/j.issn.1004-9649.201911021

• 发电 • 上一篇    下一篇

进气加热对燃气-蒸汽联合循环性能影响

张涛1,2, 刘志坦2, 干雪3, 付忠广1, 严志远2, 朱鸿飞2, 邱振波4   

  1. 1. 华北电力大学 火力发电国家工程技术研究中心,北京 102206;
    2. 国电科学技术研究院,江苏 南京 210031;
    3. 公诚管理咨询有限公司,广东 广州 510610;
    4. 神华国华(北京)燃气热电有限公司,北京 100024
  • 收稿日期:2019-11-05 修回日期:2020-04-20 出版日期:2021-03-05 发布日期:2021-03-17
  • 作者简介:张涛(1987-),男,博士研究生,从事燃机进气系统与联合循环性能优化技术研究,E-mail:powerzhangtao@126.com;干雪(1993-),女,通信作者,硕士,从事循环流化床技术、电力监理管理研究,E-mail:376383123@qq.com

Effect of Inlet Air Heating on the Performance of Gas-Steam Combined Cycle Power Plant Unit

ZHANG Tao1,2, LIU Zhitan2, GAN Xue3, FU Zhongguang1, YAN Zhiyuan2, ZHU Hongfei2, QIU Zhenbo4   

  1. 1. National Thermal Power Engineering & Technology Research Centre, North China Electric Power University, Beijing 102206, China;
    2. Guodian Science and Technology Research Institute, Nanjing 21003, China;
    3. Gongcheng Management Consulting Co., Ltd., Guangzhou 510610, China;
    4. Shenhua Guohua (Beijing) Gas-fired Thermoelectric Co., Ltd., Beijing 100024, China
  • Received:2019-11-05 Revised:2020-04-20 Online:2021-03-05 Published:2021-03-17

摘要: 以某200 MW级燃气-蒸汽联合循环机组为研究对象,利用余热锅炉尾部烟道废热加热给水并通过气-水换热器提高压气机进口空气温度,采用Aspen Plus模拟计算进气加热系统投运前后联合循环参数变化,分析空气进气加热对机组性能影响。研究结果表明,压气机进口空气温度由12.5 ℃提高至35 ℃时,50%、75%、87%负荷下燃机负荷率分别提高0.08、0.12、0.15,燃料消耗量分别降低0.11 kg/s、0.13 kg/s、0.10 kg/s,联合循环效率分别提高1.04%、1.03%、0.73%。95%负荷下燃机负荷率由0.95增大至1.00后保持不变,联合循环效率先增大后减小,100%负荷下燃机负荷率保持1.00不变,联合循环热效率持续降低。

关键词: 燃气-蒸汽联合循环, 燃气轮机, 进气加热系统, 进气温度, 性能分析

Abstract: Taking a 200 MW-class gas-steam combined cycle power plant unit(GSCC) as the research object, the exhaust heat in the tail flue of the HRSG was utilized to heat the feed water, which was directed afterwards into the gas-water heat exchanger to raise the inlet air temperature of the compressor. The parameter changes before and after the operation of the inlet air heating system were simulated by Aspen Plus and furthermore, the influence of inlet air heating on the performance of the GSCC at partial load was analyzed. Results show that when the inlet temperature of the compressor rise from 12.5 ℃ to 35 ℃ under the load of 50%, 75% and 87% of GSCC, the load rate of the gas turbine increases by 0.08, 0.12 and 0.15 respectively, while the fuel flow rate drops down by 0.11 kg/s, 0.13 kg/s and 0.10 kg/s respectively, and the combined cycle efficiency goes up by 1.04%, 1.03%, and 0.73% respectively. Under 95% load, the load rate of the gas turbine increases from 0.95 to the maximum 1.00, and the combined cycle efficiency increases first before taking a dip. Under 100% load, the load rate of the gas turbine remains unchanged at 1.00, while the heat efficiency of GSCC decreases continually.

Key words: GSCC, gas turbine, inlet air heating system, intake temperature, performance analysis