期刊文献+

三轴燃气轮机发电机组突变负载控制策略研究 被引量:5

Study of the Strategies for Controlling the Abruptly Changed Load of a Three-shaft Gas Turbine Power Generator Unit
原文传递
导出
摘要 基于整机试验与仿真,对三轴燃气轮机发电机组突变负载控制策略进行了研究。试验结果表明,改进后的功率前馈加燃气发生器转速串级PID闭环控制方案具有响应速度快、抗干扰能力强和自适应性好的特点,可满足瞬态发电要求。当突增40%负载时,动力涡轮转速下降值不大于4%,恢复时间不超过2 s;仿真结果表明,甩负荷时提前打开低压压气机出口放气阀放气不仅改善了压气机工作裕度,还可以抑制动力涡轮转速的增长,当放气25%时动力涡轮转速超调量与不放气相比下降3%,恢复时间减少10 s。 On the basis of the experiment and simulation of an integral machine,studied were the strategies for controlling the abruptly changed load of a three shaft gas turbine power generator unit. The test results show that the improved power forward feed + gas turbine rotating speed cascade PID closed cycle control version features a quick response,strong anti-interference ability and good self adaptability,thus capable of meeting the needs for transient power generation. In the case of an abrupt increase of a 40% load,the drop in the rotating speed of the power turbine will not be higher than 4% and the recovery time duration will not exceed 2 s. The simulation results show that in the case of load rejection,to open in advance the bleeding valve at the outlet of the low pressure air compressor to bleed air not only can improve the work allowance but also can contain the growth of the rotating speed of the power turbine. When the air quantity bled arrives at 25% of the rated air flow rate,the overshoot of the rotating speed of the power turbine will decline by 3% and the recovery time duration will shorten by 10 s compared with those when no air is bled.
出处 《热能动力工程》 CAS CSCD 北大核心 2016年第11期26-31,共6页 Journal of Engineering for Thermal Energy and Power
关键词 突变负载 控制策略 串级 前馈 试验与仿真 abruptly changed load control strategy cascade forward feed experiment and simulation
  • 相关文献

参考文献5

二级参考文献24

  • 1清华大学.燃气轮机[M].水利电力出版社,1978..
  • 2闻雪友,肖东明.对发展大功率船用燃气轮机的新思考[J].舰船科学技术,2007,29(4):17-21. 被引量:14
  • 3[俄]涅恰耶夫.航空动力装置控制规律与特性[M].单凤桐,程振海译.北京:国防工业出版社,1999.
  • 4Martucci A,Volponi A J.Fuzzy Fuel Flow Selection Logic for a Real Time Embedded Full Authority Digital Engine Control[J].Journal of Engineering for Gas Turbines and Power,2003,125:909~ 916.
  • 5邢家瑞,等编译.多状态飞机动力装置综合控制[M].辽宁沈阳:沈阳航空发动机研究所,1996.
  • 6[俄]古列维奇,戈尔别格.航空燃气涡轮发动机的控制方法与燃气涡轮发动机过渡态特性的数学模拟[M].程心健,朱旭津,于维凤,等译.无锡:中国航空动力控制系统研究所,1998.
  • 7胡晓煜.美国航空发动机控制技术的发展历程[J].动力控制,2004,(4):14-22.
  • 8APSLEY J M, GONZALEZ-VILLASENOR A, et al. Propulsion drive models for full electric marine propulsion systems [J]. IEEE Transactions on Industry Applications, 2009, 45(2):676-684.
  • 9PARKER D S, HODGE C G. The Electric warship [C]// Electrical Machines and Drives, 1997 Eighth International Conference on Conf. Publ. No. 444, Cambridge, Britain, 1997:319-325.
  • 10AL-HAMDAN Q z, EBAID M S Y. Modeling and simulation of a gas turbine engine for power generation [J]. ASME Journal of Engineering for Gas Turbines and Power, 2006 (128):302-311.

共引文献22

同被引文献44

引证文献5

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部