汽轮机技术
汽輪機技術
기륜궤기술
Turbine Technology
2015年
5期
321-325,340
,共6页
汽轮机%热力参数%变工况计算%基准负荷%方法研究
汽輪機%熱力參數%變工況計算%基準負荷%方法研究
기륜궤%열력삼수%변공황계산%기준부하%방법연구
steam turbine%thermal parameters%varying condition calculation%standard load%method study
针对汽轮机启停和变负荷运行过程中转子热应力计算所需的蒸汽热力参数很难准确确定的问题,对“低负荷应用比例法,高负荷应用变工况”的算法进行深入研究并对其完善。对该算法计算结果出现的参数波动问题进行修正处理,通过与回热系统计算的各级蒸汽参数误差分析比对,确定出最佳的变工况热力计算起点负荷和比例法计算的基准负荷。通过将修正算法下的计算结果与回热系统分析计算结果相比较,计算精度得到极大提高。提出的修正算法所需计算参数较少,在已知启动曲线的前提下,就可以得到各级特征面的热力参数,更加便于大型火电机组汽轮机变负荷下的热应力计算、寿命管理和运行经济性分析。
針對汽輪機啟停和變負荷運行過程中轉子熱應力計算所需的蒸汽熱力參數很難準確確定的問題,對“低負荷應用比例法,高負荷應用變工況”的算法進行深入研究併對其完善。對該算法計算結果齣現的參數波動問題進行脩正處理,通過與迴熱繫統計算的各級蒸汽參數誤差分析比對,確定齣最佳的變工況熱力計算起點負荷和比例法計算的基準負荷。通過將脩正算法下的計算結果與迴熱繫統分析計算結果相比較,計算精度得到極大提高。提齣的脩正算法所需計算參數較少,在已知啟動麯線的前提下,就可以得到各級特徵麵的熱力參數,更加便于大型火電機組汽輪機變負荷下的熱應力計算、壽命管理和運行經濟性分析。
침대기륜궤계정화변부하운행과정중전자열응력계산소수적증기열력삼수흔난준학학정적문제,대“저부하응용비례법,고부하응용변공황”적산법진행심입연구병대기완선。대해산법계산결과출현적삼수파동문제진행수정처리,통과여회열계통계산적각급증기삼수오차분석비대,학정출최가적변공황열력계산기점부하화비례법계산적기준부하。통과장수정산법하적계산결과여회열계통분석계산결과상비교,계산정도득도겁대제고。제출적수정산법소수계산삼수교소,재이지계동곡선적전제하,취가이득도각급특정면적열력삼수,경가편우대형화전궤조기륜궤변부하하적열응력계산、수명관리화운행경제성분석。
According to the problems that the thermal parameters for thermal stress calculation of rotor can not be accurately confirmed in the start-stop process and varying condition of steam turbine , this paper improves and perfects the algorithm by further researching the calculation method of "using the proportional method during low-load operational process and using thermodynamic calculation of turbine's varying operating conditions during high-load operational process".As for the fluctuation problems of thermal parameters , according to the calculated results error analysis and comparison of steam parameters based on the analysis of heat recovery system .The fluctuation problems are modified processing and the best starting load and standard load to using thermodynamic calculation of turbine 's varying operating conditions can be determined .By the comparison between the calculated results by modified algorithm and the calculated results by heat recovery system analysis , the calculation precision is greatly improved .It requires less calculating parameters for the modified algorithm to get all levels characteristics thermal parameters .It makes easier and faster for thermal stress calculation of thermal power turbine , life management and operational economic analysis .