基于分層模態(tài)綜合法的大型汽輪發(fā)電機(jī)組轉(zhuǎn)子-末級(jí)葉片耦合系統(tǒng)扭轉(zhuǎn)振動(dòng)分析
發(fā)布時(shí)間:2018-09-12 08:39
【摘要】:針對(duì)應(yīng)用三維有限元法計(jì)算大型汽輪發(fā)電機(jī)組轉(zhuǎn)子-末級(jí)葉片耦合系統(tǒng)扭轉(zhuǎn)振動(dòng)時(shí)存在自由度多和難以實(shí)現(xiàn)等問(wèn)題,在模態(tài)綜合法(CMS)的基礎(chǔ)上,推導(dǎo)了計(jì)算轉(zhuǎn)子-末級(jí)葉片耦合系統(tǒng)振動(dòng)的分層二重CMS法的基本方程,給出了降階的思路和原理.采用該方法對(duì)某1 000 MW汽輪發(fā)電機(jī)組的轉(zhuǎn)子、末級(jí)和次末級(jí)葉片組成的耦合系統(tǒng)進(jìn)行了扭轉(zhuǎn)振動(dòng)特性計(jì)算和分析,與不考慮末級(jí)、次末級(jí)葉片實(shí)際結(jié)構(gòu)影響的固有振動(dòng)特性進(jìn)行了對(duì)比.結(jié)果表明:如果不考慮末級(jí)葉片的實(shí)際結(jié)構(gòu),會(huì)漏掉一些重要的振動(dòng)模態(tài),給轉(zhuǎn)子和葉片的安全帶來(lái)隱患;降階前系統(tǒng)的自由度達(dá)到1.5億,而降階后系統(tǒng)的廣義自由度僅為原自由度的0.07%;分層二重CMS法可用于大功率機(jī)組轉(zhuǎn)子、末級(jí)、次末級(jí)耦合系統(tǒng)的扭轉(zhuǎn)振動(dòng)分析.
[Abstract]:In order to solve the problems of many degrees of freedom and difficulty to realize the torsional vibration of the rotor-last-stage blade coupling system of large turbine-generator set by using three-dimensional finite element method, the modal synthesis method (CMS) is used to solve the problem. The basic equations of the layered double CMS method for calculating the vibration of the rotor-final blade coupling system are derived, and the idea and principle of reducing the order are given. This method is used to calculate and analyze the torsional vibration characteristics of the coupled system composed of the rotor, the last stage and the secondary stage of a 1 000 MW turbine-generator set. The natural vibration characteristics of the actual structure of the secondary stage blade are compared. The results show that if the actual structure of the final stage blade is not considered, some important vibration modes will be missed, which will bring hidden trouble to the safety of rotor and blade, and the degree of freedom of the system before reducing the order can reach 150 million, The generalized degree of freedom of the reduced system is only 0.07 of the original degree of freedom, and the layered dual CMS method can be used to analyze the torsional vibration of the rotor, the last stage and the second stage coupling system of the high-power unit.
【作者單位】: 西安交通大學(xué)機(jī)械結(jié)構(gòu)強(qiáng)度與振動(dòng)國(guó)家重點(diǎn)實(shí)驗(yàn)室;東方汽輪機(jī)有限公司;
【基金】:國(guó)家973計(jì)劃資助項(xiàng)目(2011CB706505) 國(guó)家自然科學(xué)基金資助項(xiàng)目(51275385)
【分類號(hào)】:TM311
[Abstract]:In order to solve the problems of many degrees of freedom and difficulty to realize the torsional vibration of the rotor-last-stage blade coupling system of large turbine-generator set by using three-dimensional finite element method, the modal synthesis method (CMS) is used to solve the problem. The basic equations of the layered double CMS method for calculating the vibration of the rotor-final blade coupling system are derived, and the idea and principle of reducing the order are given. This method is used to calculate and analyze the torsional vibration characteristics of the coupled system composed of the rotor, the last stage and the secondary stage of a 1 000 MW turbine-generator set. The natural vibration characteristics of the actual structure of the secondary stage blade are compared. The results show that if the actual structure of the final stage blade is not considered, some important vibration modes will be missed, which will bring hidden trouble to the safety of rotor and blade, and the degree of freedom of the system before reducing the order can reach 150 million, The generalized degree of freedom of the reduced system is only 0.07 of the original degree of freedom, and the layered dual CMS method can be used to analyze the torsional vibration of the rotor, the last stage and the second stage coupling system of the high-power unit.
【作者單位】: 西安交通大學(xué)機(jī)械結(jié)構(gòu)強(qiáng)度與振動(dòng)國(guó)家重點(diǎn)實(shí)驗(yàn)室;東方汽輪機(jī)有限公司;
【基金】:國(guó)家973計(jì)劃資助項(xiàng)目(2011CB706505) 國(guó)家自然科學(xué)基金資助項(xiàng)目(51275385)
【分類號(hào)】:TM311
【參考文獻(xiàn)】
相關(guān)期刊論文 前5條
1 許楚鎮(zhèn),張恒濤;汽輪發(fā)電機(jī)組軸系扭振事故剖析和技術(shù)開發(fā)展望[J];動(dòng)力工程;1990年02期
2 楊建剛,高N,
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