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首页> 外文期刊>Electrical Engineers, Proceedings of the Institution of >Divided-winding-rotor synchronous generator. A comparison of simulated 30 MW conventional- and divided-winding-rotor turbogenerators
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Divided-winding-rotor synchronous generator. A comparison of simulated 30 MW conventional- and divided-winding-rotor turbogenerators

机译:分绕组转子同步发电机。模拟的30 MW常规和分卷式转子汽轮发电机的比较

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摘要

Experiment with a 5kVA machine showed the feasibility of a new form of turbogenerator using a rotor winding of two sections, in X formation, controlling the torque and reactive requirements separately. The performance of a conventionally wound rotor turbogenerator (c.w.r.) of 30MW size, described by Shackshaft, is compared with that of a divided-winding-rotor (d.w.r.) arrangement (CEGB patent application 2240/65) of the same machine. The analogue simulation shows that the d.w.r. can control power and reactive output satisfactorily, without altering the rotor position in relation to the generator air-gap flux. Fully rated stator current at leading power factor can be obtained continuously from no load to full load. The speed of response of the d.w.r.-generator reactive power to a step change of infinite-busbar voltage is, on average, twice that of the c.w.r. Turbogenerator stability is improved, and is shown to be independent of reactive generation or absorption, being affected only by active-power generation. Transient-stability comparisons are made by simulating 3-phase short-circuit faults close up to the high-voltage busbar, with low- and high-impedance connections to the infinite busbar. The c.w.r. simulation at full load with full excitation withstands a fault duration of 0.45s, which comes down, with reducing excitation, to 0.32s when Qu = ???????? 0.225 p.u. and rotor angle = 70???????°; 0.2s when Qu = ???????? 0.6 p.u. and rotor angle = 100???????°; and less than 0.1 s when Qu = ???????? 0.9 p.u. and rotor angle = 120???????°. Comparable d.w.r. simulation of load and excitation conditions all require a fault duration exceeding 0.4s to cause instability. Even the Qu = ???????? 2.3 p.u. condition is simulated without deterioration of control, and requires 0.4s fault duration to cause instability. The high-impedance connection to the infinite-busbar simulation shows, in general, that the maximum fault duration for each type of generator is reduced by 0.1s.
机译:用5kVA机器进行的实验表明,采用X形两段式转子绕组的新型涡轮发电机的可行性,可分别控制转矩和无功要求。将由Shackshaft描述的30MW尺寸的传统绕线式转子涡轮发电机(c.w.r.)的性能与同一机器的分卷转子(d.w.r.)装置(CEGB专利申请2240/65)的性能进行比较。模拟仿真表明d.w.r.可以令人满意地控制功率和无功输出,而无需改变转子相对于发电机气隙通量的位置。从空载到满载,可以连续获得处于领先功率因数的额定定子电流。 d.w.r.发电机无功功率对无限母线电压阶跃变化的响应速度平均为c.w.r.的两倍。涡轮发电机的稳定性得到改善,并且显示出与无功发电或吸收无关,仅受有功发电影响。通过模拟靠近高压母线的三相短路故障,并与无限母线进行低阻抗和高阻抗连接,可以进行瞬态稳定性比较。 c.w.r.在全负载下以全励磁进行的仿真可承受0.45s的故障持续时间,当Qu = ???????????时,随着励磁的减少,该故障持续时间降至0.32s。 0.225磅转子角= 70°。 Qu = ????????时为0.2秒0.6磅转子角= 100°角。当Qu = ???????????且小于0.1 s 0.9 p.u.转子角= 120°角。可比的d.w.r.负载和励磁条件的模拟都要求故障持续时间超过0.4s才能引起不稳定。连Qu = ????????? 2.3点在不降低控制能力的情况下对这种情况进行了仿真,并且需要0.4s的故障持续时间才能导致不稳定。与无限母线仿真的高阻抗连接通常表明,每种类型的发电机的最大故障持续时间都减少了0.1s。

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