首页> 外文会议>EPS Conference on Plasma Physics >Design Considerations and Research and Development of a Comb-line Traveling Wave Antenna for Helicon Current Drive in DIII-D
【24h】

Design Considerations and Research and Development of a Comb-line Traveling Wave Antenna for Helicon Current Drive in DIII-D

机译:DIII-D中Helicon电流驱动梳线行驶波天线的设计考虑与研发

获取原文

摘要

In the search for efficient methods of non-inductive current drive for tokamak reactors, attention has turned to current drive using fast waves in the lower hybrid range of frequencies, referred to as whistler waves or, more recently, helicons [1]. Early experiments on this were carried out soon after the successful demonstration of current drive with the other propagating cold-plasma wave in this frequency range, the quasi-electrostatic slow lower hybrid wave. The biggest challenges in these experiments, reviewed in [2], were (1) to obtain sufficiently strong single-pass damping, essentially by producing a plasma with sufficiently reactor-like electron beta, and (2) to efficiently excite a wave with high enough parallel index of refraction n_(||) with a wave launcher at the edge of the plasma. Both of these obstacles have been in principle overcome in the DIII-D tokamak recently. At least one operating regime has been identified [3] with simultaneously high density and electron temperature at mid-radius (p~0.5) to yield predicted full first-pass absorption of 0.5 GHz helicons launched at n_(||)~3. The launcher concept, developed by General Atomics in the early 1990s [4,5] and demonstrated at 0.2 GHz on JFT-2M [6], is the 'comb-line' traveling wave antenna. As viewed from the plasma, this launcher looks like a wide phased array of many conventional Faraday-screened poloidally-oriented current-carrying straps, while the feature that makes a large number of radiating elements practical is that rf power is fed only to one end of the array (the 'upstream' end); power not radiated into the plasma from the fed element couples to the adjacent element via mutual reactance. If any power remains at the 'downstream' end of the structure, it is coupled out of the vacuum vessel via a feed structure identical to the one at the other end. Ideally, the lack of any internal reflections, or reflections from the downstream end means that a high degree of directivity is achieved, and t
机译:在寻找托卡马克反应堆的非电感电流驱动器的高效方法中,注意力已经使用较低的混合频率范围内的快速波转向电流驱动器,称为惠斯勒波或最近,直升机[1]。早期实验在该频率范围内的另一个传播冷等离子体波的成功示范之后不久进行了,准静电慢速较低的混合波。在[2]中,这些实验中的最大挑战是(1)以获得足够强烈的单通过阻尼,基本上通过产生具有足够反应的电子β的血浆,并有效激发高的波足够的折射率N_(||)在等离子体边缘的波浪发射器的折射率n_(||)。这些障碍都是最近在Diii-D Tokamak中克服的原则上。已经鉴定了至少一个操作制度[3],在半径半径(P〜0.5)的同时高密度和电子温度,收益预测在N_(||)〜3时发射的0.5GHz螺旋的完整首次过度吸收。由一般原子开发的发射器概念在1990年代初[4,5]并在JFT-2M [6]上以0.2GHz展示,是“梳子线”行波天线。如从等离子体所知,这个发射器看起来像许多传统的法拉第屏蔽的因子携带带子的广泛分阶段阵列,而制造大量辐射元件的特征是RF功率仅被馈送到一端阵列('上游'结束);通过相互电抗,从美联元件耦合到相邻元件的电力不辐射到等离子体中。如果在结构的“下游”末端保持任何功率,则它通过与另一端相同的进料结构与真空容器一起耦合。理想情况下,缺乏任何内部反射,或来自下游结束的反射意味着实现了高度的方向性,而且

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号