Development of direct HIP-bonding processes for tungsten-brush armor joining

被引:5
|
作者
Driemeyer, DE [1 ]
Slattery, KT [1 ]
Wille, GW [1 ]
Nygren, RE [1 ]
机构
[1] Boeing Co, St Louis, MO 63166 USA
来源
18TH IEEE/NPSS SYMPOSIUM ON FUSION ENGINEERING | 1999年
关键词
D O I
10.1109/FUSION.1999.849858
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
This paper reviews the design, fabrication, and high-heat-flux testing of tungsten-armored mockups for advanced divertor applications that require active cooling. These mockups represent a single cooling channel, limited length section of a typical element of the divertor plate. They employ the tungsten-brush armor form that has demonstrated acceptable performance at 25 MW/m(2) absorbed heat flux, surviving over 500 cycles at this level in previous testing at Sandia National Laboratories. The mockups discussed here represent the first attempt to adapt the direct-bonding approach to a HIP (Hot-Isostatic-Press) process, which enables brush-armor bonding over large areas with compound-curvature surfaces. The direct-bonding approach eliminates the application of a plasma-sprayed copper matrix over the bundled brush elements and the associated clean-up machining prior to bonding. Simple, modular fabrication was a key design driver for these mockups since advanced divertor modules must be affordable yet satisfy demanding performance and remote maintenance requirements. The mockups demonstrated successful armor joining using the direct-HIP process, but final high-heat flux testing was limited due to difficulties with melting of the honeycomb layer used to fixture the tungsten rods during fabrication. The paper discusses lessons-learned on these parts and concepts for eliminating the honeycomb on future mockups.
引用
收藏
页码:369 / 372
页数:4
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