首页> 外文期刊>航空太空及民航學刊, B >Fabrication and Performance Evaluation of a Micro Film-Cooled Device for Gas Turbine Blade Cooling Effectiveness
【24h】

Fabrication and Performance Evaluation of a Micro Film-Cooled Device for Gas Turbine Blade Cooling Effectiveness

机译:燃气轮机叶片冷却效率微薄膜冷却装置的制作与性能评估

获取原文
获取原文并翻译 | 示例
       

摘要

The object of our study will focus on the fabrication development for the micro film-cooled thermal chip. This thermal chip will have 50 temperature sensors, with high accuracy, starting from the exit of the slot nozzle to measure the film cooling effectiveness. In order to provide better thermal insulation, low thermal conductivity materials were selected to fabricate the slot and the film-cooled wall. Therefore, the heater on the wall can provide a perfect uniform heating condition. The height of slot can be varied at different depths. This can be used to study film cooling performance of micro wall jet at different thickness. To our knowledge, this kind of micro film-cooling performance study has not been found in the literature. The results will have a very significant impact on the gas turbine cooling design.
机译:我们的研究目标将集中在微膜冷却热芯片的制造开发上。从狭缝喷嘴的出口开始,该热敏芯片将具有50个高精度的温度传感器,以测量薄膜的冷却效果。为了提供更好的绝热效果,选择了低导热率的材料来制造缝隙和薄膜冷却壁。因此,壁上的加热器可以提供理想的均匀加热条件。槽的高度可以在不同的深度变化。这可用于研究不同厚度的微壁射流的薄膜冷却性能。据我们所知,文献中尚未发现这种微膜冷却性能研究。结果将对燃气轮机的冷却设计产生非常重大的影响。

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