首页> 外文学位 >Numerical modeling of heat pipe radiator and fin size optimization for low and no gravity environments.
【24h】

Numerical modeling of heat pipe radiator and fin size optimization for low and no gravity environments.

机译:低和无重力环境下热管散热器的数值建模和翅片尺寸优化。

获取原文
获取原文并翻译 | 示例

摘要

A heat-pipe radiator element has been designed and modeled to study the efficiency of heat transfer for low and no gravity environments, like in lunar environments. The advantages of using heat pipe includes the significant weight reducing and heat transfer efficiency. The heat transfer can be enhanced by the use of condenser sections with attached fins.;A series of various geometries of solid fins and heat pipes with and without fins were modeled using FLUENTRTM. This was done to determine the validity of using a heat pipe in lieu of a solid fin projection. A heat pipe had a 25 mm outer diameter, 23 mm inner diameter, 25 mm wide fin. The heat pipe with fin was 300 mm in length. Using the power output per unit area and power output per unit mass, to verify that a design heat pipe was the best selection for a lunar radiator system. Then, heat pipes with various fin widths were modeled using FLUENTRTM and their power outputs were analyzed as a function of radiation surface area and mass.;The parametric study returned the expected results that the heat pipe provided the highest power output for both the mass and radiation area. The fin width study was used to determine the fin size that provided the most power output per unit mass. This showed an optimum fin width of 12.5 mm.
机译:对热管散热器元件进行了设计和建模,以研究低空和无重力环境(如月球环境)的传热效率。使用热管的优点包括显着的重量减轻和热传递效率。可以通过使用带有连接翅片的冷凝器部分来增强传热。;使用FLUENTRTM对一系列固体翅片几何形状以及带有和不带有翅片的热管进行建模。这样做是为了确定使用热管代替实心翅片投影的有效性。热管的外径为25毫米,内径为23毫米,散热片为25毫米。带翅片的热管的长度为300mm。使用每单位面积的功率输出和每单位质量的功率输出,以验证设计的热管是月球辐射器系统的最佳选择。然后,使用FLUENTRTM对具有不同翅片宽度的热管进行建模,并根据辐射表面积和质量对它们的功率输出进行分析。;参数研究返回了预期结果,即热管在质量和质量方面均提供了最高的功率输出。辐射面积。散热片宽度研究用于确定散热片尺寸,该尺寸可提供每单位质量最大的功率输出。这显示出最佳的翅片宽度为12.5mm。

著录项

  • 作者

    Bieger, Virginia R.;

  • 作者单位

    University of Nevada, Las Vegas.;

  • 授予单位 University of Nevada, Las Vegas.;
  • 学科 Engineering Chemical.;Engineering Aerospace.
  • 学位 M.S.E.
  • 年度 2013
  • 页码 118 p.
  • 总页数 118
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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