• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文会议>Congress of the International Council of the Aeronautical Sciences; 20060903-08; Hamburg(DE) >TRANSIENT SIMULATION OF A DIRECT-EVAPORATING CO2 COOLING SYSTEM FOR AN AIRCRAFT
【24h】

TRANSIENT SIMULATION OF A DIRECT-EVAPORATING CO2 COOLING SYSTEM FOR AN AIRCRAFT

机译：飞机直接蒸发CO2冷却系统的瞬态模拟

获取原文
获取原文并翻译 | 示例
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

Integrating a direct-evaporating system in an aircraft requires an exact analysis of the operating conditions. The boundary conditions can vary significantly in temperature and humidity inside and outside the aircraft. The heat that is removed from the galleys by the refrigerant is rejected to the ambient air at the gas cooler. The presented paper shows the advantages of transient numerical simulations. Conditions which cannot be adjusted at the existing test rig can be investigated having the opportunity to see even processes like the mass movement in the system or the quality change in the heat exchangers. Furthermore it is possible to investigate operating conditions which could lead to the damaging of the test rig.
机译：在飞机上集成直接蒸发系统需要对运行条件进行精确分析。边界条件在飞机内部和外部的温度和湿度会发生很大变化。通过制冷剂从厨房去除的热量在气体冷却器中被排到周围的空气中。本文介绍了瞬态数值模拟的优势。可以研究无法在现有测试平台上进行调节的条件，从而有机会看到均匀的过程，例如系统中的质量运动或热交换器中的质量变化。此外，有可能研究可能导致测试台损坏的运行条件。

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