• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文会议>International Conference on Environmental Systems >Performance validation of a cooling generation system for a pilot thermal garment
【24h】

Performance validation of a cooling generation system for a pilot thermal garment

机译：试点热衣服冷却发电系统的性能验证

获取原文
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

Pilots in fighter aircraft can be subjected to high temperatures during ground operating phases in hot climate conditions, especially if APU mode is not available. A Cooling Generation System (CGS) used with a protective thermal garment for fighter aircraft pilots has been developed that allows cooling of the pilot in the cockpit. The unit is designed to operate under worst case conditions and requires only that the pilot plugs in upon entering the cockpit. A liquid circulates inside the garment that covers the pilot's torso, arms and head (area under the helmet). The temperatures are defined to guarantee the user's comfort. The pilot can adjust the power delivered by the CGS, i.e., the temperature of the circulating fluid, up to a maximum cooling capacity of 400 W. The CGS design is based on a small variable speed compressor with a brushless motor, which is the outcome of a dedicated development, and a custom-made evaporator and condenser for maximum efficiency and minimum volume. A demonstrator of the CGS has been fabricated and tested with pilots under worst case conditions. In parallel to these tests, efforts have been made to define available volumes inside the cockpit in which the CGS can be fitted. The results of the two studies will be combined to define the flight version of the CGS. This paper describes the cooling performance validation of the CGS on a demonstrator and the design features for accommodation inside the aircraft cockpit.
机译：在热气候条件下，防撞机的飞行员可以在地面运行阶段进行高温，特别是如果不可用的APU模式。已经开发出用于用于战斗机飞行员的保护性热衣架的冷却发电系统（CGS），允许在驾驶舱内冷却飞行员。该装置旨在在最坏情况下运行，只需要飞行员插入进入驾驶舱时。液体循环衣服，覆盖飞行员的躯干，臂和头部（头盔下的区域）。温度被定义为保证用户的舒适度。导频可以调节CGS，即循环流体的温度，最大冷却能力为400W .CGS设计基于具有无刷电机的小型变速压缩机，这是结果专用开发，以及定制蒸发器和冷凝器，最大效率和最小体积。在最坏的情况下，在最坏的情况下，使用飞行员制造和测试了CGS的演示。与这些测试并行，已经努力在驾驶舱内定义可用的体积，其中可以安装CGS。两项研究的结果将组合以定义CGS的飞行版本。本文介绍了CGS对演示者的冷却性能验证以及飞机驾驶舱内的住宿的设计特征。

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