首页> 外国专利> AIR CONDITIONING PIPING STRUCTURE FOR AIRCRAFT AND AIR CONDITIONING SYSTEM

AIR CONDITIONING PIPING STRUCTURE FOR AIRCRAFT AND AIR CONDITIONING SYSTEM

机译:飞机和空调系统的空调管路结构

摘要

To provide an air conditioning piping structure for an aircraft which can promote mixing of temperature adjusted air and recirculated air flowing into a mixing chamber forming an air conditioning system. An air conditioning piping structure causes temperature adjusted air obtained by an air conditioning apparatus of an aircraft and recirculated air discharged from a pressurized compartment to flow into a mixing chamber which mixes the temperature adjusted air and the recirculated air. This air conditioning piping structure includes a first pipe through which the temperature adjusted air flows, a second pipe through which the recirculated air flows, and which is connected to the first pipe, and a flow passage restricting part configured to apply a resistance to at least one of the temperature adjusted air and the recirculated air in a vicinity of a merging position where the temperature adjusted air and the recirculated air are merged.
机译:提供一种用于飞机的空调管道结构,其可以促进温度调节的空气和流入形成空调系统的混合室的再循环空气的混合。空调配管结构使由飞机的空调装置获得的经温度调节的空气和从加压室排出的再循环空气流入混合室,该混合室将经温度调节的空气和再循环的空气混合。该空调配管结构包括:第一管,被调节温度的空气流过;第二管,被循环的空气流过,并且与第一管连接;以及流路限制部,其被构造成至少对第一管施加阻力。调温空气和再循环空气中的其中之一在调温空气和再循环空气合并的合并位置附近。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

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