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Aircraft air conditioning piping structure and air conditioning system

机译:飞机空调管路结构及空调系统

摘要

PROBLEM TO BE SOLVED: To provide an aircraft air-conditioning piping structure capable of promoting mixing of temperature-controlled air flowing into a mixing chamber constituting an air-conditioning system and recirculated air, and an air-conditioning system including the same. .. SOLUTION: An air-conditioning piping structure 30 has a temperature-regulated air and a mixing chamber 3 for mixing temperature-controlled air obtained by an aircraft air conditioner 2 and recirculated air discharged from a pressurized compartment 40. Inflow recirculated air. In the air-conditioning piping structure 30, the first pipe 31R through which the temperature-regulated air flows, the second pipe 32R through which the recirculated air flows and is connected to the first pipe 31R, and the temperature-controlled air and the recirculated air merge. A flow path limiting portion 35 that provides resistance to at least one of the temperature adjusting air and the recirculated air is provided in the vicinity of the merging position 33R. [Selection diagram] Fig. 4
机译:解决的问题:提供一种飞机空调管道结构,其能够促进流入构成空调系统的混合室的温度控制空气和再循环空气的混合,以及包括该空调系统的空调系统。解决方案:空调管道结构30具有温度调节空气和混合室3,该混合室3用于混合由飞机空调2获得的温度受控空气和从增压室40排出的再循环空气。流入再循环空气。在空调配管结构30中,温度调节空气流过的第一管31R,再循环空气流过并连接到第一管31R的第二管32R,以及温度受控的空气和再循环的空中合并。在合流位置33R的附近设置有流路限制部35,该流路限制部35对温度调节用空气和再循环空气中的至少一种提供阻力。 [选择图]图4

著录项

  • 公开/公告号JP2020132015A

    专利类型

  • 公开/公告日2020-08-31

    原文格式PDF

  • 申请/专利权人 三菱航空機株式会社;

    申请/专利号JP20190029678

  • 发明设计人 石丸 卓;田中 康也;弘津 聡史;

    申请日2019-02-21

  • 分类号B64D13;F16L55;F24F13/04;F24F13/02;

  • 国家 JP

  • 入库时间 2022-08-21 11:37:36

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