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Air conditioning arrangement for an aircraft with a plurality of climate zones that may be individually temperature-controlled

机译:用于具有多个气候区的飞机的空调装置,这些气候区可以分别进行温度控制

摘要

An air conditioning arrangement for an aircraft with a plurality of climate zones that may be individually temperature-controlled includes a main branching system having an air supply feed path system with a mixing chamber and a plurality of sub-branching systems branching from the mixing chamber and leading to one of the climate zones in each case. Basic temperature control means are used for controlling the temperature of the air supply in the mixing chamber. Individual temperature-control means are used on the other hand for individually controlling the temperature of the air supply in each of the sub-branching systems as a function of a desired temperature value of the respective climate zone. Basic temperature control of the air supply in the mixing chamber preferably takes place independently of a temperature requirement of the climate zone with associated combined heat and power engine.
机译:用于具有多个可单独控制温度的气候区的飞机的空调装置包括:主分支系统,该主分支系统具有带有混合室的空气供应进给路径系统;以及从所述混合室和空气分支的多个子分支系统。分别导致一个气候区。基本的温度控制装置用于控制混合室内的空气供应温度。另一方面,使用单独的温度控制装置来根据各个气候区的期望温度值单独地控制每个子分支系统中的空气供应温度。混合室中的空气供应的基本温度控制优选独立于气候区的温度要求以及相关的热电联产发动机进行。

著录项

  • 公开/公告号US8435103B2

    专利类型

  • 公开/公告日2013-05-07

    原文格式PDF

  • 申请/专利权人 NICO CENTOFANTE;

    申请/专利号US20070162147

  • 发明设计人 NICO CENTOFANTE;

    申请日2007-01-11

  • 分类号B64D13/02;

  • 国家 US

  • 入库时间 2022-08-21 16:43:17

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