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Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft

机译:控制注入到客机机舱区域的进气温度的方法

摘要

With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controlled feed air, the temperature of the injected feed air is controlled for each cabin zone, dependent upon the deviation of an injection temperature actual value for the feed air injected into the cabin zone in question, measured by sensors, in relation to an injection temperature optimum value. If there is no, or at least no usable reading of the ambient temperature of this cabin zone for a cabin zone, an optimum value for the injection temperature of this cabin zone can be established in accordance with a variation, whereby it is determined upon the basis of the injection temperature optimum values and/or the injection temperature actual values of other cabin zones, whereby the measurement by sensors of the cabin temperature works reliably. In accordance with another variation, the injection temperature optimum value of a cabin zone can be established without measuring ambient temperature by sensors or without reliably measuring ambient temperature from the temperature measured for the external surrounds of the aircraft.
机译:通过一种用于控制被注入到客机的机舱区域中的进料空气的温度的方法,该客舱的机舱被细分为分别被提供有专门温度控制的进料空气的几个机舱区域,所注入的进料的温度取决于由传感器测量的,注入到所讨论的机舱区域中的进料空气的喷射温度实际值相对于喷射温度最佳值的偏差,来控制每个机舱区域的空气。如果没有或至少没有该车厢区域的环境温度对于车厢区域的可用读数,则可以根据变化来确定该车厢区域的喷射温度的最佳值,由此根据温度来确定。基于喷射温度最佳值和/或其他车厢区域的喷射温度实际值,由此通过车厢温度传感器进行的测量可靠地进行。根据另一变型,可以建立机舱区域的喷射温度最佳值,而无需通过传感器测量环境温度,或者无需从针对飞机外部环境所测量的温度可靠地测量环境温度。

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