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METHOD AND DEVICE FOR ENVIRONMENTAL CONTROL OF AN AIRCRAFT SUPPLIED WITH BLEED AIR AT INTERMEDIATE PRESSURE

机译:中压泄气的飞机环境控制方法和装置

摘要

The invention relates to a method and a device for environmental control of cabin (11) aircraft. A compressor air intake (39) of the aircraft engine at a single intermediate pressure value is connected to an inlet of a compressor (48) of an intermediate turbocharger (47), an air outlet of this compressor (48) is connected to an inlet of an air cycle turbine engine (15), an output of the air cycle turbine engine is connected to the cabin (11), an inlet of a turbine (49) of the turbocharger (47) intermediate coupled to the compressor (48) receives air from the cabin (11), and the air pressure delivered to the air outlet of the compressor (48) of the turbocharger (47) intermediate is limited to a predetermined maximum value.
机译:本发明涉及一种用于机舱(11)飞机的环境控制的方法和设备。处于单个中间压力值的飞机发动机的压缩机进气口(39)连接到中间涡轮增压器(47)的压缩机(48)的入口,该压缩机(48)的出气口连接到入口在空气循环涡轮发动机(15)的一部分中,空气循环涡轮发动机的输出连接至机舱(11),涡轮增压器(47)的涡轮(49)的入口联接至压缩机(48),中间来自机舱(11)的空气,并且输送到涡轮增压器(47)中间的压缩机(48)的空气出口的气压被限制为预定的最大值。

著录项

  • 公开/公告号EP3342709A1

    专利类型

  • 公开/公告日2018-07-04

    原文格式PDF

  • 申请/专利权人 LIEBHERR-AEROSPACE TOULOUSE SAS;

    申请/专利号EP20170209968

  • 发明设计人 LAVERGNE DAVID;ROCCHI JÉRÔME;

    申请日2017-12-22

  • 分类号B64D13/02;B64D13/06;

  • 国家 EP

  • 入库时间 2022-08-21 13:15:10

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