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Differential pressure sensor system, aircraft equipped with a differential pressure sensor system and method for operating a differential pressure sensor system

机译:压差传感器系统,配备有压差传感器系统的飞机以及用于操作压差传感器系统的方法

摘要

A differential pressure sensor system for use in an aircraft comprises a differential pressure sensor for determining a differential pressure between a pressurizable aircraft cabin and an aircraft environment, the differential pressure sensor having a first port connectable to the pressurizable aircraft cabin via a first line and a second port connectable to the aircraft environment via a second line. A shut-off device of the differential pressure sensor system is arranged in the second line which is switchable between an open position in which it opens the second line, such that a pressure prevailing in the aircraft environment acts on the second port of the differential pressure sensor, and a shut-off position in which it closes the second line, such that the second port of the differential pressure sensor is shut off from the pressure prevailing in the aircraft environment.
机译:用于飞机的压差传感器系统包括用于确定可加压的飞机机舱与飞机环境之间的压差的压差传感器,该压差传感器具有可通过第一管线和可加压的飞机机舱连接的第一端口。第二端口可通过第二条线路连接到飞机环境。差压传感器系统的关闭装置布置在第二管线中,该切断装置可在打开位置之间切换,在该断开位置中,该差动装置打开第二管线,从而在飞机环境中普遍存在的压力作用在差压的第二端口上传感器和一个关闭位置,在该位置它关闭第二条管线,从而使差压传感器的第二个端口与飞机环境中存在的压力关闭。

著录项

  • 公开/公告号US10472085B2

    专利类型

  • 公开/公告日2019-11-12

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号US201715597223

  • 申请日2017-05-17

  • 分类号B64D45;B64C25;B64C25/34;B64D13/02;G01L13;G01L19;B64D13/04;

  • 国家 US

  • 入库时间 2022-08-21 11:30:19

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