TRIPLE-REDUNDANT AIR DATA SYSTEM ARCHITECTURE

    公开(公告)号:EP3333577A1

    公开(公告)日:2018-06-13

    申请号:EP17206457.8

    申请日:2017-12-11

    Abstract: A first air data system for providing first aircraft air data parameter outputs is formed by a first electronics channel (28) of a first multi-function probe (MFP) (12A) that is electrically coupled with a first static pressure sensor. A second air data system for providing second aircraft air data parameter outputs is formed by a first electronics channel (30) of a second MFP (12B) that is electrically coupled with a second static pressure sensor. A third air data system for providing third aircraft air data parameter outputs is formed by a second electronics channel (30) of the first MFP (12A) that is electrically coupled with a second electronics channel (30) of the first MFP (12A).

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