TRIPLE-REDUNDANT AIR DATA SYSTEM ARCHITECTURE
A first air data system for providing first aircraft air data parameter outputs is formed by a first electronics channel of a first multi-function probe (MFP) that is electrically coupled with a first static pressure sensor. A second air data system for providing second aircraft air data parameter o...
Saved in:
Main Authors | , |
---|---|
Format | Patent |
Language | English |
Published |
14.06.2018
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | A first air data system for providing first aircraft air data parameter outputs is formed by a first electronics channel of a first multi-function probe (MFP) 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 of a second MFP 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 of the first MFP that is electrically coupled with a second electronics channel of the first MFP. |
---|---|
Bibliography: | Application Number: US201615374457 |