A cabin pressure assessment system for an aircraft includes a plurality of polling devices within an internal cabin of the aircraft. The plurality of polling devices are associated with passenger seats onboard the aircraft. A cabin pressure assessment control unit is communicatively coupled to the plurality of polling devices. The cabin pressure assessment control unit is configured to receive cabin pressure comfort data from the plurality of polling devices.
Aircraft cabin pressure assessment systems and methods
10.07.2018
Patent
Elektronische Ressource
Englisch
CABIN PRESSURE SENSOR (CPS) SYSTEM FOR PRESSURIZED-CABIN AIRCRAFT AND ASSOCIATED METHODS
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