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
2018-07-10
Patent
Electronic Resource
English
CABIN PRESSURE SENSOR (CPS) SYSTEM FOR PRESSURIZED-CABIN AIRCRAFT AND ASSOCIATED METHODS
European Patent Office | 2023
|Cabin Pressure Control Systems for General Aviation Aircraft
SAE Technical Papers | 1980
|