A cabin pressure sensor system (100) for an aircraft including a plurality of air pressure sensors (104) positioned within an aircraft environment, an indication device (106), a central processing unit (CPU) (102) electrically coupled to the plurality of air pressure sensors (104) and the indication device (106), being configured to receive air pressure measurements from each of the first air pressure sensor and the second air pressure sensor, defining received air pressure measurements, identify received air pressure measurements that are below the minimum cabin air pressure limit, defining an anomalous cabin air pressure measurement, and operate the indication device (106) responsive to identifying an anomalous cabin air pressure measurement. The system (100) further includes a power supply device (108) electrically coupled to the CPU, the sensor, and the indication device (106).
CABIN PRESSURE SENSOR (CPS) SYSTEM FOR PRESSURIZED-CABIN AIRCRAFT AND ASSOCIATED METHODS
KABINENDRUCKSENSOR (CPS)-SYSTEM FÜR DRUCKKABINE EINES FLUGZEUGS UND ZUGEHÖRIGE VERFAHREN
SYSTÈME DE CAPTEURS DE PRESSION DE CABINE (CPS) POUR AÉRONEF À CABINE PRESSURISÉE ET PROCÉDÉS ASSOCIÉS
2023-08-30
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
CABIN PRESSURE SENSOR (CPS) SYSTEM FOR PRESSURIZED-CABIN AIRCRAFT AND ASSOCIATED METHODS
European Patent Office | 2021
|Notes on design of pressurized cabin aircraft
Engineering Index Backfile | 1946
|Decompression of pressurized cabin
Engineering Index Backfile | 1963
|