A pressure control system includes a first sensor, and a second sensor which is dis-similar to the first sensor, where the second sensor generates a same processed data as the first sensor does, but in a way different from the first sensor does. A receiving unit is connected to the first sensor and the second sensor by a wireless connection to receive the processed data from the first sensor and the second sensor. In addition, the receiving unit is connected to the first sensor by a second connection different from the wireless connection to receive the processed data from the first sensor. Additional receiving units are connected to the first sensor and the second sensor by the wireless connection to receive the processed data.
Wireless aircraft cabin pressure control system utilizing smart pressure sensors
2018-10-23
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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