An airborne platform includes a body and a sensor device. The body includes a first material having a first flexibility. The sensor device is positioned inside the body, and includes an electric conductor. The electric conductor includes a second material that has a second flexibility that is less than the first flexibility. The sensor device is configured to output an output signal indicating whether the sensor device has undergone mechanical failure in response to a load applied to the sensor device that is greater than a load threshold.
Systems and methods for conductive aircraft sensors
2021-03-16
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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