An airplane off ground advisory system employs at least one position sensor (218a, 218b) attached for detection of an extended condition and a compressed condition of a main landing gear (MLG, 12a, 12b). A control system (200) receives an input from the position sensor (218a, 218b). The control system (200) records a toggling of the input from an extended to a compressed to an extended condition and providing an output. At least one indicator (222a, 222b) is coupled to the control system (200) to be activated by the output.
Airplane off ground advisory system
Flugzeugabhebewarnsystem
Système de conseil hors sol d'un avion
06.09.2017
Patent
Elektronische Ressource
Englisch
PERFORMANCE STANDARD FOR AIRPLANE GROUND ICE DETECTION SYSTEM, AIRPLANE/GROUND BASED
SAE Technical Papers | 1996
Airplane ground power interface device and airplane ground power supply method
Europäisches Patentamt | 2023
|