A method of monitoring a first freewheel interposed between a first drive shaft of a first engine and a rotor. The state of operation of said first freewheel is correct if the first inlet speed of rotation of the first drive shaft lies in a second range of values corresponding to the current stage of operation while the outlet speed of rotation of the rotor lies in a first range of values corresponding to the current stage of operation.
Method of monitoring at least one freewheel of a rotary wing aircraft, and an aircraft
2018-07-10
Patent
Elektronische Ressource
Englisch
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