The invention relates to a method for synchronising the engines of an airplane, according to an activation logic having a deactivated state, an armed state and an activated state, in which: the switching of the activation logic from the armed state to the activated state is carried out via a first and then a second successive intermediate state; every instance of the activation logic switching from the intermediate state to the activated state involves the following: taking into consideration, on each engine, the activation state of the synchronisation, and exchanging said data between the engines; the switching of the activation logic of one of the engines to the activated state requires that the safety and activation conditions of the other engines are all met; if one of the engines enters the deactivated state, the others do so as well; and, for each engine, the switching of the activation logic from the armed state to the first and then to the second intermediate state takes place automatically when a first portion and then a second portion of the safety and/or activation conditions are met.
PROCÉDÉ DE SYNCHRONISATION DES MOTEURS D'UN AVION A DOUBLE ETAT INTERMEDIAIRE
METHOD FOR SYNCHRONISING THE ENGINES OF AN AIRPLANE WITH DUAL INTERMEDIATE STATE
VERFAHREN ZUR SYNCHRONISIERUNG DER MOTOREN EINES FLUGZEUGS MIT DUALEM ZWISCHENZUSTAND
2018-06-06
Patent
Electronic Resource
French
PROCÉDÉ DE SYNCHRONISATION DES MOTEURS D'UN AVION A DOUBLE ETAT INTERMEDIAIRE
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