The invention relates to a method for modifying the installation configuration of an aircraft (1) and an aircraft (1) comprising an engine (10) housed in an engine compartment (22) and an engine control device (15) adapted to control at least one parameter of the engine (10), in which the engine control device (15) is installed in said engine compartment (22).
AIRCRAFT WITH AN ENGINE CONTROL DEVICE IN THE ENGINE COMPARTMENT AND METHOD TO OBTAIN SUCH AIRCRAFT
FLUGZEUG MIT EINER MOTORSTEUERVORRICHTUNG IM MOTORRAUM UND VERFAHREN ZUR HERSTELLUNG EINES SOLCHEN FLUGZEUGS
AÉRONEF COMPORTANT UN DISPOSITIF DE COMMANDE DE MOTEUR DANS LE COMPARTIMENT MOTEUR ET PROCÉDÉ POUR OBTENIR UN TEL AÉRONEF
2021-08-18
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / H02G INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES , Verlegen oder Installieren elektrischer Kabel oder Leitungen, Verlegen oder Installieren kombinierter optischer und elektrischer Kabel oder Leitungen |
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