An aircraft propulsion assembly has an engine casing, an attachment pylon, a first front engine attachment with a pin and a blade fitted on the pin and fastened in an articulated manner on either side of a median plane to the casing and a second front engine attachment with a central rod in the median plane fastened in an articulated manner to a lower wall of the attachment pylon and to a fitting of the casing. The central rod is generally parallel to a longitudinal axis. In this arrangement, the casing is brought closer to the attachment pylon for a saving in terms of height.
AIRCRAFT PROPULSION ASSEMBLY HAVING AN ENGINE, A PYLON AND MEANS FOR ATTACHING THE ENGINE TO THE PYLON
19.06.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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