Frame assembly for a rear section of an aircraft, comprising at least one frame (2) having a plane of symmetry (4), wherein the frame assembly also comprises at least one supporting element (3) having two ends (3'), wherein each one of the ends (3') is attached to said at least one frame (2) at different sides of the plane of symmetry (4).It permits a more effective transfer of loads coming from the vertical tail plane of the aircraft to the fuselage.
FRAME ASSEMBLY FOR A REAR SECTION OF AN AIRCRAFT AND REAR SECTION OF AN AIRCRAFT COMPRISING SAID FRAME ASSEMBLY
RAHMENANORDNUNG FÜR EIN HECKTEIL EINES FLUGZEUGS UND HECKTEIL EINES FLUGZEUGS MIT BESAGTER RAHMENANORDNUNG
ENSEMBLE DE CADRE POUR UNE SECTION ARRIÈRE D'UN AÉRONEF ET SECTION ARRIÈRE D'UN AÉRONEF COMPRENANT LEDIT ENSEMBLE DE CADRE
2024-01-03
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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