Rear fuselage section (2) of an aircraft comprising at least one closed frame (6) constructed as a unitary body, and a horizontal tail plane (23) comprising a box-type central element (19) and two lateral torsion boxes (20), said horizontal tail plane (23) trimmable with respect to a pivot axis (29), characterized in that the horizontal tail plane (23) is mounted at the closed frame (6) and the pivot axis (29) is contained in a horizontal plane (36) below the lowest end (37) of said closed frame (6).
La section de fuselage arrière (2) dun aéronef comprend au moins un cadre fermé (6) construit sous la forme dun corps unitaire, et un plan de queue horizontal (23) comprenant un élément central de type boîte (19) et deux boîtes de torsion latérales (20), ledit plan de queue horizontal (23) étant réglable par rapport à un axe de pivot (29), caractérisé en ce que le plan de queue horizontal (23) est monté au niveau du cadre fermé (6) et laxe de pivotement (29) est contenu dans un plan horizontal (36) au-dessous de lextrémité la plus basse (37) dudit cadre fermé (6).
REAR FUSELAGE SECTION OF AN AIRCRAFT
SECTION DE FUSELAGE ARRIERE D'UN AERONEF
2021-05-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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