B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/20 (2006.01) B64C 5/06 (2006.01) B64C 27/02 (2006.01)
Patent
CA 2622151
The invention concerns a turbojet (1) for aircraft, characterized in that it supports at least one tail fin (7), said tail fin being fixed on the strong structure (11) of said turbojet so as to form a single-unit assembly. The turbojet may also support one or more accessory devices required for operating said turbojet. The invention also concerns an aircraft equipped with such a turbojet, and a method for mounting such a turbojet on an aircraft.
L'invention concerne un turboréacteur (1) pour aéronef, caractérisé en ce qu'il supporte au moins une dérive (7), ladite dérive étant fixée sur la structure forte (11) dudit turboréacteur de manière à former un ensemble monobloc. Le turboréacteur peut également supporter un ou plusieurs des dispositifs annexes nécessaires au fonctionnement dudit turboréacteur. L'invention concerne également un aéronef muni d'un tel turboréacteur, et un procédé de montage d'un tel turboréacteur sur un aéronef.
Guering Bernard
Teulou Olivier
Airbus France
Airbus Operations Sas
Bcf Llp
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