Aircraft engine assembly

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/26 (2006.01)

Patent

CA 2576095

The invention relates to an aircraft engine assembly (1) comprising a turbojet (2), a pylon (4) and a plurality of engine mounts (6a, 6b, 8) which are disposed between the pylon (4) and the turbojet (2). According to the invention, each of the engine mounts (6a, 6b, 8) is fixed to a turbojet (2) fan case (12).

L'invention se rapporte à un ensemble moteur (1) pour aéronef comprenant un turboréacteur (2) , un mât d'accrochage (4) ainsi qu'une pluralité d'attaches moteur (6a, 6b, 8) interposées entre le mât d'accrochage (4) et le turboréacteur (2) . Selon l'invention, chacune des attaches moteur (6a, 6b, 8) est fixée à un carter de soufflante (12) du turboréacteur (2) .

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