Fairing for a pylon via which a turbine engine is suspended...

Details Fairing for a pylon via which a turbine engine is suspended... Fairing for a pylon via which a turbine engine is suspended...

B - Operations, Transporting

64

D

B64D 27/26 (2006.01) B64D 27/18 (2006.01) B64D 29/06 (2006.01)

Patent

CA 2653067

Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft. According to the invention, the forward attachment (15) of the anterior part (14) of the fairing (7) for the suspension pylon (6) is radially flexible.

Carénage pour mât de suspension d'un turbomoteur à une aile d'aéronef. Selon l'invention, l'attache avant (15) de la pièce antérieure (14) du carénage (7) du mât de suspension (6) est radialement flexible.

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