B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 27/18 (2006.01)
Patent
CA 2608940
The invention relates to an aircraft jet engine pylon suspension attachment comprising a rigid structure (10) provided with a central longitudinal caisson (22). According to said invention, the rigid structure also comprises two side caissons (24a, 24b) fixed to the front part of the central caisson (22), the pylon is provided with first (6a) and second (6b) front engine fasteners which are constructed in such a way that they pick up loads produced in the longitudinal direction (X) of the pylon, wherein said first and second fasteners are connected to the two side caissons, respectively.
L'invention se rapporte à un mât d'accrochage de turboréacteur pour aéronef, le mât disposant d'une structure rigide (10) comportant un caisson central longitudinal (22). Selon l'invention, la structure rigide comprend en outre deux caissons latéraux (24a, 24b) solidaires d'une partie avant dudit caisson central (22), le mât comportant également une première (6a) et une seconde attache moteur avant (6b) conçues de manière à reprendre des efforts s'exerçant selon une direction longitudinale (X) du mât, ces première et seconde attaches étant respectivement agencées sur les deux caissons latéraux.
Chartier David
Diochon Lionel
Petrissans Isabelle
Sarrato Michael
Airbus France
Chartier David
Diochon Lionel
Goudreau Gage Dubuc
Petrissans Isabelle
LandOfFree
Turbojet suspension pylon for aircraft does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Turbojet suspension pylon for aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbojet suspension pylon for aircraft will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-2071165