B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/26 (2006.01)
Patent
CA 2700089
The invention relates to a propulsion assembly for an aircraft, that comprises : a turbojet engine (1) including a fan casing (3) and an engine casing (5) ; a pylon for holding said turbojet engine (1); and a device for suspending said turbojet engine under the pylon, that comprises two front suspension connecting rods (9), two rear suspension connecting rods (11), and a thrust acceleration connecting rod (15) extending between the front portion (17) of said engine casing (5) and the pylon in a plane containing the axis (A) of said turbojet engine (1). An additional connecting rod (19) extends between said fan casing (3) and said pylon in a direction substantially parallel to that of the axis (A) of said turbojet engine.
Cet ensemble propulsif pour aéronef comprend : un turboréacteur (1) comportant un carter de soufflante (3) et un carter de moteur (5); un pylône de support de ce turboréacteur (1); et un dispositif de suspension de ce turboréacteur sous ce pylône comprenant deux bielles de suspension avant (9), deux bielles de suspension arrière (11) et une bielle de reprise de poussée (15) s'étendant entre la partie avant (17) dudit carter de moteur (5) et ledit pylône dans un plan comprenant l'axe (A) dudit turboréacteur (1). Une bielle complémentaire (19) s'étend entre ledit carter de soufflante (3) et ledit pylône selon une direction sensiblement parallèle à celle de l'axe (A) dudit turboréacteur.
Aircelle
Norton Rose Or S.e.n.c.r.l. S.r.l./llp
LandOfFree
Ensemble propulsif pour aeronef does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Ensemble propulsif pour aeronef, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Ensemble propulsif pour aeronef will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1595401