B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/26 (2006.01) B64D 29/06 (2006.01)
Patent
CA 2735951
This strut (9), designed to support an aircraft turbojet engine, has, on the one hand, a connecting part (11) for connection between the casing (1) of the fan (3) or the casing of the gas generator (5) of the said turbojet engine and a wing of the said aircraft and, on the other hand, a Y-shaped box-section part (19), secured to the said connecting part (11) and designed to form the upper part of the inner fixed structure of the said nacelle.
Ce mât (9), adapté pour supporter un turboréacteur d'aéronef, présente d'une part une partie de liaison (11 ) entre le carter (1) de soufflante (3) ou le carter du générateur de gaz (5) dudit turboréacteur et une aile dudit aéronef, et d'autre part une partie caissonnée en Y (19), solidaire de ladite partie de liaison (11) et adaptée pour former la partie supérieure de la structure interne fixe de ladite nacelle.
Caruel Pierre
Vauchel Guy Bernard
Aircelle
Fasken Martineau Dumoulin Llp
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