B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/18 (2006.01) B64D 29/02 (2006.01)
Patent
CA 2623792
The invention concerns an engine mounting structure designed to be interposed between an aircraft wing system and said engine, the structure comprising a rigid structure (8) as well as front aerodynamic structure (24) mounted fixedly on said structure (8) via mounting means, the front aerodynamic structure being designed to support fan cowlings and to be interposed between the rigid structure and the wing system. The invention is characterized in that the mounting means comprise at least one connecting rod with adjustable length (32) one end of which is mounted on the structure (8), and the other end of which is mounted on the front aerodynamic structure (24).
La présente invention se rapporte à un dispositif d'accrochage d'un moteur destiné à être interposé entre une voilure d'aéronef et ce moteur, le dispositif comportant une structure rigide (8) ainsi qu'une structure aérodynamique avant (24) montée fixement sur ladite structure (8) par l'intermédiaire de moyens d'accrochage, la structure aérodynamique avant étant destinée à porter des capots de soufflante et à être interposée entre la structure rigide et la voilure. Selon l'invention, les moyens d'accrochage comprennent au moins une bielle de longueur réglable (32) dont une extrémité est montée sur la structure (8), et dont l'autre extrémité est montée sur la structure aérodynamique avant (24).
Combes Stephane
Lafont Laurent
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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