B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/26 (2006.01)
Patent
CA 2623758
The invention concerns a method for mounting an aircraft engine on a rigid structure of a strut, comprising a step of fixing, on the structure a locking body (46) of an engine fastener, said locking body being designed to be pressed against a contact surface of the rigid structure oriented towards the front, and fixed on said structure via at least one shear pin (86) passing through first and second primary orifices, the step of fixing the body (46) including the following operations: pre-positioning the engine relative to the strut so as to place the first orifice opposite the second orifice; and introducing a pin guide equipped with a convex centering head through both orifices, such that said pin guide constitutes the shear pin.
L'invention concerne un procédé de montage d'un moteur d'aéronef sur une structure rigide d'un mât, comportant une étape de fixation, sur la structure, d'un corps d'attache (46) d'une attache moteur, ce corps d'attache étant destiné à être plaqué contre une surface de contact de la structure rigide orientée vers l'avant, et fixé sur cette structure par l'intermédiaire d'au moins un pion de cisaillement (68) traversant un premier et un second orifice primaire, l'étape de fixation du corps (46) comprenant les opérations suivantes: - pré-positionnement du moteur par rapport au mât dans le but de mettre le premier orifice en regard du second orifice; et- introduction d'un axe équipé d'une tête bombée de centrage à travers les deux orifices, de sorte que cet axe constitue le pion de cisaillement.
Journade Frederic
Lafont Laurent
Renaud Eric
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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