B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 27/26 (2006.01)
Patent
CA 2658149
The present invention relates to an aircraft engine attachment device comprising a rigid structure and means for attaching the engine to the rigid structure, the attachment means comprising a thrust-reacting device (14) comprising two lateral thrust-reacting link rods (26) each having a rear end (26b) mounted on a balance beam (28) of the device (14) via a mechanical link (44). According to the invention, each link (44) is made using a peg (48) provided on the balance beam and passing through a hole (50) made in the rear end (26b), the peg (48) being arranged in such a way as to run substantially transversely with respect to the attachment device.
La présente invention se rapporte à un dispositif d'accrochage d'un moteur d'aéronef comportant une structure rigide et des moyens d'accrochage du moteur sur la structure rigide, les moyens d'accrochage comportant un dispositif de reprise des efforts de poussée (14) comportant deux bielles latérales de reprise des efforts de poussée (26) présentant chacune une extrémité arrière (26b) montée sur un palonnier (28) du dispositif (14), par l'intermédiaire d'une liaison mécanique (44). Selon l'invention, chaque liaison (44) est réalisée à l'aide d'un pion (48) prévu sur le palonnier et traversant un orifice (50) pratiqué dans l'extrémité arrière (26b), le pion (48) étant agencé de manière à s'étendre sensiblement transversalement par rapport au dispositif d'accrochage.
Beaufort Jacques
Levert Stephane
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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