System for connecting a crossbar to an aircraft engine pylon

Details System for connecting a crossbar to an aircraft engine pylon System for connecting a crossbar to an aircraft engine pylon

B - Operations, Transporting

64

D

B64D 27/26 (2006.01)

Patent

CA 2621845

The invention relates to a system (33) for connecting a crossbar to the rigid structure of an aircraft engine pylon, comprising an axle system (32) which is mounted to slide in a first passage (38) in a fitting (34) such that it can move along a first longitudinal axis in a first direction from a normal extracted position to a retracted position in which it is retracted into the fitting, and vice versa. The inventive system also comprises an axle extension member (60) which is supported by the axle system (32) and which can be moved in parallel with the longitudinal axis in a second direction from a normal retracted position to an extracted position in which it is solidly connected to the system (32) and projects out in relation to same, and vice versa.

L'invention concerne un agencement (33) adapté pour raccorder un palonnier à une structure rigide d'un mât d'accrochage de moteur d'aéronef, comprenant un système d'axe (32) monté coulissant dans un premier passage (38) d'une ferrure (34) de façon à permettre un déplacement de celui-ci selon un premier axe longitudinal, dans un premier sens d'une position normale extraite à une position de retrait dans laquelle il est escamoté dans cette même ferrure, et inversement. De plus, l'agencement comporte un organe d'extension d'axe (60) porté par le système (32) et capable d'être déplacé parallèlement à l'axe longitudinal, dans un second sens d'une position normale de retrait à une position extraite dans laquelle il est solidaire du système (32) et en saillie par rapport à celui-ci, et inversement.

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