Aircraft connector assembly

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/18 (2006.01) H01R 11/12 (2006.01) H01R 13/533 (2006.01)

Patent

CA 2585480

The invention relates to a connector assembly (1, 100) for connecting a motor to the cable (5, 103) of a strut fixing said motor to an aircraft wing. A male part (2, 101) comprises pins (7, 107) and female part (3, 102) lugs (10, 108). In an embodiment, the pins extend radially around the axis (A) of a cable (5) provided with said pins. In another embodiment, the pins extend in a parallel position to the axis (A') of the cable (103) provided therewith and in a perpendicular direction with the cable provided therewith.

L'invention concerne un ensemble connecteur (1, 100) apte à établir une connexion entre un moteur et un câble (5, 103) d'un mât solidarisant ledit moteur à une aile d'un aéronef. Une partie mâle (2, 101) porte des picots (7, 107), et une partie femelle (3, 102) porte des cosses (10, 108). Dans un exemple de réalisation, les picots s'étendent radialement par rapport à un axe (A) d'un câble (5) portant lesdits picots. Dans un autre exemple, les picots s'étendent parallèlement à un axe (A') d'un câble (103) portant lesdits picots, les cosses s'étendant perpendiculairement par rapport à un câble portant lesdites cosses.

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