| 摘要 |
The invention relates to a connector assembly (1, 100) for connecting a motor to the cable (5,103) of a strut fixing the motor to an aircraft wing. A male part (2, 101) includes 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 the 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. |
