An aircraft landing gear having a male part interlocked with a female part along an interlocking direction is provided. The external contact surface of the male part, when it is observed along the interlocking direction, can be an exclusively convex closed surface having external contact surface portions in the form of rounded lobes that form obstacles to the pivoting of the female part with respect to the male part about the interlocking direction. The aircraft landing gear is suitable for use with an aircraft.
Aircraft landing gear having interlocked male and female parts for transmitting mechanical torque
2025-04-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT LANDING GEAR HAVING INTERLOCKED MALE AND FEMALE PARTS FOR TRANSMITTING MECHANICAL TORQUE
European Patent Office | 2025
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