Coupling device of a motorized wheel of aircraft landing gear
A technology of aircraft and landing gear, applied in landing gear, wheels, aircraft parts, etc., can solve problems such as inability to transmit torque, achieve good torque transmission, optimize weight, and optimize length
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[0029] Referring to the drawings, a strut 1 of an aircraft (not shown) landing gear (not shown in detail) carries at its end an axle 2 on which is mounted a rim 3, the tire of which is not shown.
[0030] A wheel motor assembly including an electric motor 4 and a speed reducer device 5 is installed on the wheel shaft 2 . As a variant, the electric motor 4 can be a hydraulic motor.
[0031] The speed reducer device 5 will not be described in detail. It may be of the usual type known to those skilled in the art. It can also be of the type with an oscillating member as described in patent application EP-2 527 249 . The speed reducer device 5 has an output gear 6 which can be driven to rotate about the axle 2 when the electric motor 4 rotates.
[0032] The output gear 6 is coupled to the rim 3 via a coupling device 7 .
[0033] The coupling device 7 is a preferably metallic part, which has a star shape in plan. This metal part comprises a central part or hub 8 and a number of...
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