| 摘要 |
The arrangement of a rotary apparatus for aircraft landing gears comprises, disposed in an aircraft wheel axle a modular assembly in one unit comprising a stator and a rotor which is mounted in the stator by two rolling bearings, the stator and the rotor being respectively divided into two stator parts and two rotor parts forming a genetachometer and an electromagnetic coupling of the rotating transformer type for sensors carried by the wheel.
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