| 摘要 |
A drive arrangement for an aircraft belt loader having a frame, an electric motor with a releasable mounting ring, a vertical support plate affixed to the frame with a circular opening, the center thereof being elevated above the frame, a flange positioned in the opening and secured to the support plate and releasably secured to the ring, and a planetary reducer with an output housing and a mounting plate, the reducer being driven by the motor; the mounting plate releasably secured to the flange and a drive wheel affixed to the housing.
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