Motor wiring structure of electric aircraft
The utility model discloses a motor wiring structure of an electric aircraft, which comprises a stator wire spool, two stator coils are arranged on the stator wire spool, and the two stator coils are arranged front and back. Through mutual cooperation of a rectangular block, a transmission rod, a dr...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The utility model discloses a motor wiring structure of an electric aircraft, which comprises a stator wire spool, two stator coils are arranged on the stator wire spool, and the two stator coils are arranged front and back. Through mutual cooperation of a rectangular block, a transmission rod, a driving bevel gear, a driven bevel gear, a worm, a worm gear, a vertical rod, a winding roller, a rope, movable blocks, a limiting rod and first springs, the adjacent movable blocks can move up and down under the action of the adjacent sliding grooves and the sliding blocks and the cooperation of the two adjacent first springs; according to the wiring terminal protection device, the clamping blocks fixed to the adjacent movable blocks are inserted into the inner cavities of the adjacent clamping grooves, so that the protection cover can be conveniently installed, the wiring terminal can be conveniently protected, the use effect of the device is improved, a telescopic rod, a second spring and an arc-shaped clamping pl |
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