Loosening tiller aircraft nose mechanism
The utility model provides a loosening tiller aircraft nose mechanism, the threading mechanism comprises an installation plate, the articulated slab, it is still including articulated seat, wherein, the articulated slab is horizontal installation's H shape, one of which end yoke arm is articula...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The utility model provides a loosening tiller aircraft nose mechanism, the threading mechanism comprises an installation plate, the articulated slab, it is still including articulated seat, wherein, the articulated slab is horizontal installation's H shape, one of which end yoke arm is articulated bottom the mounting panel, the other end is articulated with articulated foot stall portion, articulated seat is the U -shaped, its cell body is located mounting panel one side, articulated seat both sides lateral wall bottom is articulated with corresponding articulated slab yoke respectively, eacharticulated first cylinder of articulated seat both sides lateral wall top, article two, first cylinder is articulated mutually with mounting panel top both ends respectively, be equipped with the armthat loosens the soil in the articulated seat cell body, the arm upper portion of loosening the soil articulates with second cylinder one end, and the second cylinder other end articulates at the mounting panel middle part, a |
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