| 摘要 |
A door assembly for a landing gear of an aircraft. The door assembly comprises a door section that in turn has two panels, moveable between closed and open positions by a positioning section. In one embodiment, the positioning section comprises mounting arms fixed to the panels which are connected by parallel linkages and which move the panels in a rotational path from a closed position aligned with the door opening through a path of rotation to a location spaced laterally of the door opening, with the panels being in proximity with another and these partially overlapping. In another arrangement, the inside surfaces of the panels face one another in the open position, and the panels are hinge mounted to one another.
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