| 摘要 |
An exemplary implementation of an aircraft interior table includes a base unit which includes a storage compartment having laterally projecting ends. A bi-fold table comprised of a table panels is horizontally stowed and supported on the upper surface of the base unit. Thus, in a stowed condition, one of the table panels is folded so as to be sandwiched between the other of the table panels and the upper surface of the base unit. The edge of the other table panel opposite to its hinged edge adjoining both table panels is pivotally connected to the base unit by means of a primary hinge. In use, the table panels may be rotated as a unit about the primary hinge so as to achieve an intermediate fold-out condition. While in such a position, the table will present itself half-sized so as to provide the associated aircraft seat occupant with minimal forward obstruction. From the intermediate fold-out condition, the other of the table panels may then be pivoted so that both table panels are positioned horizontally adjacent to one another. The fully deployed table panels will thus be supported in a cantilevered manner by the primary hinge attached to the base. Reversing such a procedure will fold the table panels and place them in a stowed condition.
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