Abstract: 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.

Abstract: Aircraft seats are provided which may be convertible between a seating condition and a bedding condition. According to exemplary embodiments, aircraft seats comprise a seat bottom, a seat back, and a pair of arm rests positioned laterally with respect to the seat bottom, the seat back being mounted to the seat bottom for pivotal movements between an upright position (wherein the seat back extends vertically upwardly relative to the seat bottom) and a reclined position (wherein the seat back extends substantially horizontally relative to the seat bottom), and each of arm rests being coupled to the seat back and the seat bottom so as to be moveable between raised and lowered positions in response to the seat back being pivoted from the upright position to the reclined position, respectively.

Abstract: Aircraft seats are provided which may be convertible between a seating condition and a bedding condition. According to exemplary embodiments, aircraft seats comprise a seat bottom, a seat back, and a pair of arm rests positioned laterally with respect to the seat bottom, the seat back being mounted to the seat bottom for pivotal movements between an upright position (wherein the seat back extends vertically upwardly relative to the seat bottom) and a reclined position (wherein the seat back extends substantially horizontally relative to the seat bottom), and each of arm rests being coupled to the seat back and the seat bottom so as to be moveable between raised and lowered positions in response to the seat back being pivoted from the upright position to the reclined position, respectively.

Abstract: 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.