Abstract: An aircraft cabin comprising a credenza and a lounge chair disposed above the credenza is disclosed. The lounge chair is adjustable between a first configuration defining a first seating arrangement and a second configuration defining a second seating arrangement. Also disclosed is a mechanism to facilitate the adjustment of the lounge chair.

Abstract: An apparatus for a vehicle having a carriage and a rotatable insert configured to be moved between a stowed position and an open position in the carriage. The carriage is configured to be mounted within a side-ledge and includes a first carriage panel having a first slot and a second slot. The first slot has an arcuate curve thereto and the second slot is linear. The rotatable insert includes a first insert panel and a compartment. The first insert panel includes first and second protrusions extending therefrom that are configured to respectively engage the first and second slots such that, as the rotatable insert is moved to the open position, the first and second protrusions travel respectively up the first and second slots. The compartment that is hidden when in the stowed position and can carry at least one item when in the open position.

Abstract: An aircraft cabin comprising a credenza and a lounge chair disposed above the credenza is disclosed. The lounge chair is adjustable between a first configuration defining a first seating arrangement and a second configuration defining a second seating arrangement. Also disclosed is a mechanism to facilitate the adjustment of the lounge chair.

Abstract: An aircraft cabin comprising a credenza and a lounge chair disposed above the credenza is disclosed. The lounge chair is adjustable between a first configuration defining a first seating arrangement and a second configuration defining a second seating arrangement. Also disclosed is a mechanism to facilitate the adjustment of the lounge chair.

Abstract: An apparatus for a vehicle having a carriage and a rotatable insert configured to be moved between a stowed position and an open position in the carriage. The carriage is configured to be mounted within a side-ledge and includes a first carriage panel having a first slot and a second slot. The first slot has an arcuate curve thereto and the second slot is linear. The rotatable insert includes a first insert panel and a compartment. The first insert panel includes first and second protrusions extending therefrom that are configured to respectively engage the first and second slots such that, as the rotatable insert is moved to the open position, the first and second protrusions travel respectively up the first and second slots. The compartment that is hidden when in the stowed position and can carry at least one item when in the open position.

Abstract: A system for providing a passenger interface for a passenger in a seat including at least one sensor adapted to generate a signal representative of the position, the configuration, and/or the direction of movement of hand of the passenger; a controller, and a projector for projecting a passenger interface, placement of which is determined based at least on the signal. A method includes receiving a first signal indicative of a position and/or an arm of the passenger; projecting, by a projector, a passenger interface onto a predetermined surface, the passenger interface location on the predetermined surface being based on the first signal, receiving a second signal indicative of the position, configuration, and/or direction of movement of the passenger's hand of with respect to the passenger interface; and adjusting at least one of a passenger controllable feature, and projection of at least one media display by a second projector.

Abstract: An aircraft table configuration includes a first table section and a second table section. The first and second table sections are hingedly connected along a first hinge line so that the second table section is configurable between a deployed, opened position and a folded, closed position. The first table section presents a first angled side and the second table section table presents a second angled side. The first angled side defines a first angle with respect to the first hinge line, and the second angled side defines a second angle with respect to the first hinge line. The first angled side and the second angled side are opposite to one another on either side of the first hinge line, wherein the first and second angled sides are adapted to define an aisle width in the aircraft. The aisle width does not change between the open position and the closed position.

Abstract: An aircraft cabin comprising a credenza and a lounge chair disposed above the credenza is disclosed. The lounge chair is adjustable between a first configuration defining a first seating arrangement and a second configuration defining a second seating arrangement. Also disclosed is a mechanism to facilitate the adjustment of the lounge chair.

Abstract: An aircraft table configuration includes a first table section and a second table section. The first and second table sections are hingedly connected along a first hinge line so that the second table section is configurable between a deployed, opened position and a folded, closed position. The first table section presents a first angled side and the second table section table presents a second angled side. The first angled side defines a first angle with respect to the first hinge line, and the second angled side defines a second angle with respect to the first hinge line. The first angled side and the second angled side are opposite to one another on either side of the first hinge line, wherein the first and second angled sides are adapted to define an aisle width in the aircraft. The aisle width does not change between the open position and the closed position.