A four-suite unit positionable in an aircraft cabin to one side of a longitudinal aisle and including first and second suites positioned longitudinally-aligned and facing each other, a shared passageway positioned between foot ends of the first and second suites, third and fourth suites positioned longitudinally-aligned and to one side of the respective first and second suites, a first passageway positioned between a portion of the first suite and a portion of the third suite for accessing the third suite from the shared passageway, and a second passageway positioned between a portion of the second suite and a portion of the fourth suite for accessing the fourth suite from the shared passageway.

A four-suite unit positionable in an aircraft cabin to one side of a longitudinal aisle and including first and second suites positioned longitudinally-aligned and facing each other, a shared passageway positioned between foot ends of the first and second suites, third and fourth suites positioned longitudinally-aligned and to one side of the respective first and second suites, a first passageway positioned between a portion of the first suite and a portion of the third suite for accessing the third suite from the shared passageway, and a second passageway positioned between a portion of the second suite and a portion of the fourth suite for accessing the fourth suite from the shared passageway.

Disclosed is a deployable panel assembly that includes a support plate (101), a front support arm (105) with a first end having at least two pivotable attachments (106, 107) to a first edge of the support plate (101) and a second end having at least two pivotable attachments (108, 109) to a seat shell, and a rear support arm (110) with a first end (111) pivotably attached to a second edge of the support plate (101) and a second end (112) pivotably attached to the seat shell, wherein the support plate is configured to move between a stowed position and a deployed position.

A seating assembly may employ one or more of: a seat stagger, a seat overlap, and a seat angling to offer significant width and comfort gains and reduce the negative impact of width and leg room gains on seating density. With one seat of a pair staggered forward with respect to the other seat each may then be moved laterally and overlap (as seen from the front). The seating positions may be further improved by angling each seat away from their center arm rest area, reducing the encroaching effect of the overlap by pointing the passenger away from the overlap, reducing the visual impact of the staggered seating by pointing the passenger away from the nearest seat ahead, and improving leg room by directing the passenger's legs forward at an angle.

A slave Bluetooth device establishes first and second connections with first and second master Bluetooth devices, respectively, that each operate in a master mode. The slave Bluetooth device operates in a slave mode when communicating through any of the first and second connections. The slave Bluetooth device communicates connection parameter update request packets containing timeout values to the first and second master Bluetooth devices. The slave Bluetooth device alternates during non-overlapping time slots between at least: 1) monitoring the first connection for traffic transmitted by the first master Bluetooth device while not monitoring the second connection; and 2) monitoring the second connection for traffic transmitted by the second master Bluetooth device while not monitoring the first connection; and controls a rate at which the alternating is performed based on the first timeout value and the second timeout value.

A method of operation for a system incorporating a graphical user interface in a mobile computing device for a crew member within a cabin of an aircraft. The method includes displaying a menu for at least one controllable parameter, receiving a selection of the controllable parameter, displaying at least one control for the selected controllable parameter, receiving a control input for the selected controllable parameter, and adjusting the selected controllable parameter consistent with the control input. The controllable parameter include a plurality of controllable parameters selected from a group encompassing light intensity, light color, temperature, and the degree of openness of at least one window shade. A system and executable computer program product also are provided.

A stowable computer workstation (SCW) for a workplace within a vehicle is described, where the workplace has an inner sidewall of the vehicle. The SCW may include a video display mount assembly and a deployment support attached to the video display mount assembly. The deployment support is configured to deploy and stow the video display mount assembly against the inner sidewall and the deployment support is secured to the inner sidewall.

Described is a stowable display apparatus (200) suitable for stowing a display, such as an in-flight entertainment monitor, in a storage module (110) located above a spreader or a seat bottom of a passenger seat (102). The stowable display apparatus can include an arm (228, 236) pivotally coupled to a mounting plate (222) at a pivot point (250) that is located above the spreader or seat bottom and proximate the forward end of the seat (102), thus enabling a display bracket of the arm to pivot upwards and out of an armrest assembly before rotating into a deployed position. The display arm (228, 236) can provide an easy, safe, and low-cost mechanism for stowing and deploying a display. The thin profile of the display arm allows a storage module (110) two inches wide or less to stow both a display and a table surface, each independently deployable and stowable irrespective of the other's position.

A display adaptation system for a vehicle includes a display that is configured to show one or more features. A motion sensor is configured to detect motion of the vehicle. The motion sensor outputs a motion signal indicative of the motion of the vehicle. A motion-compensating control unit is in communication with the display and the motion sensor. The motion-compensating control unit is configured to analyze the motion signal to determine the motion of the vehicle. The motion-compensating control unit is configured to move the feature(s) shown on the display based on the motion of the vehicle.

A system for alerting a passenger is disclosed. The system includes an aircraft seat including a haptic mechanism, the haptic mechanism configured to be selectively activated. The system includes one or more buttons operationally coupled to the haptic mechanism. The one or more buttons are configured to be selectively operated. The one or more buttons are further configured to activate the haptic mechanism based on an operation of at least one of the one or more buttons.