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.

A holding device for a display and/or operating unit for use in an aircraft on an aircraft seat is proposed, with a holding arm and an attachment device and a coupling unit for connecting the display and/or operating unit, wherein one end region of the holding arm is provided on the attachment device so as to be pivotable about an axis of rotation and the coupling unit for pivotably connecting the display and/or operating unit is provided on the opposite end region of the holding arm, and wherein the holding arm can take up a use position and a storage position on the attachment device. According to the invention, a spiral spring unit is arranged between the attachment device and the holding arm is such a manner that a torque is exerted on the holding arm by the spiral spring unit.

Passenger seating arrangements for an airliner or other conveyance including a plurality of individual suites arranged into longitudinal columns. Lateral aisles extending from longitudinal aisles lead to branch aisles that provide access to suites spaced apart from the longitudinal aisles, and each lateral aisle can be shared to provide access to two outboard suites. Suites are arranged to maximize seating density and privacy, and each suite is equipped with premium features and amenities for use by occupants during flight.

A tray for a seat of a passenger vehicle including: (a) a first article that is at least partially transparent to a wavelength or wavelength range within the visible spectrum of electromagnetic radiation comprising a first primary surface; and (b) a first display separated from an external environment by the first article, the first display, when activated, at least partially visible through the first article from the external environment. A seat of a passenger vehicle including a seatback and the tray coupled to the seatback. The tray can be manipulable to, from, and between a stowed position and a deployed position. The first display is activated when the tray is in the deployed position. The tray can include a second display that is activated when the tray is in the stowed position to be viewable by a passenger rearward of the seatback to which the tray is coupled.

The present invention relates to an assembly (1) of seats (2, 3, 2, 3) for airplanes, said assembly (1) comprising at least two rows (4, 4) of pairs of adjacent seats (2, 3; 2, 3), each seat (2; 3; 2; 3) comprising one seatback (5), one sitting portion (6), and an element (7) for the support of the lower limbs, each seat (2; 3; 2; 3) being configured in order to make a reclining movement along a respective recline axis (r.sub.2; r.sub.3; r.sub.2; r.sub.3) between a sitting position, wherein at least said seatback (5) and said sitting portion (6) cooperate in order to form a sitting element, and an extended position, wherein said seatback (5), said sitting portion (6) and said element (7) cooperate in order to form a bed surface, and vice versa, each seat (2; 3; 2; 3) being tilted in respect to the adjacent seat (3; 2; 3; 2) of a first angle (; ) obtained by the intersection of the respective recline axis (r.sub.2, r.sub.3; r.sub.2, r.sub.3) in a convergence point (A; A) arranged rearward said pair of adjacent seats (2, 3; 2, 3), at least a first seat (2; 3) of a first row (4) being separated from the seat (2; 3) of the second row (4) arranged in front to it so that, both when both are in sitting position and when both are in extended position, there is always at least a space (8) between them (2 and 2; 3 and 3) for the passage of a passenger in order to access the adjacent seat (3; 2) to said at least one first seat (2; 3) of said first row (4). The present invention further relates to the arrangement of said assembly (1) of seats (2, 3; 2, 3) within an airplane cabin (100).

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 mounting arm assembly movable between stowed and deployed configurations, includes a pivot arm pivotally engaging an armrest of a seat; a tilt arm engaging the pivot arm; and a mount engaging the tilt arm for supporting a personal electronic device.

A device is for holding two or more monitors at an operator chair. The device comprises an arm arrangement adapted to be shifted between different horizontal poses. The arm arrangement comprises a support structure, a first rocker arm, a second rocker arm and a third rocker arm that are rotatably attached at separate locations of the support structure via a respective first pivot, second pivot and third pivot. The support structure is adapted to be attached to or in vicinity of the operator chair. The arm arrangement further comprises a connection arrangement between the first rocker arm, the second rocker arm and the third rocker arm.

A multifunctional chaise chair for outdoor use enhances smart device usability and user comfort. The chair includes a seating assembly, support system, and an upper cover assembly with a frontal panel strategically positioned parallel to the backrest to hold a smart device, and an overhead panel for shade. This arrangement improves display visibility by reducing bright light reflections while maintaining a natural, comfortable viewing angle. The chair incorporates a solar power system, a wireless communication module for internet and device connectivity, and at least one of a multi-function interface port or wireless power transfer module for data and power delivery. Optional collapsible side panels made of partially light-transmissive, air-permeable material reduce reflections and allow airflow. Additional features include a mist sprayer, speaker assembly, and adjustable seating and device positioning to accommodate users of different heights and preferences.

The invention relates to a transport system (1) intended to be installed on a space launcher (100) comprising: an aircraft (2) which comprises propulsion means configured to propel the aircraft (2) in a direction of flight, and at least one seat (4) intended to receive a passenger which is movable in rotation about an axis (0) perpendicular to the direction of flight of the aircraft (2), an acceleration sensor being installed on each at least one seat (4) to measure the acceleration of each at least one seat (4); a passenger interface for each at least one seat (4) which comprises a screen intended to display images to the passenger installed on said at least one seat (4), the screen being coupled to said at least one seat (4) so to remain fixed relative to said at least one seat (4); a control unit (6) which is connected to the acceleration sensor and to said at least one seat (4), the control unit (6) being configured to calculate a load factor experienced by the passenger installed on the at least one seat (4) from the acceleration of said at least one seat (4), the control unit (6) being configured to monitor the rotation of the at least one seat (4) during the operation of the transport system (1) in order to maintain the position of the seat (4) fixed relative to the load factor experienced by the passenger throughout the flight.