2599results about "Seating arrangements" patented technology

A seat for a passenger vehicle is provided that comprises a first sensor for detecting the presence or absence of an occupant in the seat and a second sensor for validating the seat occupancy. The seat further comprises a transmitter for transmitting a signal indicative of valid occupancy of the seat. The first sensor may be a non-contact, capacitive sensor and the second sensor may comprise a near-field communication device for receiving a seat validation code. A seat validation system may be established on a passenger vehicle such as a train, wherein a central controller may report on seat occupancy status for the vehicle.

An aircraft is provided comprising a fuselage and a central monitoring system positioned within the fuselage. A plurality of seating elements is also positioned within said fuselage. Each of the plurality of seating elements includes a plurality of seat options integrated into the seating element and an electronics control system integrated into the seating element. The electronics control system includes a seat processor having logic adapted to monitor an operational status of each of the seat options and communicate the operational status to the central monitoring system via wireless communication.

A seatback holder for a tablet computer including a bracket configured to releasably engage within a seatback pocket and a frame pivotally connected to the bracket configured to hold an installed tablet computer securely therein and pivot relative to the bracket to adjust the viewing angle of the installed tablet computer relative to a seatback.

A passenger cabin of a passenger transport vehicle such as an aircraft includes single passenger seats arranged between an aisle and an outside cabin wall. Each seat is tiltably adjustable between an upright seating configuration and a reclined lying configuration, and is rotatable between a forward-facing orientation facing 0 to 18° relative to the cabin longitudinal axis, and an inwardly-turned orientation facing 50 to 600 relative to the longitudinal axis. The forward-facing orientation is for upright seating during take-off and landing. The inwardly-turned orientation provides additional leg room and sufficient space for the reclined lying configuration. The pitch spacing between seats can be minimized, and total seating capacity is high, while providing substantial space and comfort for each passenger. Screening partitions adjacent to the cabin wall and the aisle provide privacy screening and define a personal space allocated to each seat.

An aircraft seat assembly including at least one electronic component usable by a passenger and a single integrated electronics system which provides signal decoding, signal routing, data management, built in test, and power conversion for each user accessible electronic component which is installed in the seat assembly. The integrated electronics system provides power conversion, signal routing, data management and other electronic requirements for each of the electronic components. The integrated electronics system not only integrates power conversion and signal management responsibilities into one system, but also is integrated into the seat assembly.

A vehicle seating arrangement can comprise a fore-facing lower seating assembly, an aft-facing lower assembly, and an upper seating assembly positioned between the fore-facing and aft-facing lower assemblies. The lower and upper assemblies can be configured to form a 3-seat unit in which a portion of a seat of said fore-facing and aft-facing lower seat assemblies underlaps a portion of an upper seating assembly. At least one of the fore-facing and aft-facing lower assemblies can be angled with respect to the upper seating assembly to shorten the overall linear dimension of the 3-seat unit and provide egress areas for lower passengers to aisle access. A vertical member can be configured to attach to the upper seating assembly and to a ceiling structure to reduce the load on the floor.

The present invention provides an aircraft passenger seat assembly that includes: (a) first and second seats selectively movable between upright and reclined positions and adapted for being positioned beside and at inwardly-facing angles relative to each other; (b) a center console having a relatively wide aft end and a relatively narrow forward end for being positioned between the first and second seats; and (c) the relatively wide aft end of the center console including first and second foot wells therein adapted to permit the feet of a passenger seated in an aft-positioned first or second seat to extend therein when the aft-positioned first or second seat is in the recline position.

A 3-seat seating grouping is presented that includes a center seat configured for vertical translation from a lower position to a raised position when converted from an upright to an inclined mode. The center seat can be disposed between an aft-facing seating assembly and a fore-facing seating assembly, and be configured to overlap both when in a lie-flat position. Non-overlapping footspace can be shared between a center passenger and an aft-facing passenger. When upright, a center seat can be at the same height as a non-translating aft- or fore-facing seat, reducing loads on a seat track during aircraft take-off. Seats within the 3-seat group can be angled or aligned with respect to cabin longitudinal axis. A plurality of 3-seat groups can be combined in various orientations to span a cabin. Groups can be arranged to mirror each other to maximize seating directed to an aisle.

A method of controlling motion of movable components of a powered seat includes, using the controller, monitoring a feedback signal of an actuator during motion of a component. During an acceleration phase of the motion of the component, a reference state of the time-varying motion command is detected and a reference value of the monitored feedback signal is determined as a reference value. A feedback-signal acceptance range is determined using the reference value of the monitored feedback signal. During a steady-state phase of the motion, the motion of the component is terminated if the monitored feedback signal departs the determined feedback-signal acceptance range. A control system for a powered seat of a vehicle is described. A powered seat assembly is described.

A passenger seating arrangement includes a first seat unit, facing in a first direction; a first ottoman having a first support surface positioned to receive the feet of a passenger seated in the first seat unit; a second seat unit facing in a second direction generally opposite to the first direction; and a second ottoman disposed laterally adjacent to the first ottoman and having a second support surface positioned to receive the feet of a passenger seated in the second seat unit.

A system and method for integrating air and ground transportation of passengers and cargo. The system comprises a plurality of universal passenger containers. The system further comprises a plurality of universal cargo containers. An airplane is provided with a hollow fuselage adapted to be loaded with a plurality of passenger and / or cargo containers. A flatbed trailer can be provided to carry a passenger or a cargo container. A tractor vehicle can be provided to transport flatbed trailers between airplanes, locations within the airport, and points of origin and destination outside the airport complex. A system can be provided to load and unload passenger and cargo containers into and out of airplanes at the airport. A system is provided comprised of an airport complex including take-off and landing runways, taxiways, airplane staging areas, apparatus for detection of weapons in passenger and cargo containers, and air terminals with arrival and departure gates and baggage handling conveyors. A system is also provided comprised of remote air terminals at strategic locations a distance from the airport complex.

A system for providing prophylaxis against thrombosis comprises in combination a vehicle and a plurality of inflatable compression sleeves. The vehicle has a pneumatic pressure source for supplying a predetermined flow of pneumatic fluid to a plurality of passenger positions. The pneumatic pressure source has a plurality of leads, which extend to a connection port located in each of the passenger positions. Each of the inflatable compression sleeves has a plurality of inflatable chambers therein. The sleeves are constructed to be engaged to a connection port, thereby providing fluid communication between the pneumatic pressure source and the plurality of chambers. The sleeves may be worn by a passenger to help prevent the occurrence of deep vein thrombosis. Individual sleeves comprise at least two inflatable chambers wherein a second inflatable chamber is subsequent to the inflation of a first inflatable chamber.

A power distribution system having a continuous power bus to supply power and / or data to aircraft passenger seats in a mobile platform. The power distribution system generally includes a bus strip that extends along a length of the passenger cabin and a connector operable to provide a connection between the bus strip and the passenger seats. Power and / or data can be transmitted between the bus strip and the passenger seats, via the connector, at any point along the bus strip, thus eliminating the need to run separate connections between the power and / or data source and each passenger seat.

The present invention provides an aircraft passenger seat assembly that includes: (a) first and second seats selectively movable between upright and reclined positions and adapted for being positioned beside and at inwardly-facing angles relative to each other; (b) a center console having a relatively wide aft end and a relatively narrow forward end for being positioned between the first and second seats; and (c) the relatively wide aft end of the center console including first and second foot wells therein adapted to permit the feet of a passenger seated in an aft-positioned first or second seat to extend therein when the aft-positioned first or second seat is in the recline position.

An adjustable tray table assembly for a vehicle seat including a bi-fold tray table, an adjustment assembly for adjusting the tray table in the fore / aft and lateral directions, a support arm for supporting the tray table and slidably receiving the adjustment assembly, and an attachment arm interconnected with the support arm for attaching the tray table assembly to the vehicle seat. The adjustment assembly includes a guide bracket that slides both within an elongated opening of the support arm and along at least one guide attached to the tray table to provide the adjustability.

A module for an aircraft having a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane. The frame device is adapted for attachment to the fuselage structure of the aircraft at a second location, wherein the second location is not in the floor plane.

A seating arrangement for location at the longitudinal centre line of a commercial passenger vehicle that has a longitudinally extending passenger seating area. The seating arrangement includes a pair of seats disposed alongside and secured to each other. Each seat comprising a backrest portion, and a seat pan portion, wherein the seats face at an acute angle to each other, and wherein the backrest portions of the respective seats are nearest the vertex of the acute angle than the seat pan portions.

A patient transport arrangement is provided in the passenger cabin of an aircraft and includes a patient stretcher, medical supplies and equipment, and a compartment that is variably and adaptably useable as a restroom compartment and as a medical care compartment. The compartment is arranged adjacent to the doorway clearance area in front of the cabin door of the aircraft. The adaptable compartment includes a foldable wall element so that the stretcher can extend at least partially into the compartment during take-off, landing and ground operations of the aircraft while leaving the doorway clearance area unobstructed, and so that the stretcher can be repositioned out of the compartment and into the doorway clearance area during cruise flight so as to allow the compartment to be used as a passenger restroom during the flight. This arrangement makes efficient use of space within the passenger cabin that would otherwise be unused during various phases of flight.

A passenger seat assembly convertible between a two-seat configuration and a three-seat configuration, and including a seat assembly base and first, second and third seats for carrying respective seat bottom and seat back cushions, the first and third seats defining outboard seats and the second seat defining a center seat. First and second armrests are mounted between the first and third outboard seats on opposing sides of the center seat and are moveable between an upright use position and a retracted storage position above the seat bottom of the center seat. A tray table is mounted for movement between a raised retracted position wherein a bottom surface of the tray table defines at least a portion of the seat back of the center seat, and a lowered use position wherein the tray table resides above the seat bottom of the center seat to provide additional seating space and a tray table for the occupants of the outboard seats.

A track fastener assembly for securing a seat or cargo apparatus to a floor track of a vehicle. The assembly includes a base with a longitudinal slot formed therein, and a ramp disposed in its upper surface near the forward end of the slot. A movable slide carrying locking studs runs in the longitudinal slot. A locking rod having a helical groove formed in its outer surface is operatively connected to the base and the slide. Rotation of the locking rod causes the slide to move axially along the longitudinal slot from an installation position near the aft end of the base to a locking position near the forward end of the base. As the slide moves to the locking position, the slide engages the ramp in the base, thereby deflecting the slide with the attached locking studs upwards and clamping the track fastener assembly to the track.

A passenger seat including a seat base for being mounted on a support surface. A seat frame is carried by the seat base, and includes a seat bottom frame member and a seat back frame member is positioned in a fixed angular relation to each other and the seat base. A seat bottom pan is positioned on the seat bottom frame member. A seat back pan is positioned on the seat back frame member. Guide means cooperate with the bottom pan and bottom frame members and the back pan and back frame members, respectively, for unison translational movement of the back pan and the bottom pan between an upright position when the bottom pan is in the aft position and a recline position when the bottom pan is in the forward position.

An aircraft seat assembly including at least one electronic component usable by a passenger and a single integrated electronic system which provides signal decoding, signal routing, data management, built in test, and power conversion for each user accessible electronic component which is installed in the seat assembly. The electronic components generally include at least a video display unit, an audio system, or a telephone. The integrated electronics system provides power conversion, signal routing, data management and other electronic requirements for each of the electronic components. The integrated electronics system not only integrates power conversion and signal management responsibilities into one system, but into such a system that is readily integrated into the seat assembly.

An aircraft passenger seat position control apparatus is provided. The control apparatus includes a plurality of seat actuators operable to adjust the passenger seat to a selected one of a plurality of discrete seat positions and a touch-sensitive control interface having a plurality of touch-responsive sites thereon corresponding to the plurality of discrete seat positions. The control interface communicates with the plurality of seat actuators and is positioned in proximity to the aircraft passenger seat for use by a passenger seated in the passenger seat. The control interface is also adapted to output a signal to the plurality of seat actuators in response to a touch-selected position by the passenger to thereby adjust the position of the aircraft passenger seat to selected one of the plurality of discrete seat positions.

A conductive bus device and method operable to distribute signals throughout a platform. The bus delivers signals to any number of select locations within the platform, such as to seats mounted to a seat track. The bus is mounted beneath a floor of the platform. The signals can be transmitted between the power bus and the passenger seats using a conductor that extends from the passenger seats to the bus through a opening in the seat track. The bus device and method eliminates the need to run separate connections between a signal source and each seat. This device and method significantly reduce the cost, energy, and time necessary to wire each seat individually.

In herringbone seats of the prior art, armrests on the closed angle side form an obstacle for the passengers in the seat in case of a shock, since the latter are generally projected along the axis of the vehicle and thus towards the armrest thus creating a high risk of injury for the passenger in case of a shock. The present invention provides a secure herringbone arrangement for the armrest of a seat i.e. making it possible to reduce the risk of injuries caused by the armrest, in case of a shock. Therefore, the present invention provides to leave a space between the seating part structure and the armrest to enable the passenger on the seat to be projected along the axis of the airplane in case of a shock without hitting the armrest. More precisely, the aim of the invention is a herringbone arrangement for the armrest of a seat wherein the armrest is angularly shifted with respect to the seat, so as to form a free space (33) between the seat and the armrest. The present invention also relates to a seat and a seat assembly provided with such an arrangement.