152 results about "Airplane passenger" patented technology

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.

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.

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.

A computer implemented method for an aviation system to manage, consistent with specified system business goals, the temporal assignment of airport gates for use by a plurality of aircraft which are to-be-serviced by specified ground resources, including ground personnel, equipment and supplies, so as to deliver and receive specified passengers, their baggage and cargo during a specified time period, based upon specified data pertaining to the aircraft, passengers and ground resources, includes the steps of: (a) collecting and storing the specified data, (b) processing the data to predict the trajectories of the aircraft, wherein these trajectories including the expected gate arrival time, required ground servicing period and projected departure time of each of the aircraft, (c) processing the data to predict the loads imposed on the ground resources and gates associated with the movement of the passengers, equipment and supplies in relation to the arrival and departure of the aircraft, (d) processing the data, trajectories and loads to identify the various possible ways to distribute the ground system resources and assign the gates so as to meet the time constraints of the predicted trajectories and loads, and (e) assigning to each of the plurality of aircraft a gate for use for a prescribed period, with these assignments being made in such a manner as to allow the aviation system to optimally meet its business goals.

A convertible seat to accommodate an aircraft passenger. The seat includes a frame, a sitting portion borne by the frame, a back, and a jointed footrest along the transverse edge of the sitting portion. The seat can change from a so-called seated position in which the back forms an angle with the sitting portion and its base is close to the rear transverse edge of the sitting portion to a so-called lying-down position in which it has a more or less level surface intended to accommodate a passenger in the lying down position. The frame is a fixed frame. At most two of the elements of the whole constituted by the sitting portion, the back, and the footrest form the more or less level surface of the seat in lying-down position. At least one additional berth is provided to cooperate with the sitting portion and / or the back and / or the footrest to form the more or less level surface intended to accommodate a passenger in the lying-down position.

A laptop computer display module (28) for use in a clamshell type laptop computer includes a telescoping rail assembly (100) that enables the display module (28) to be extended upwardly from a keyboard module (24) of the laptop computer when the display module is rotated to an open position. A computer display panel (28) is rotatably mounted to a display support member (120) of the display module adjacent a top margin of the display panel (70) so that the display panel (70) can be manually swung away from the display support member (120) and toward a user of the laptop computer (20). The invention enables the display panel (70) to be positioned at a comfortable viewing angle without blocking access to the keyboard module (24) for typing and is particularly useful in depth-constrained workspaces such as airplane passenger seats, where the display support member (120) must be positioned at an acute angle relative to the keyboard module (24).

A seating arrangement for a cabin of a passenger aircraft that includes 5-abreast passenger accommodation suites, each including a privacy wall and a seat movable between a seating position and a lie-flat bed position, and adapted to be laterally positioned in the aircraft cabin in respective adjacent outboard, middle and inboard positions. Three of the suites are adapted to be positioned in a longitudinally-offset position in relation to each other and defining respective ingress / egress paths to a cabin aisle extending along a longitudinal axis of the aircraft cabin adjacent the third suite. Two of the suites are positioned in a longitudinally-offset position in relation to each other and defining respective ingress / egress paths on the opposite side of the cabin aisle. At least some of the suites define an angular offset relative to the longitudinal axis of the cabin aisle.

A passenger seat of the type having passenger-controllable functions, and including a seat base, a seat frame mounted on the seat base, and a seat back and seat bottom carried by the seat frame. The passenger seat includes at least one passenger-operable function. A function control communication system is carried by the passenger seat for operative communication with a rearward-facing seat back panel of a second passenger seat positioned immediately forward of the passenger seat. Function controls carried on the rearward-facing seat back panel for operative connection with the function control communication system, that may be wireless and remotely or manually operable, for permitting a passenger seated in the passenger seat to control functions of the seat by utilization of the function controls on the seat back panel of the second passenger seat immediately forward of the passenger.

A passenger accommodation unit with deployable bed, including a passenger seat and a passenger bed positioned relative to the seat and adapted for movement between a stowed position wherein the bed is upright and adjacent to the seat, and a deployed position wherein the bed is horizontal for use and overlaps and is supported in part by the seat. The unit includes a credenza positioned adjacent the seat and between the seat and the bed that supports the bed when deployed.

A portable pet carrier which can be folded flat for storage when not in use and which can be moved in a horizontal direction with the pet carrier removably attached to a rollable platform having a unique carrying handle rotatable to be at an angle to the pet carrier to permit the pet carrier to be transported from one horizontal location to another with the pet carrier remaining in a horizontal orientation to facilitate the pet's comfort during transportation. The pet carrier is also small enough and flexible enough to be retained under a passenger seat of an airplane.

An arrangement for installing electric cables in the floor region of an aircraft includes longitudinal guide elements that form cable channels and essentially extend in the longitudinal direction of the aircraft parallel to seat rails that are arranged in the aircraft floor and serve for the mechanical attachment of seat legs. The longitudinal guide elements, which accommodate the data and supply cables to be installed, are not visible to aircraft passengers, but are still readily and easily accessible to the maintenance personnel. The floor plate features an elongate groove-shaped recess extending parallel to the seat rail in the longitudinal direction of the aircraft in the immediate vicinity of one of the two seat rails, wherein an elongate extruded profile is arranged in said recess. The extruded profile features an elongate drawer for transmitting shearing forces and an elongate cable shaft arranged above the drawer and serves for accommodating electric cables.

A premium class passenger suite that includes a main seat positioned in the suite together with separate bed. The bed has a flexible mattress of predetermined dimensions and is movable between a stowed position to one side of the main seat and a deployed position above and separate from the main seat. A drive apparatus is provided for driving the bed between the stowed and deployed positions. The main seat is configured to be movable between a seating position when the bed is stowed, and a stowed position with a lowered seat back when the bed is deployed for use.

A method, system, and device for interfacing with a portable electronic device such as a laptop computer on an airplane, while the laptop computer is stowed in a seat pocket. A keyboard, touch screen display, and electrical interfaces are attached to the back of each display-enabled passenger seat on an airplane, such that the passenger seated behind each enhanced passenger seat may access the keyboard, touch screen display, and electrical interfaces. Display, mouse, and keyboard data interface connections are located in each seat pocket. The electrical interfaces allow a laptop computer user to utilize the keyboard, which is preferably waterproof and embedded in a fold-down tray table attached to the back of the seat in front of the user. The electrical interfaces allow a touch screen display, which is preferably embedded in the back of the seat in front of the user, to regenerate data from the laptop computer.

A child's portable activity pack having folding pouches for amusement or educational items. The pack can be unfolded and its rear pouch placed on a folded down airplane passenger service tray. The back straps can be tightened beneath the tray to securely hold the pack on the tray and a front pouch with an erase board unfolds upwardly and hooks on the service tray catch provided to hold the service tray in its fold-up position. Friction hinges are also provided to releasably hold the front pouch in an upright position when not aboard an aircraft. The portable activity pack has side pouches, which hang down at the sides of the service tray, or other support, for storing the amusement and educational items. The back pouch includes a clear plastic game board and a compartment beneath the game board for game boards and flat items.

An arrangement for controlling the closing and opening operation of an aircraft passenger door includes electromechanical actuators and manual actuators for moving the door and for actuating the various latching and locking mechanisms of the door, a door control unit, as well as an actuator control unit, an operating console, and sensors that sense position and status conditions of the door, all connected to the door control unit, a power supply, and power switches connected serially between the power supply and the actuator control unit. In an operating method, the door control unit controls the actuator control unit, and can switch all of the individual function steps for opening or closing the door selectively between being manually controlled and being electromechanically controlled. While the door can be actuated electrically, in the case of a malfunction or if desired by the operator, it can be operated fully or partly mechanically under a manual control.

A system and method for delivering oxygen to a passenger of an aircraft including a a supply of oxygen, an oral-nasal mask, a controller for adjusting a flow of oxygen from the supply of oxygen to the oral-nasal mask, and a sensor for determining a user's blood oxygen saturation level, wherein the controller adjusts the flow of oxygen based on the sensor's determination of the user's blood oxygen saturation level.

A passenger seat 100 for an aircraft, including a seat bottom frame 210, a backrest frame 220 and a headrest frame 230 that constitute a reclining assembly, which are supported by a spreader 170 and pipes 130 and 132 fastened to a floor by seat track fittings 110, the pipes 130 and 132 passing through left and right legs 120. A direct-acting-type damper 300 is attached to the backrest frame 230, and an extension member 400 is attached to the headrest frame 230, whereby a structural design is provided in which the reclining assembly, the direct-acting-type damper and the extension member can be easily replaced.

A footrest for airplane passengers includes a platform and a number of supporting legs, at least some of which contain springs or resilient members so that when the legs are deployed the passenger can exercise his feet and legs by pressing down on the platform. The legs can be folded or otherwise collapsed against the platform when the device is not in use.

An in-arm monitor seat. In one embodiment, the device comprises an aircraft passenger monitor apparatus that includes a seat assembly having an armrest and a monitor presenter. The monitor presenter may include a lift latch and a rotational dampener that is configured to present a monitor from the armrest. The result is a device, system and method that provides an improved monitor presentation that is convenient, efficient and safe for the user, particularly when used in the armrest of an aircraft passenger seat.

In a door closing procedure, an aircraft passenger door is pivoted from an open position to a pivoted-in position, shifted to a closed position, locked into a locked condition, and then secured into a secured locked condition. A control method and arrangement for controlling the closing procedure includes sensors that respectively each sense the completion of a respective allocated one of the steps of the closing procedure, and then responsively initiate the next following step of the procedure. The closing procedure is carried out in an automatic sequential step-wise manner using a simple robust arrangement, without requiring a computer control.

An arrangement for controlling the closing and opening operation of an aircraft passenger door includes electromechanical actuators and manual actuators for moving the door and for actuating the various latching and locking mechanisms of the door, a door control unit, as well as an actuator control unit, an operating console, and sensors that sense position and status conditions of the door, all connected to the door control unit, a power supply, and power switches connected serially between the power supply and the actuator control unit. In an operating method, the door control unit controls the actuator control unit, and can switch all of the individual function steps for opening or closing the door selectively between being manually controlled and being electromechanically controlled. While the door can be actuated electrically, in the case of a malfunction or if desired by the operator, it can be operated fully or partly mechanically under a manual control.

The present invention relates to an airplane passenger bridge or airplane passenger gangway ladder with a transition part baseboard (30), wherein, the airplane passenger bridge or airplane passenger gangway ladder is provided with a vestibule diaphragm (1) straddled on the transition part baseboard, especially a U-shaped vestibule diaphragm, wherein, the clear height between the transition part baseboard (30) and the ceiling of the vestibule diaphragm (1) is changeable.

The invention discloses an airplane gravity center automatic regulation system, which comprises a center display control sub system and an antifreezing solution balancing sub system connected with the center display control sub system, wherein the center display control sub system comprises a control cabinet arranged in an airplane passenger cabin and a gravity center display touch screen arranged in a cab; an integral work station, a PLC (programmable logic controller) and an AD (analog-to-digital) conversion module are arranged in the control cabinet; the output end of the PLC is connected with the AD conversion module and is then connected with the integral work station. The invention also discloses a regulation method of the airplane gravity center automatic regulation system. The problem of large airplane gravity center position change range in the airplane flying process in the prior art is solved.

A ventilated seat assembly such as an aircraft passenger seat including a cushion assembly supported by a structural element, a plurality of Venturi tubes positioned to direct a flow of air through the cushion assembly, an air compressor supplying compressed air, a manifold assembly coupled in fluid communication with the air compressor, a conduit network fluidly coupling the manifold assembly with the plurality of Venturi tubes, and a controller for activating the air compressor and actuating the manifold assembly. Supplying a small volume of pressurized air to the Venturi tubes induces a larger flow of ambient air and a multiplied air effect to ventilate the passenger seat.

An aircraft passenger seat swivel assembly for an aircraft seating unit that includes a pair of transversely spaced-apart base rails, each including fore and aft fittings for connecting the base rails to an aircraft deck. The base rails define a transversely-extending horizontal plane extending between the pair of base rails. A swivel assembly is mounted between the pair of base rails in the laterally-extending horizontal plane. The swivel assembly provides a low profile seat with a spar that forms a part of the swivel assembly and transfers loads from the seat efficiently to the aircraft deck. A slide assembly enables the seat occupant to slide the seat fore-and-aft and side-to-side independent of the rotation of the seat on the swivel.

A passenger seat with increased knee space for an aft-seated passenger, including a seat base for being attached to a supporting deck and at least one seat frame including a seat back and seat bottom carried by the seat base. At least one arm rest assembly is carried by the seat frame and including an arm rest mounted for pivotal movement about a pivot member between a use position with an upper support surface in a horizontal position for supporting a forearm of a passenger seated in the seat, and a stowed position wherein the upper support surface of the arm rest is perpendicular to the use position. The arm rest pivot member is mounted on the seat frame at a point forward of a plane defined by the seat back carried by the seat and above a point defined by the seat bottom for allowing the knee of an aft-seated passenger to occupy space behind the pivot member of the arm rest.

The invention provides a composite material explosion-proof box which comprises an inner box, an outer box and a parcel bag, wherein the inner box is a drawer-shaped structure; the outer box is a drawer cabinet-shaped structure; and the parcel bag is a flexible cylindrical structure. When the composite material explosion-proof box is in a carried transportation state, the parcel bag is folded andthen accommodated in the inner box, and the inner box is accommodated in the outer box so as to obtain good portable mobility; and when the composite material explosion-proof box is in a stored transportation state, a suspected explosive is accommodated in the inner box, the inner box is accommodated in the outer box, and the outer box is accommodated in the parcel bag so as to obtain omnibearingprotection. Compared with the prior art, the invention provides the composite material explosion-proof box which has the advantages of small size, light weight, all-sided protection and no secondary killing and is suitable for occasions with limited spaces, such as airplane passenger cabins, motor train carriages, offices, and the like.