962results about "Aircraft crew accommodation" patented technology

A structural shroud for a passenger seat assembly includes a hollow body having a first end, a second end opposite from the first end, and a central cavity between the first end and the second end. In certain embodiments, the structural shroud may include a magnesium alloy and / or an aluminum alloy, and may be formed via casting, forging, and / or additive manufacturing, among others. In some embodiments, a base frame assembly for a passenger seat assembly includes a monolithic base frame having a first leg portion and a first tube portion integrally formed with the first leg portion.

An aircraft includes a flight deck including a flight deck door configured to be moved between an open position and a closed position, a first monument, second monument, and a secondary barrier door moveably secured between the first monument and the second monument. The secondary barrier door is configured to fold into a stowed position in which a path to the flight deck is open, and unfold into a deployed position in which the path to the flight deck is closed.

An electrically operated folding table arrangement (1) for a vehicle, in particular a motor vehicle, comprises a base support (2), a support arm arrangement (3) coupled to the base support (2), which has a support arm (6) pivotally mounted about a first pivot axis (A), and a tabletop arrangement (4) coupled to the support arm (3), which is pivotable relative to the support arm (3) about a second pivot axis (B). The tabletop arrangement (4) has a retaining arm (7) pivotally connected to the support arm (6) and a tabletop (8) which is rotatably mounted on the retaining arm (7) about a pivot axis (C). Each pivot axis (A, B) is assigned a drive unit (11, 13) with a motor unit (12, 14') for driving and controlling the respective pivoting movement about the respective pivot axis (A, B). Another motor-assisted drive device (16) can be provided for driving and controlling the rotational movement of the table top (8) about the axis of rotation (C).

Provided is a vehicle seat having a variable cushion length. The vehicle seat includes: a front panel of metal arranged on a front-end side of a seat cushion to form a frame of the seat cushion; a sliding device allowing a movable portion to be displaceable and including a sliding member of resin displaceable relative to the front panel in seat front-rear directions; and a bracket of metal that is coupled to the front panel in a manner displaceable relative to the front panel in the seat front-rear directions and that is displaced integrally with the sliding member, the bracket transmitting a load acting on the movable portion to the front panel.

A structural shroud assembly for a passenger seat includes a structural shroud having a first end, a second end opposite from the first end, and a central cavity between the first end and the second end. An armrest pivot may be supported at the first end of the structural shroud. In some cases, the structural shroud may be an armrest. In other cases, the structural shroud is an upper spreader for the passenger seat configured to support a seat back of the passenger seat, and a lower spreader configured to receive at least one seat beam tube is attached to the upper spreader.

A partition including, but not limited to, a first body comprising a planar, foldable material. The partition further comprises a plurality of flat substrates resistant to folding. The partition further comprising an adhesive. The substrates are adhered to the first body by the adhesive and arranged in a repeating pattern that defines a plurality of columns and rows. Each column and each row is spaced apart from its neighbor, thus defining longitudinal gaps between the columns and lateral gaps between the rows. The first body folds laterally along the longitudinal gaps in an accordion-like manner and contemporaneously folds longitudinally along the lateral gaps in an accordion-like manner. The partition contracts both laterally and longitudinally when first body contemporaneously folds laterally and longitudinally. The partition extends both laterally and longitudinally when the first body contemporaneously unfolds laterally and longitudinally.

Disclosed is one example of an easy chair capable of inhibiting links from being deformed and damaged when a large load acts on a cushion frame. A posture-changing mechanism of the easy chair includes a first link, a second link, and a male threaded rod, and these form a truss structure. Thus, in principle, no large bending moment is generated in the first link, the second link, and the male threaded rod. This posture-changing mechanism makes it possible to inhibit the first link, the second link, and the male threaded rod from being deformed and damaged by a bending moment when a large load acts on the cushion frame.

A payload including a housing provided with one or more toothed guides or with one or more docking mechanisms, each of which is configured to detachably toothedly interact with an unmanned aircraft apparatus being docked so as to enable the movement of said docked unmanned aircraft apparatus with respect to the housing of the payload, wherein the housing of the payload is further configured to detachably toothedly interact with yet another (other) unmanned aircraft apparatus so as to enable the action of said yet another unmanned aircraft apparatus onto said docked unmanned aircraft apparatus for withdrawal of the latter from interaction with the housing of the payload. Furthermore, embodiments of an air transport system include two or more unmanned aircraft apparatuses and one of the payload.

A docking station for storing a handset. A storage tray has a first recessed area for storing the handset and a second recessed area for a passenger to grip a top surface of the stored handset. The docking station includes a second latch extended into the second recessed area to engage an indent in the bottom surface of the handset. The docking station includes a first latch extended into the second recessed area to engage an indent located in the front surface of the handset. Depression of a release actuator retracts the first latch to release the top surface of the handset. The release actuator extends through an opening in the first recessed area, which has a length sufficient to allow a finger to actuate the release actuator and grip the top surface of the remote control handset while the remote control handset is stored in the storage tray.

A structure system for installation into a fuselage structure in an interior of an aircraft is proposed, the system comprising at least one first carrier element, at least one second carrier element, at least one elongate frame element having a first end and a second end, at least one first attachment device for attaching the first carrier element to the fuselage structure or to an element coupled with the fuselage structure, at least one first coupling device mounted to the first end for coupling the first carrier element to the at least one frame element, and at least one second coupling device mounted to the second end for coupling the second carrier element to the at least one frame element, wherein the at least one frame element is adapted for holding at least one component to be installed in the interior, wherein the at least one first carrier element is designed for coupling with the at least one first coupling device, wherein the at least one second carrier element is designed for coupling with the at least one second coupling device, and wherein one of the at least one first coupling device and the at least one second coupling device is adapted to snap into the respective carrier element, to be moved relative to the respective end of the frame element and to be arrested in a desired relative position thereto.

A seat for a vehicle includes a frame. The frame includes a headrest portion. The seat for a vehicle also includes an energy absorption spacer coupled to the frame; a seat garnish positioned over the energy absorption spacer and the frame; and a seat trim cover. The seat trim cover has a first portion and a second portion. The first portion of the seat trim cover is coupled to the headrest portion, and the second portion of the seat trim cover extends between the energy absorption spacer and the seat garnish.

Described is a passenger seat having a seat member moveable between a stowed position and a deployed position and at least one actuator coupled to at least one portion of the seat member, wherein the at least one actuator is activable without direct contact with a passenger's hand to change a lock state of the seat member, and wherein an unlocked state of the seat member permits movement of the seat member between the stowed position and the deployed position.

Systems and methods are provided for a transportation vehicle. A system includes a power delivery component comprising a power delivery port and a power meter component to measure a power delivery component voltage received at the power delivery component via a cable, and a seat box connected to the power delivery component via the cable and configured to provide a supply voltage to the power delivery component via the cable. The seat box comprises a DC-to-DC converter to convert an initial DC voltage to a seat box DC voltage, a voltage compensation component to change the seat box DC voltage to the supply voltage, and a microcontroller configured to receive the power delivery component voltage from the power meter component, determine a voltage drop across the cable based on the power delivery component voltage, and control the voltage compensation component to adjust the supply voltage based on the voltage drop.

The invention provides an aircraft passenger accommodation unit (1000) comprising a seat (100), a shell (110) defining an opening (120), and a door (130). The door (130) is translatable along a first path across the opening (120) between a closed position in which passenger egress through the opening (120) is at least partially blocked, and an open position which allows passenger access between a seat (100) and an aisle (300). The door (130) is translatable in a second direction that is transverse to the first direction, between a first configuration and a second configuration. In the first configuration, the door (130) is translatable across the opening (120) along the first path, and when the door (130) is in the second configuration, the door (130) is translatable across the opening (120) along a second path. The invention also provides a door arrangement and a method of using a door.

A cushion frame comprises first and second side frames and a coupling member coupling rear end portions of the first and second side frames. Each of the first and second side frames has a fixation portion at a corresponding rear end portion. The first side frame comprises first and second bead portions in the rear end portion thereof. In the first side frame, a hypothetical ridge line of the first bead portion substantially coincides with an imaginary line extending from the coupling member to the fixation portion. An angle between the hypothetical ridge line of the first bead portion and a hypothetical ridge line of the second bead portion is equal to or less than a preset angle.

The invention relates to a push / pull rod (10) comprising at least one first fastening device (12) with a coupling element (12a) and a shank (12b) which is arranged on it, at least one first connection piece (18), wherein the first fastening device (12) is connected to the first connection piece (18) such that it can be rotated via a threaded arrangement (30) in order to change the length of the push / pull rod (10), a holding device with first and second holding elements interact, and are pressed against one another by means of a spring element (28), wherein the first holding element of the holding device is connected fixedly to the first connection piece (18) for conjoint rotation, and the second holding element is arranged fixedly on the first fastening device (12) for conjoint rotation.

An in-flight risk management system includes an eye sensor, a seat sensor, and one or more in-flight risk management computers that perform operations including: obtaining history information for a flight crew member, obtaining flight information associated with a flight on which the flight crew member will be present, determining, based on the history information and the flight information, a predicted fatigue profile for the flight crew member, determining, based on the predicted fatigue profile for the crew member, one or more fatigue indicator profiles for the flight crew member, obtaining, from at least one of the eye sensor or seat sensor, one or more measured fatigue indicator values associated with the flight crew member, generating, based on the one or more measured fatigue indicator values, one or more updated fatigue indicator profiles, and generating, based on the one or more updated fatigue indicator profiles, an updated predicted fatigue profile.

An aircraft is disclosed here. An embodiment of the aircraft includes a cabin having a cabin ceiling, a display element arranged on the cabin ceiling and oriented to present visual content to an occupant of the cabin, a source of aircraft status data that provides aircraft status data corresponding to current operating status of the aircraft, and at least one video processor coupled to the source of aircraft status data. The video processor is configured to render image data corresponding to an adaptive virtual representation of the sky, wherein the image data is rendered based on at least some of the aircraft status data. The display element is coupled to the at least one video processor to receive the rendered image data, and is configured to display the adaptive virtual representation of the sky based on the received image data.

Methods, apparatuses, and systems for mechanically releasing a predetermined amount of supplemental oxygen to a user via a mechanical initiator are disclosed with the release of the amount of supplemental oxygen based on and in response to the combined factors of a user's determined oxygen consumption based on sensing a user's inhalation combined with determining the ambient pressure in the area of the user.

A method for providing data connectivity for a passenger in a commercial passenger vehicle is provided. The method comprises: receiving, by a server onboard a commercial passenger vehicle, one or more data connectivity requests from one or more passenger electronic devices (PEDs) associated with one or more passengers; obtaining passenger information associated with the one or more passengers; performing, based on the passenger information, an authenticated communication based on the passenger information with one or more service provider candidates according to an order that defines priorities of the one or more service provider candidates such that the authenticated communication with a second service provider candidate is performed after it is determined that a first service provider candidate is unable to meet one or more constraints that are predetermined for providing wireless connection services for a PED associated with a particular passenger; establishing, based on the authenticated communication, data connectivity for the PED associated with the particular passenger.

A holding system for a wheelchair in an aircraft is proposed, including a plate-shaped base unit having first fastening elements at an underside configured to be connected to complementarily shaped second fastening elements in the form of seat rails on a floor or surrounding structure in the aircraft for fastening the base unit, a front holding unit and a rear holding unit arranged on an upper side of the base unit at a distance from each other and defining therebetween a placement area for a wheelchair. The front holding unit and the rear holding unit are configured to form a releasable form-fit connection with the wheelchair disposed on the placement area so that the wheelchair is braced between the front holding unit and the rear holding unit. The holding system is configured to fix the wheelchair stationarily to the floor during operation of the aircraft.

A system and a method include a wand assembly including a sanitizing head having an ultraviolet (UV) lamp configured to emit UV light to sanitize a surface of a component. The wand assembly further includes a first monitored member. The system also includes a second monitored member. A verification control unit is in communication with the first monitored member and the second monitored member. The verification control unit is configured to detect a speed of the wand assembly based on a comparison of the first monitored member in relation to the second monitored member.

The invention discloses an automatic braking device and method for an aviation dining car, and is applied to the technical field of aviation dining car braking. A plurality of brake trundle assemblies are evenly and fixedly connected to the bottom of the aviation dining car, and a brake handle assembly used for controlling the brake trundle assemblies to be unlocked is fixedly connected to the top of the aviation dining car. The brake trundle assembly comprises an installation base fixedly connected to the aviation dining car in a locked mode and a wheel fork rotationally connected to the installation base in the horizontal direction, the wheel fork is rotationally connected with a locking disc and a wheel coaxially and fixedly connected to the locking disc, and the wheel fork is rotationally connected with a clamping block. An unlocking assembly is slidably connected to the wheel fork in the vertical direction, and the unlocking assembly is rigidly connected with the brake handle assembly; the automatic locking device has the technical effects that automatic locking can be realized, the safety performance is improved, and the use cost is reduced.

A system includes a collecting unit for collecting a current oxygen pressure value of the oxygen bottles, an estimating unit for estimating an average degradation model, an adapting unit for adapting the average degradation model, a generating unit for generating several future degradation scenarios, an estimating unit for estimating, for each of the future degradation scenarios, a remaining useful lifetime, and for generating a remaining useful lifetimes probability distribution, a transmitting unit for transmitting an end-of-lifetime alert signal to an alert device if a remaining useful lifetime of an oxygen bottle is below a predetermined alert threshold.

A payload including a housing provided with one or more toothed guides or with one or more docking mechanisms, each of which is configured to detachably toothedly interact with an unmanned aircraft apparatus being docked so as to enable the movement of said docked unmanned aircraft apparatus with respect to the housing of the payload, wherein the housing of the payload is further configured to detachably toothedly interact with yet another (other) unmanned aircraft apparatus so as to enable the action of said yet another unmanned aircraft apparatus onto said docked unmanned aircraft apparatus for withdrawal of the latter from interaction with the housing of the payload. Furthermore, embodiments of an air transport system include two or more unmanned aircraft apparatuses and one of the payload.

An aerial vehicle has a passenger cabin for receiving at least one passenger, a load-bearing structure beneath the cabin, and a propulsion system including a number of propulsion units, which propel the aerial vehicle for powered flight and vertical take-off and landing (VTOL). The propulsion units are preferably carried by support arms attached to the load-bearing structure and extending upwards therefrom so as to support the propulsion units at a level above the cabin. The aerial vehicle is preferably reconfigurable to a compact configuration after landing, with at least some of the propulsion units overlapping the cabin and / or each other, while still allowing passenger transfer in and out of the vehicle, thereby facilitating efficient use of space for implementing a vertiport.

The invention relates to the technical field of zone control of illumination, in particular to a zone control method of an airplane passenger cabin scene illumination system, which comprises the following steps: acquiring real-time external natural light parameters of each porthole area in a passenger cabin and real-time passenger distribution data of each zone in the passenger cabin, and generating a first illumination distribution diagram through a ray tracing algorithm; real-time biological rhythm feedback signals of the passenger groups in all the partitions are obtained based on a non-imaging microwave radar sensor, the biological rhythm feedback signals comprise a first type of signals and a second type of signals, the current overall activity state of the passenger groups in all the partitions is judged based on the first type of signals, and the rest state depth is subdivided based on the second type of signals; and when the adjustment amplitude of the illumination parameters of the adjacent partitions exceeds a fifth preset threshold value, generating a natural transition zone of the illumination parameters between the adjacent partitions. By arranging the transition zone, the visual boundary is eliminated through gradient change of the transition zone of the adjacent partitions, and discomfort is reduced.