Patent classifications
B64D2011/0053
SEAT ASSEMBLY HAVING INTEGRATED LIGHTING SYSTEM
A seat assembly for an internal cabin of a vehicle includes a backrest, and a lighting system coupled to the backrest. A method of forming a seat assembly for an internal cabin of a vehicle includes coupling a lighting system to a backrest.
ACCENT LIGHTING SYSTEM FOR AN INTERIOR CABIN OF A VEHICLE
An accent lighting system is configured to provide accented light onto a desired location. The accent lighting system includes an accent adapter assembly that is configured to securely couple to a light source. The accent adapter assembly includes an accenting plate that is configured to accent light that is emitted from the light source. A method of securing an accent lighting system within an internal cabin of a vehicle includes removing an existing light source from an aperture of a composite panel, securing an accent adapter assembly to the existing light source to form the accent lighting system, and securing the accent lighting system in the aperture of the composite panel.
ILLUMINATING DEVICE AND INTERIOR PART FOR A VEHICLE
An illuminating device for a vehicle includes a carrier module, a flat light guide attached to the carrier module with a plurality of emitting points, and multiple light sources for illuminating the light guide. The flat light guide is concealed with a translucent haptic layer, which is attached to a visible side of the light guide, which, in turn, is covered by a decorative layer. The illuminating device comprises a rope-like light guide, which has an inherent light source and is connected to the decorative layer via a retaining device. This therefore results in a flat arrangement, which can be easily integrated into the interior parts and simultaneously enables illumination over a large surface area. In doing so, additional light effects can be integrated by means of the rope-like light guide. The illuminating device is not visible while switched off, as the illuminating device is covered by the decorative layer.
Aircraft passenger reading light having a visible and infrared light source
An aircraft passenger reading light comprises at least one reading light source, which is arranged for emitting visible light in a reading light emission direction; and at least one infrared light source, which is arranged for emitting infrared light in an infrared light emission direction. The infrared light emission direction is inclined with respect to the reading light emission direction.
Passenger supply system for installation in a passenger supply channel
A passenger supply system installed in a passenger supply channel (PSC) on board a vehicle, such as an aircraft. The supply system comprises a rail track configured to be mounted along the PSC. The supply system further comprises an indiv panel mounted on the rail track and connectable to the PSC for supplying a passenger with conditioned air, medical outlet and/or oxygen. The indiv panel comprises a crossover area. The supply system further comprises a passenger supply unit mounted on the rail track and connectable to the PSC for supplying the passenger with light, visual information and/or sound information. The supply unit comprises an overlapping area. The supply unit and the indiv panel are configured such that in a mounted state of the supply unit and of the indiv panel the overlapping area of the supply unit at least partially overlaps with the crossover area of the indiv panel.
OVERHEAD LUGGAGE COMPARTMENT FOR AIRCRAFT
The invention relates to an overhead luggage compartment for aircraft, comprising: a tray for accommodating pieces of luggage, which tray can be pivoted about an axis of rotation between a closed position and an open position; and comprising a housing, which encloses the tray in the closed position and which has devices arranged thereon for fastening to a supporting structure of the aircraft and has a suspension device for a passenger service unit; and comprising a closure element for holding the tray in the closed position. The housing is formed by two frame parts arranged lateral to the tray, which frame parts are connected to each other by means of cross-braces, and the fastening devices and the suspension device for the passenger service unit and at least one stop element for limiting the open position of the tray are arranged on the frame parts.
Reading lamp for installation in a cabin trim element of a vehicle
The invention relates to a reading lamp for installation in a cabin trim element (4) of a vehicle, in particular of an aircraft, comprising an installation frame (1) having a ring element (2), a lamp housing (7) having a mating support surface (8), and a clamping ring (9) wherein the clamping ring (9) is connected to the installation frame (1) by means of tension spring elements (10), such that the lamp housing (7) is forced against the support surface (6) of the inner surface of the ring element (2) by means of the clamping ring (9) and may be moved with respect to the installation frame (1) in the manner of a ball and socket joint.
Passenger service module with integrated cabin lighting
A service module for supplying passengers in a passenger space of a means of transport, in particular of an aircraft, and to a service system having a service channel and a plurality of such service modules. The service module comprises at least one service component arrangement having one or more service components for individually supplying one or more passengers, and a cabin lighting unit for illuminating the passenger space of the means of transport, in particular of the aircraft.
Aircraft power management system and method for managing power supply in an aircraft
An aircraft power management system includes an electrical power supply input configured to be coupled to an electrical power supply, a first power supply bus bar coupled to the power supply input, at least one primary electrical equipment including a primary load coupled in parallel to the first power supply bus bar, a bus bar switch configured to selectively deactivate the first power supply bus bar downstream of the at least one primary electrical equipment, a load monitoring device configured to monitor the power demand of the primary load and to output a deactivation signal to the bus bar switch for selectively deactivating the first power supply bus bar, if the monitored power demand of the primary load exceeds a primary threshold, and at least one tertiary electrical equipment including a tertiary load coupled to the first power supply bus bar downstream of the at least one primary electrical equipment.
GASPER EXTENSION FOR REDUCED DISEASE TRANSMISSION
A gasper for use in a passenger aircraft includes an inlet configured to receive air. The gasper further includes an outlet configured to output the air towards a passenger seat. The gasper further includes a body extending from the inlet to the outlet and being adjustable between at least three lengths.