A mounting system configured to mount a personal electronic device (PED) in an aircraft flight deck is provided. The mounting adapter includes: an annunciator light including an LED strip for providing an annunciation regarding the PED; a display disable system mounted within the mounting adapter for disabling the PED display; and a controller configured to: obtain a captured frame of the PED display; send the captured frame to a server for determining whether a problem exists with an image displayed on the PED display; and responsive to receiving an annunciation indicator from the server indicating that the problem exists with the image displayed on the PED display, enable the display disable system to shut off the PED display and command the annunciator light to illuminate in a particular color that indicates that the PED display was shut off because the problem exists with the image displayed on the PED display.

A floor lighting assembly includes a luminous composite sheet and a light transmissive carpet. The luminous composite sheet has a top side, a bottom side, and an edge extending from the top side to the bottom side. The light sources are arranged in a row and are configured to emit light into the light guide film through the edge. The light transmissive carpet is disposed above the top side of the light guide film. The light transmissive carpet includes a backing structure and a pile mounted to and extending from the backing structure. The light guide film is configured to spread and redirect the light that is received therein through the edge for emitting the light through the top side of the light guide film such that some of the light is transmitted through the light transmissive carpet.

Systems and methods to combine lights and cameras are disclosed. Exemplary implementations may carry a housing that holds both a lighting component and a video camera; receive instructions to operate the lighting component in at least one of two different lighting modes, including a landing lighting mode and a taxi lighting mode; control the video camera to capture video information at a particular frame rate; and control the lighting component to emit light in a manner that supports at least one particular lighting mode and that includes switching off or turning down the lighting component in synchrony with the particular frame rate to reduce glare and/or otherwise improve the captured video information.

An aircraft light includes a support board and a supporting profile. The support board supports at least one electric light source, in particular at least one LED. The support board has two lateral edges, which extend in a longitudinal direction of the support board and which are spaced apart from each other in a transverse direction (T) of the support board. The supporting profile comprises a receiving space for receiving and supporting the support board. The receiving space is defined by a base, extending in a longitudinal direction (L) of the supporting profile and in a transverse direction (T) of the supporting profile, and two opposing side walls protruding from the base. The supporting profile further comprises two undercut sections, forming opposing slots in the two opposing side walls that are dimensioned for accommodating a lateral edge of the support board, respectively.

A self-powered, wireless lighting system for an aircraft evacuation system. The lighting system includes a piezoelectric sensor configured to generate electrical energy under an aircraft evacuation event when the aircraft evacuation system is deployed, and a first light source disposed on the aircraft evacuation system, the first light source configured to provide illumination to the aircraft evacuation system. The piezoelectric sensor is operably connected to the first light source and configured to supply electrical energy to the light source based on vibrations in the evacuation system during deployment of the evacuation system and during use of the evacuation system as passengers evacuate the aircraft.

The present disclosure is directed to a blended wing body aircraft including a blended wing body, wherein the blended wing body is characterized by having no clear dividing line between wings and a main body along a leading edge of the aircraft, at least a rib, wherein the at least a rib runs longitudinally from fore to aft of the main body, and a plurality of transparent panels located in the top surface of the main body, wherein the plurality of transparent panels are located in channels, wherein the channels are separated by the at least a rib.

A method of indicating a flight direction of an aerial vehicle, having a vehicle body and a plurality of rotors supported by the vehicle body, includes: on the basis of a momentary flight direction of the aerial vehicle, controlling a matrix of light sources, in particular a matrix of LEDs, which are mounted to the vehicle body of the aerial vehicle, to provide an illumination pattern to an observer of the aerial vehicle, with the illumination pattern comprising a flight direction indication, indicative of the momentary flight direction of the aerial vehicle.

An air duct system comprising an air duct having a main body, a visible light source, and one or more photovoltaic devices. The main body of the air duct defines a passageway having a reflective inner surface. The visible light source is configured to generate visible light, where the visible light source directs the visible light along the reflective inner surface of the air duct. The one or more photovoltaic devices are disposed along the reflective inner surface of the air duct, where a portion of the visible light generated by the visible light source is converted into electrical power by the one or more photovoltaic devices.

A sanitizing unit configured for use in an air distribution system of a passenger aircraft is disclosed. The sanitizing unit may include an input structure connected to a cabin air supply plenum, a UV reflective insert that defines an irradiation chamber, at least one ultraviolet (UV) light emitting diode (LED) positioned to provide UV radiation to an airflow within the irradiation chamber, a UV attenuator; and an output structure connected to at least one overhead passenger vent, wherein the at least one overhead passenger vent is configured to output a treated airflow.

The invention relates to a method for automatically guiding a drone with a computer, with a view to landing the drone on a docking and recharging platform, the drone comprising a first luminous means that emits a first light signal and a second luminous means that emits a second light signal different from the first light signal, the first luminous means and the second luminous means being fastened at two separate points to the drone, the station receiving images captured by a camera, said method comprising: —analyzing the images captured by the camera so as to locate the first and second luminous means, —determining the position and orientation of the drone depending on the determined position of the first and second luminous means, —generating, with the computer, piloting instructions intended for the drone, said instructions being configured to guide the drone towards the docking and recharging platform, —transmitting said instructions to the drone, —the drone receiving and implementing said instructions.