A method, system and controller for controlling power supplied to a heating device of a window on a vehicle, comprising receiving information indicative of at least one parameter associated with operation of the vehicle, generating a power signal at least in part on a basis of the information indicative of the at least one parameter and stored control logic, the power signal being indicative of a power modulation level for power to be supplied to the heating device and transmitting the power signal to a power regulator for causing power to be supplied to the heating device in accordance with the power modulation level.

A translucent panel system comprising a panel (13) comprising a translucent layer provided with a transparent screen on which there is mounted a device having sensors sensing light energy from a light source, so as to allow viewing through the translucent layer, the panel (13) further comprising an internal layer provided with a polarisable film intended to modify the degree of opacity of the panel (13), the translucent layer being opposite the internal layer. The translucent panel system comprises an element for transmitting and/or storing energy originating from the device having sensors and a system for supplying power and adjusting the degree of opacity of the polarisable film, the power supply and adjustment system being at least partially supplied by the element for transmitting and/or storing light energy.

Various techniques provide systems and methods for facilitating aperture protection. In one example, a system for facilitating aperture protection is provided. The system includes an optical limiter device. The optical limiter device includes a thermochromic material and a plurality of nanostructures, where each of the nanostructures is in contact with a portion of the thermochromic material. At least a subset of the nanostructures is configured to receive incident light and generate heat in response to the incident light. At least a portion of the thermochromic material is configured to transition from a first state to a second state in response to the heat and block the incident light when the portion is in the second state. The portion is configured to transition from the second state back to the first state when the portion cools, such as upon removal of the incident light. Related methods and products are also provided.

A laminated glazing includes a first and a second glass sheet that are bonded by a first interlayer adhesive layer, a peripheral zone of the laminated glazing being covered by a stepped metal element, a window press that is rigidly connected to the structure for mounting the laminated glazing making contact with the laminated glazing, so as to hold the laminated glazing secure to its mounting structure, an electrical conductor having a first end that is electrically linked to the stepped metal element and a second tapered end at a non-zero distance at most equal to 1 mm from the window press.

Arrangements for an aircraft passenger cabin including a seating area containing first and second passenger seats, a monument disposed at one end of the seating area, and at least one privacy divider deployable in a longitudinal direction of the seating area to divide at least a portion of the seating area for privacy. In some embodiments, the at least one privacy divider includes a first privacy divider adapted to deploy to divide the seating area forward of the first and second passenger seats and a second privacy divider deployable to the seating area between the first and second passenger seats.

Aspects of this disclosure relate to a removable fuselage expansion window assembly, comprising: a window panel; an outer window frame; a window bracket configured to secure the window panel to the outer window frame; an inner window frame with an indented rim that is aligned with the window bracket; and a latch assembly located below the indented rim of the inner window frame between the outer window frame and the inner window frame. The latch assembly includes one or more retainers to hold a bottom portion of the removable fuselage expansion window assembly within a rectangular frame formed by vertical and horizontal beams in an outer wall of an aircraft, wherein the latch assembly includes a lever that releases the removable fuselage expansion window assembly by disengaging the one or more retainers from the rectangular frame when the lever is pulled.

Methods and systems for controlling an aircraft cabin display are described herein. The method comprises obtaining a reflected color on a surface adjacent to a cabin window of an aircraft, generating an image having an image color in accordance with the reflected color on the surface adjacent to the cabin window, and displaying the image having the image color on a display device covering the cabin window.

A network system for monitoring and storing data of aircraft intelligent windows or windshields to provide useable life of, provide real life performance of, and/or measure characteristics and/or properties of, the windshields forwards the data from sensors mounting the windshield to a window sensing hub having a microprocessor programed to receive and process the data to determine the performance of the windshield and formatting the data in accordance to a preset program, wherein the program includes providing data from the sensors that measures characteristics and properties of the windshield that are active during the period in which the data is taken. An aircraft central maintenance system connected to the window sensing hub receives the formatted information from the window sensing hub and unfiltered or unformatted information, wherein the unfiltered information from the windshield is acted on by the central maintenance system to provide an estimated useable life of the windshield.

An article is provided. The article includes a first transparent conductive oxide layer, a transparent metal layer on the first transparent conductive oxide layer, wherein a thickness of the transparent metal layer continuously decreases in a direction; and a second transparent conductive oxide layer on the transparent metal layer.

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.