Abstract: Advancements in executive aircraft interior design explicitly address the limitations of traditional physical windows within aircraft cabins. The passenger experience is transformed by integrating advanced hybrid technology, replicating expansive exterior views, fostering a sense of connection to the surroundings, and an immersive travel experience through a mimetic virtual display.

Abstract: Overhead passenger comfort modules are provided with a module segment having a support frame member which includes a perimetrical trim frame member, and a ventilation system supported by the support frame member. The ventilation system includes a supply conduit adapted to being fluid-connected to a supply of ventilation air, and first and second branch conduits fluid-connected at one end to the supply conduit and terminating in elongate first and second ventilation openings at first and second edge regions of the support frame member. First and second concavely curved edge diffuser portions are provided which are adjacently positioned to and spaced from the first and second ventilation openings respectively.

Abstract: Separable partition assemblies provide privacy between adjoining aircraft cabin sections, e.g., between a main passenger cabin section and a section having an emergency exit and a belted toilet seat such as may be provided in executive aircraft. The separable partition assembly includes a bulkhead structure defining a bulkhead passageway opening to allow passenger egress from one vehicle cabin section to an adjoining vehicle cabin section that is provided with at least one panel sized and configured to close the bulkhead passageway. A nonpermanent mounting system mounts the panel to an inboard edge of the bulkhead structure to allow the at least one panel to be separably uncoupled from the bulkhead structure in response to exertion of a force of predetermined magnitude thereagainst to thereby allow unimpeded passenger egress between the adjoining vehicle cabin sections.

Abstract: Separable partition assemblies provide privacy between adjoining vehicle cabin sections, e.g., between a main passenger cabin section and a section having an emergency exit and a belted toilet seat such as may be provided in executive aircraft. According to the disclosed embodiments, the partition assembly includes a bulkhead structure defining a bulkhead passageway opening to allow passenger egress from one vehicle cabin section to an adjoining vehicle cabin section. At least one panel is provided which is sized and configured to close the bulkhead passageway opening defined in the bulkhead structure. A nonpermanent mounting system mounts the at least one panel to an inboard edge of the bulkhead structure to allow the at least one panel to be separably uncoupled from the bulkhead structure in response to exertion of a force of predetermined magnitude thereagainst, the mounting system having separable mounting elements (e.g.

Abstract: Passenger interface units include individual passenger modules having co-located controls for passenger comfort and entertainment systems. The modules will include a glass panel having front and rear surfaces, a structural support panel bonded to the rear surface of the glass panel and a light-emitting unit supported by the support panel behind the rear surface of the glass panel. The rear surface of the glass panel may include an opaque printed coating layer having at least one unpainted region that is transparent to visible light emitted by the light-emitting unit thereby allowing the visible light to be transmitted through the glass panel and visible at the front surface thereof.

Abstract: Adaptive, self-adjusting decorative trim assemblies are especially adapted for use in aircraft cabin interiors where the fuselage undergoes deformation and/or distortion due to pressurization during flight. The self-adjusting features of the decorative trim assemblies according to the embodiments described herein thus allow for relative movement between mutually intersecting interior cabin panels without jeopardizing the cabin interior aesthetics (e.g., since the relative positioning of the panels is not disrupted by virtue of such fuselage deformations).

Abstract: Adaptive, self-adjusting decorative trim assemblies are especially adapted for use in aircraft cabin interiors where the fuselage undergoes deformation and/or distortion due to pressurization during flight. The self-adjusting features of the decorative trim assemblies according to the embodiments described herein thus allow for relative movement between mutually intersecting interior cabin panels without jeopardizing the cabin interior aesthetics (e.g., since the relative positioning of the panels is not disrupted by virtue of such fuselage deformations).

Abstract: Passenger interface units include individual passenger modules having co-located controls for passenger comfort and entertainment systems. The modules will include a glass panel having front and rear surfaces, a structural support panel bonded to the rear surface of the glass panel and a light-emitting unit supported by the support panel behind the rear surface of the glass panel. The rear surface of the glass panel may include an opaque printed coating layer having at least one unpainted region that is transparent to visible light emitted by the light-emitting unit thereby allowing the visible light to be transmitted through the glass panel and visible at the front surface thereof.