Abstract: An evacuation slide to provide an egress path from an exit of an aircraft. The evacuation slide includes one or more slide lanes. One or more jump targets and indicators are positioned along each of the slide lanes to visually inform persons how to enter a ramp of the slide. Lights illuminate one or more sections of the slide to further provide visual guidance on how to enter the ramp.

Abstract: An evacuation slide to provide an egress path from an exit of an aircraft. The evacuation slide includes one or more slide lanes. One or more jump targets and indicators are positioned along each of the slide lanes to visually inform persons how to enter a ramp of the slide. Lights illuminate one or more sections of the slide to further provide visual guidance on how to enter the ramp.

Abstract: An evacuation slide to provide an egress path from an exit of an aircraft. The evacuation slide includes one or more slide lanes. One or more jump targets and indicators are positioned along each of the slide lanes to visually inform persons how to enter a ramp of the slide. Lights illuminate one or more sections of the slide to further provide visual guidance on how to enter the ramp.

Abstract: An evacuation slide to provide an egress path from an exit of an aircraft. The evacuation slide includes one or more slide lanes. One or more jump targets and indicators are positioned along each of the slide lanes to visually inform persons how to enter a ramp of the slide. Lights illuminate one or more sections of the slide to further provide visual guidance on how to enter the ramp.

Abstract: Disclosed herein is an example ceiling header system for an aircraft cabin that includes a ceiling between a first storage bin and a second storage bin. The ceiling header system includes a ceiling header that includes a top surface that conforms to the ceiling and a bottom surface that is opposite the top surface. The ceiling header system also includes a curtain track. The top surface is configured to be held against the ceiling via the curtain track being placed against the bottom surface, the curtain track being (i) attachable at a first end of the curtain track to a first rail of the first storage bin and (ii) attachable at a second end of the curtain track to a second rail of the second storage bin.

Abstract: Disclosed herein is an example ceiling header system for an aircraft cabin that includes a ceiling between a first storage bin and a second storage bin. The ceiling header system includes a ceiling header that includes a top surface that conforms to the ceiling and a bottom surface that is opposite the top surface. The ceiling header system also includes a curtain track. The top surface is configured to be held against the ceiling via the curtain track being placed against the bottom surface, the curtain track being (i) attachable at a first end of the curtain track to a first rail of the first storage bin and (ii) attachable at a second end of the curtain track to a second rail of the second storage bin.

Abstract: A light projection device includes a mixing tube having an open exit end, and a plurality of light sources, each of the plurality of light sources positioned to emit a light stream toward the open exit end of the mixing tube. A diffuser is disposed between the plurality of light sources and the open exit end of the mixing tube, the diffuser configured to diffuse at least one light stream from the plurality of light sources into a diffused light stream. A template is positioned proximate the open exit end of the mixing tube and configured to shape the diffused light stream from the diffuser into a patterned light stream.

Abstract: A light projection device includes a mixing tube having an open exit end, and a plurality of light sources, each of the plurality of light sources positioned to emit a light stream toward the open exit end of the mixing tube. A diffuser is disposed between the plurality of light sources and the open exit end of the mixing tube, the diffuser configured to diffuse at least one light stream from the plurality of light sources into a diffused light stream. A template is positioned proximate the open exit end of the mixing tube and configured to shape the diffused light stream from the diffuser into a patterned light stream.

Abstract: Aircraft having multiple seating configurations and associated systems and methods are disclosed. An aircraft in accordance with one embodiment, for example, can include a fuselage having a generally circular cross-sectional shape and one or more passenger cabin portions. The individual cabin portions can include a floor connected to the fuselage and a plurality of passenger seats attached to the floor. The passenger seats are in a configuration selected from a first twin aisle seat-row arrangement and a second, single aisle seat-row arrangement. Each of the first and second seat-row arrangements is implementable in the fuselage. Further, the seats in either the first seat-row arrangement or the second seat-row arrangement have between a three abreast and a six abreast seating configuration.

Abstract: The disclosure provides for an aircraft video control station. In an embodiment, the aircraft video control station comprises a wall mounted control panel, a desktop, a seat that is stowed when not in use, and a cabinet that contains the wall mounted control panel, the desktop, and the seat. The cabinet may have a depth in the range of about 10 inches to about 37 inches, and preferably has a depth of 15 inches. The seat may be in the form of a swing out seat.

Abstract: The disclosure provides for an aircraft video control station. In an embodiment, the aircraft video control station comprises a wall mounted control panel, a desktop, a seat that is stowed when not in use, and a cabinet that contains the wall mounted control panel, the desktop, and the seat. The cabinet may have a depth in the range of about 10 inches to about 37 inches, and preferably has a depth of 15 inches. The seat may be in the form of a swing out seat.

Abstract: Aircraft having multiple seating configurations and associated systems and methods are disclosed. An aircraft in accordance with one embodiment, for example, can include a fuselage having a generally circular cross-sectional shape and one or more passenger cabin portions. The individual cabin portions can include a floor connected to the fuselage and a plurality of passenger seats attached to the floor. The passenger seats are in a configuration selected from a first twin aisle seat-row arrangement and a second, single aisle seat-row arrangement. Each of the first and second seat-row arrangements is implementable in the fuselage. Further, the seats in either the first seat-row arrangement or the second seat-row arrangement have between a three abreast and a six abreast seating configuration.

Abstract: A modular overhead stowage bin system has an outboard bin support and a center bin support coupleable to the fuselage. First and second stowage bin modules having different storage capacities are connectable to the outboard and center bin supports in first and second configurations. In a first configuration, the first and second stowage bin modules are coupled to the fuselage and have a first overhead aisle therebetween with first opposing edge portions. The first and second stowage bin modules in the second configuration are coupled to the fuselage and have a second overhead aisle therebetween. The second overhead aisle has second opposing edge portions each shifted laterally relative to the position of the first opposing edge portions of the first overhead aisle when the first and second stowage bin modules are in the first configuration.

Abstract: A modular overhead stowage bin system has an outboard bin support and a center bin support coupleable to the fuselage. First and second stowage bin modules having different storage capacities are connectable to the outboard and center bin supports in first and second configurations. In a first configuration, the first and second stowage bin modules are coupled to the fuselage and have a first overhead aisle therebetween with first opposing edge portions. The first and second stowage bin modules in the second configuration are coupled to the fuselage and have a second overhead aisle therebetween. The second overhead aisle has second opposing edge portions each shifted laterally relative to the position of the first opposing edge portions of the first overhead aisle when the first and second stowage bin modules are in the first configuration.