Abstract: In accordance with at least one aspect of this disclosure, a contoured class divider for dividing an aircraft cabin arrangement between at least one forward passenger seat and at least one aft passenger seat, includes a panel positioned adjacent to and rearwardly of the at least one forward seat. The panel has a contoured shape for receiving the back of the forward passenger seat in at least one of a reclined position and an upright position. The panel extends substantially from an underside of an overhead bin to a cabin floor. In embodiments, at least a portion of the panel is configured to deform or break during a crash event due to one or more of a head impact by a passenger in the aft passenger seat with the panel and/or inertial forces of the crash event acting on the panel.

Abstract: An implementation of a contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having an aft-facing convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include an articulation system to articulate at least a portion of the panel from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft.

Abstract: An implementation of a contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having an aft-facing convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include an articulation system to articulate at least a portion of the panel from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft.

Abstract: An implementation of a contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having an aft-facing convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include an articulation system to articulate at least a portion of the panel from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft.

Abstract: A contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having a convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include multiple panel portions that are coupled together and articulate relative to one another. The contoured class divider may include an articulation system to articulate the panel portions with respect to one another from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft.

Abstract: In a preferred embodiment, a contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having an aft-facing convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include an articulation system to articulate at least a portion of the panel from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft.

Abstract: A contoured class divider for dividing an aircraft cabin according to a predetermined class arrangement and including a divider panel having a contour closely matching a contour of a forward-positioned seatback, and adapted for being positioned in closely spaced-apart relation to the seatback for providing additional space aft of the divider panel. At least one leg is provided for supporting the panel on an aircraft cabin deck. A viewing window is formed in the panel for providing the ability of a flight attendant to observe areas of the cabin.

Abstract: In a preferred embodiment, a retrofit storage bin door hinge includes an extension member than increases the storage volume of the bin by at least 5 percent or 10 percent, thereby permitting the storage of larger carry-on bags. Required access to the ceiling panels during maintenance operations is preserved by the hinges pivotable attachment to a pivot mount attached to the ceiling of a storage bin. In this manner, the hinge assembly and door may be readily translated downwardly to provide full access to the ceiling panels during a maintenance operation.

Abstract: An implementation of a contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having an aft-facing convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include an articulation system to articulate at least a portion of the panel from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft.

Abstract: In a preferred embodiment, a retrofit storage bin door hinge includes an extension member than increases the storage volume of the bin by at least 5 percent or 10 percent, thereby permitting the storage of larger carry-on bags. Required access to the ceiling panels during maintenance operations is preserved by the hinges pivotable attachment to a pivot mount attached to the ceiling of a storage bin. In this manner, the hinge assembly and door may be readily translated downwardly to provide full access to the ceiling panels during a maintenance operation.

Abstract: An aircraft interior surface for partitioning, dividing, or establishing privacy within a cabin space includes a transparent material that provides for transmission of light within the aircraft cabin. A graphical design may be applied to the transparent material, the graphical design including indicia arranged in predetermined patterns based on a location or function of the transparent material. A light source located proximate to the transparent material may wash light across a surface of the transparent material such that the graphical design exhibits predetermined properties when illuminated by the light source. The transparent material may be selectively dimmable to increase opacity.

Abstract: A modular environment for a vehicle. The modular environment may include a configurable service space with a mounting system within the vehicle that has a number of modules configured to releaseably engage the mounting system. The module environment also may include a service space control system able to electronically communicate with and identify at least one of the modules. The modular environment may also include an arch framework that supports a number of fixed modules and a number of configurable modules. A further embodiment is shown of a method for using a service space control system that controls a modular environment for a vehicle having a configurable service, and including a mounting system configured to releaseably engage a number of modules in a service space. The service space control system electronically communicates with and can identify at least one of the modules and limit its use to only authorized users.

Abstract: A compartment for a transportation device is provided. The compartment may include a one-piece basin, an inflatable wall member, and multi-directional support arms to attach the basin within the transportation device. The one-piece basin may fit through an opening in the transportation device. Methods of installation for installing the compartment within the transportation device are also provided.

Abstract: An aircraft is provided comprising a fuselage and a central monitoring system positioned within the fuselage. A plurality of seating elements is also positioned within said fuselage. Each of the plurality of seating elements includes a plurality of seat options integrated into the seating element and an electronics control system integrated into the seating element. The electronics control system includes a seat processor having logic adapted to monitor an operational status of each of the seat options and communicate the operational status to the central monitoring system via wireless communication.

Abstract: Apparatus and methods for increasing useable space within a mobile platform compartment, such as an aircraft lavatory, which is adjacent a predetermined area, such as a passenger doorway area, of the mobile platform. The apparatus generally includes a turntable module rotatably coupled to supporting structure within the mobile platform. The turntable module can be rotated to a first angular position in which the turntable module is substantially within the compartment but outside the predetermined area. The turntable module can also be rotated to a second angular position in which the turntable module is substantially within the predetermined area but outside the compartment. The turntable module supports at least one item, such as a lavatory sink, which is accessible from within the compartment when the turntable module is in the second angular position.