Passenger seats having improved comfort emergency egress solutions for mini suites or other types of passenger seats that have a privacy screen, wall, or sliding door that divides the passenger seat from the aisle area or other common area. Specific embodiments find particular use on-board passenger transportation vehicles, such as aircraft, where comfort and privacy must be balanced with safety and federal regulations.

An aircraft cabin includes an upper deck, and a cargo area. The cargo area is configured to accommodate at least one passenger and is situated at a different level than the upper deck. An accessway provides access between the upper deck and the cargo area. The upper deck has, at least locally, a raised floor in the vicinity of the accessway so that at least one part of the cargo area has a ceiling height higher than the ceiling height of the rest of the area cargo.

An aircraft cabin includes an upper deck, and a cargo area. The cargo area is configured to accommodate at least one passenger and is situated at a different level than the upper deck. An accessway provides access between the upper deck and the cargo area. The upper deck has, at least locally, a raised floor in the vicinity of the accessway so that at least one part of the cargo area has a ceiling height higher than the ceiling height of the rest of the area cargo.

The present invention concerns a cooling device and method of forming and regenerating same for use in keeping perishable products cool. The cooling device includes a porous substrate that has been soaked in a first composition including at least one anti-freeze agent before being soaked in a second composition including at least one crosslinking agent and be exposed to UV irradiation. The cooling device further includes a substrate cover for sealingly covering the porous substrate after being soaked in the second composition and exposed to the UV irradiation. Prior to use, the cooling device is cooled to a desired temperature and exposed to further UV irradiation.

A handle system for a vehicle is disclosed and includes a support structure defining a handle. The support structure is movable between a stowed position where the handle is inaccessible by a passenger and a deployed position where the handle is accessible by the passenger. The handle system also includes an actuator operably coupled to the support structure and configured to move the support structure between the stowed position and the deployed position. The handle system further includes one or more sensors configured to obtain data indicative of vehicle motion and a controller. The controller is configured to determine the vehicle exceeds a threshold rate of movement based on the data obtained by the one or more sensors. In response to determining the vehicle exceeds the threshold rate of movement, the controller instructs the actuator to move the support structure from the stowed position into the deployed position.

A handle system for a vehicle is disclosed and includes a support structure defining a handle. The support structure is movable between a stowed position where the handle is inaccessible by a passenger and a deployed position where the handle is accessible by the passenger. The handle system also includes an actuator operably coupled to the support structure and configured to move the support structure between the stowed position and the deployed position. The handle system further includes one or more sensors configured to obtain data indicative of vehicle motion and a controller. The controller is configured to determine the vehicle exceeds a threshold rate of movement based on the data obtained by the one or more sensors. In response to determining the vehicle exceeds the threshold rate of movement, the controller instructs the actuator to move the support structure from the stowed position into the deployed position.

An apparatus for securing a raceway assembly within an aircraft, which includes a clip assembly associated with the raceway assembly, which secures the raceway assembly to a seat rail. The apparatus further includes a floor panel positioned in overlying relationship to the raceway assembly and the clip assembly.

The present application relates to securing a mattress within an aircraft including a pliable enclosure configured for enclosing a cushion including a fastener system for providing access to an interior of the pliable enclosure when the fastener system is in an open state and for restraining the mattress when the fastener system is in a closed state and wherein the pliable enclosure has a top surface and a bottom surface and a strapping system affixed to the bottom surface wherein the strapping system includes a strap extension affixed to the strapping system wherein the strap extension is configured to be received by a retention clip secured to a bed support platform.

Described is a passenger seat assembly that may include a seat back including a rearward surface, a seat shroud positioned proximate to the rearward surface of the seat back and fixedly coupled to a seat frame, wherein the seat shroud remains stationary as the seat back moves between a stowed position and a deployed position, and at least one moveable shroud member coupled to the seat shroud at an attachment point and positioned proximate a rearward surface of the seat shroud, wherein a location of the attachment point is adjustable.

A component system for an aircraft, having at least one furnishing component, a plurality of component rails, a plurality of guide elements engageable with and movable relative to the component rails, a plurality of retaining elements connected to the guide elements and configured to be coupled to a hull structure of the aircraft or the at least one furnishing component, and a plurality of locking units arranged on the component rails and/or on the guide elements and configured to lock the guide elements to a particular rail. At least two component rails are arranged on the at least one furnishing component or the hull structure at a distance and parallel to each other such that the furnishing component is retractable via the component rails on guide elements or component rails that are spatially fixed in the aircraft and can be locked in a retracted position by the locking units.