Abstract: An adjustable bed assembly for a vehicle includes a contoured bed frame, a foundation disposed in the bed frame and coupled to an articulated frame having a support platform with a plurality of sectional support members. A linkage mechanism couples the support platform to the foundation and a drive mechanism operably coupled to the linkage assembly adjusts the position of at least one sectional support member. A mattress is disposed on the support platform and configured to conform with the plurality of sectional support members. A monitor mounted on the bed frame is movable between a retracted position and an extended position. A control device has a first preset for concurrently adjusting the articulated frame and moving the monitor.

Abstract: The present application relates to providing an aircraft storage container including a lower portion having a horizontal bottom and a plurality of vertical sides configured to form a storage volume, an upper portion rotationally coupled to one of the plurality of vertical sides, a gas piston having a locking mechanism wherein the gas piston is coupled between the lower portion and the upper portion, the gas piston being configured to support the upper portion when the locking mechanism is engaged, a rotational member operative to disengage the locking mechanism when rotated and to engage the locking mechanism when released, and a latch mechanism having a rotational lever, wherein the latch mechanism is operative to rotate the rotational member in response to a pressure on the rotational lever.

Abstract: 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.

Abstract: 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.

Abstract: The present application relates to providing an aircraft storage container including a lower portion having a horizontal bottom and a plurality of vertical sides configured to form a storage volume, an upper portion rotationally coupled to one of the plurality of vertical sides, a gas piston having a locking mechanism wherein the gas piston is coupled between the lower portion and the upper portion, the gas piston being configured to support the upper portion when the locking mechanism is engaged, a rotational member operative to disengage the locking mechanism when rotated and to engage the locking mechanism when released, and a latch mechanism having a rotational lever, wherein the latch mechanism is operative to rotate the rotational member in response to a pressure on the rotational lever.

Abstract: An adjustable bed assembly for a vehicle includes a contoured bed frame, a foundation disposed in the bed frame and coupled to an articulated frame having a support platform with a plurality of sectional support members. A linkage mechanism couples the support platform to the foundation and a drive mechanism operably coupled to the linkage assembly adjusts the position of at least one sectional support member. A mattress is disposed on the support platform and configured to conform with the plurality of sectional support members. A monitor mounted on the bed frame is movable between a retracted position and an extended position. A control device has a first preset for concurrently adjusting the articulated frame and moving the monitor.

Abstract: An interior panel for an aircraft, an aircraft including an interior panel, and a method for making an interior panel for an aircraft are provided. In one example, the interior panel includes a support substrate that has a substrate surface. A first trim section is coupled to the support substrate. The first trim section has a first exposed surface that extends to a first edge portion. A second trim section is coupled to the support substrate. The second trim section has a second exposed surface that extends to a second edge portion that is disposed adjacent to the first edge portion. The first edge portion is offset from the second edge portion to define a gap. A light source is substantially covered by the first exposed surface and generates light that passes through the gap and illuminates at least a portion of the second exposed surface.