A reinforcing element for a structural profile, in particular for a round, oval or elliptical structural tube. The reinforcing element comprises: a fiber structure which has a hollow-cylindrical, helically wound mesh of fiber strands and forms an inner shell surface formed to receive the structural profile; and a matrix material into which the fiber strands are respectively embedded and which is formed to be shrinkable by heating so that the fiber structure can be fastened to the structural profile with the inner shell surface by heating the matrix material. Also provided are a structural arrangement with such a reinforcing element, an aircraft or spacecraft with such a structural arrangement, as well as a method for producing such a structural arrangement.

A galley cart stowage system for stowing galley carts in a galley of an aircraft includes a lower cart compartment and an upper cart compartment located above the lower cart compartment both configured to receive at least one galley cart. At least one vertical conveyance device extends between the cart compartments to move the galley carts between the cart compartments. A galley workspace having a workspace volume is located between the cart compartments. The galley workspace has a countertop movable between a deployed position and a clearance position to form an opening between the lower cart compartment and the upper cart compartment to allow movement of the galley carts between the lower cart compartment and the upper cart compartment.

A galley cart stowage system for stowing galley carts in a galley of an aircraft includes a lower cart compartment and an upper cart compartment located above the lower cart compartment both configured to receive at least one galley cart. At least one vertical conveyance device extends between the cart compartments to move the galley carts between the cart compartments. A galley workspace having a workspace volume is located between the cart compartments. The galley workspace has a countertop movable between a deployed position and a clearance position to form an opening between the lower cart compartment and the upper cart compartment to allow movement of the galley carts between the lower cart compartment and the upper cart compartment.

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.

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 power management system and method for a vehicle includes a plurality of ultraviolet (UV) light sub-systems within an internal cabin of the vehicle. A power management control unit is in communication with the plurality of UV light sub-systems. The power management control unit is configured to adaptively control power supplied to the plurality of UV light sub-systems based on power usage data. The power supplied to the plurality of UV light sub-systems changes. The power usage data includes information regarding adaptable power requirements for the plurality of UV light sub-systems.

An aircraft is disclosed with a fuselage including a cabin delimited by a cabin floor and having crew quarters. The crew quarters include an upper portion above a floor plane defined by the cabin floor and a lower portion beneath the floor plane. The crew quarters include a seat adjustable between a sitting configuration and a berthing configuration. A method of transitioning a crew member of an aircraft to a berthing configuration in a crew quarters is also disclosed.

Countertop storage assembly are provided. In one example, a countertop storage assembly includes a countertop having a countertop area outer surface, a countertop area inner surface, and an opening formed therethrough. A retractable storage assembly includes a lid that is disposed in the opening when in a closed position and that moves between the closed position and an open, retracted position. During movement from the closed position to the open, retracted position, the lid moves downward and away from the opening to below the countertop off-set from the opening. A storage area includes a base that is in a retracted position situated below the countertop when the lid is in the closed position. The base moves from the retracted position to a deployed position where the base is disposed in the opening when the lid is in the open, retracted position.

Countertop storage assembly are provided. In one example, a countertop storage assembly includes a countertop having a countertop area outer surface, a countertop area inner surface, and an opening formed therethrough. A retractable storage assembly includes a lid that is disposed in the opening when in a closed position and that moves between the closed position and an open, retracted position. During movement from the closed position to the open, retracted position, the lid moves downward and away from the opening to below the countertop off-set from the opening. A storage area includes a base that is in a retracted position situated below the countertop when the lid is in the closed position. The base moves from the retracted position to a deployed position where the base is disposed in the opening when the lid is in the open, retracted position.

An aircraft trolley retention device may include a retention latch with a shaft including a first component of an interlocking assembly and a sleeve including a second component of the interlocking assembly and configured to receive the shaft, and an interlocking assembly. The retention latch may be configured to actuate between a closed position and an open position. The interlocking assembly may be configured to guide the retention latch during the actuation between the closed position and the open position. The retention latch may be configured to retain an aircraft trolley within an aircraft trolley bay when the retention latch is in the closed position. A portion of the retention latch may be configured to be positioned in front of a striker plate corresponding to a handle of an aircraft trolley bay door of the aircraft trolley bay when the retention latch is in the open position.