An aerospace galley insert includes an oven defining therein an oven inner cavity for receiving food to be prepared and a fluid supply for supplying fluid comprising water or water vapour to the oven inner cavity. The galley also includes an exterior space, a heat pipe extending between the cavity and the exterior space, a first temperature sensor for detecting a first temperature in the cavity, a second temperature sensor for detecting a second temperature in the exterior space, and a third temperature sensor for detecting a third temperature of the heat pipe where it extends into the exterior space. The system also includes a control unit configured to determine an actual water vapour concentration in the oven inner cavity based on the first, second and third temperatures, and configured to control the fluid supply in order to adjust the actual water vapour concentration to a target water vapour concentration.

A vehicle includes an internal cabin. An enclosed component is within the internal cabin. The enclosed component includes an intumescent coating. As an example, the enclosed component is a lavatory within the internal cabin. As another example, the enclosed component is a waste compartment. As another example, the enclosed component is a grille within a door.

A vehicle includes an internal cabin. An enclosed component is within the internal cabin. The enclosed component includes an intumescent coating. As an example, the enclosed component is a lavatory within the internal cabin. As another example, the enclosed component is a waste compartment. As another example, the enclosed component is a grille within a door.

A vehicle includes an internal cabin. One or more areas are within the internal cabin. The one or more areas include one or more water-drawing components. A water supply system is within the internal cabin. The water supply system is configured to provide water to the one or more water-drawing components. A water leak detection system includes one or more sensing devices configured to detect water flow from the water supply system to the one or more water-drawing components. One or more shut-off valves are disposed on or within the water supply system. A control unit is in communication with the one or more sensing devices, the one or more shut-off valves, and the one or more water-drawing components. The control unit is configured to operate the one or more shut-off valves to stop the supply of water to the one or more water-drawing components in response to the one or more sensing devices detecting the water flow when the one or more water-drawing components are not in use.

The present disclosure provides system for sealing a refrigerated galley of an aircraft. The system includes a door, and a seal assembly positioned at a bottom surface of the door. The seal assembly includes (i) a housing coupled to the bottom surface of the door, (ii) a seal positioned at least partially in the housing, wherein the seal is moveable relative to the housing and the door, (iii) a biasing mechanism coupled to the housing and the seal and configured to hold the seal in a relaxed state by applying a biasing force to the seal in a direction away from a floor surface of the refrigerated galley, and (iv) an activation mechanism coupled to the housing. The activation mechanism is configured to transition the seal from the relaxed state to a compressed state in response to a rotation of the door from an open position to a closed position.

The present disclosure provides system for sealing a refrigerated galley of an aircraft. The system includes a door, and a seal assembly positioned at a bottom surface of the door. The seal assembly includes (i) a housing coupled to the bottom surface of the door, (ii) a seal positioned at least partially in the housing, wherein the seal is moveable relative to the housing and the door, (iii) a biasing mechanism coupled to the housing and the seal and configured to hold the seal in a relaxed state by applying a biasing force to the seal in a direction away from a floor surface of the refrigerated galley, and (iv) an activation mechanism coupled to the housing. The activation mechanism is configured to transition the seal from the relaxed state to a compressed state in response to a rotation of the door from an open position to a closed position.

An aircraft interior structure for an aircraft cabin may include a main body with a plurality of walls, where at least one wall of the plurality of walls may be shared with an adjacent passenger suite including an aircraft seat. The passenger suite may be installed at an angle relative to an aisle of the aircraft cabin. The aircraft interior structure may include a cavity defined within the main body. The cavity may be a trapezoidal shape defined at least in part by the angle at which the passenger suite is installed in the aircraft cabin. The cavity may be configured to receive a plurality of galley carts. A length of each of the plurality of galley carts may be dependent on a depth of the cavity at respective locations in the trapezoidal shape.

An aircraft interior structure for an aircraft cabin may include a main body with a plurality of walls, where at least one wall of the plurality of walls may be shared with an adjacent passenger suite including an aircraft seat. The passenger suite may be installed at an angle relative to an aisle of the aircraft cabin. The aircraft interior structure may include a cavity defined within the main body. The cavity may be a trapezoidal shape defined at least in part by the angle at which the passenger suite is installed in the aircraft cabin. The cavity may be configured to receive a plurality of galley carts. A length of each of the plurality of galley carts may be dependent on a depth of the cavity at respective locations in the trapezoidal shape.

A stowage and removal system for an accommodation space for storing rollable containers in a vehicle is provided. It preferably has a rail system in the floor region of the accommodation space, on which rail system a transfer plate is movable, which transfer plate can assume a storage position and an insertion and removal position for the container. The storage position of the container is provided with its rear wall in the region of the rear wall of the accommodation space. The insertion and removal position is provided in the region of an insertion opening, arranged oppositely in relation to the rear wall, for the insertion and removal of a container into the accommodation space.

A stowage and removal system for an accommodation space for storing rollable containers in a vehicle is provided. It preferably has a rail system in the floor region of the accommodation space, on which rail system a transfer plate is movable, which transfer plate can assume a storage position and an insertion and removal position for the container. The storage position of the container is provided with its rear wall in the region of the rear wall of the accommodation space. The insertion and removal position is provided in the region of an insertion opening, arranged oppositely in relation to the rear wall, for the insertion and removal of a container into the accommodation space.