Abstract: An integrated chilling unit for above-counter installation in an aircraft galley. The integrated chilling unit includes a housing. The housing includes a top wall, a rear wall, a first side wall, a second side wall and a bottom wall. The integrated chilling unit also includes a door hingedly attached to the housing. An interior of the integrated chilling unit stores items for cooling. The housing includes a vacuum insulation structure, wherein the vacuum insulation structure comprises a vacuum insulation panel.

Abstract: A panel for use in the construction of a galley of an aircraft is disclosed. The panel comprises a décor panel and at least one insulation panel. The décor panel has first and second opposing faces, and a housing aperture extends through the décor panel between the first and second faces. The housing aperture is of substantially the same configuration as the insulation panel or the insulation panels collectively when arranged side by side or when stacked. The housing aperture is configured to receive the at least one insulation panel, and the or each insulation panel is located in the housing aperture.

Abstract: A panel for use in the construction of a galley of an aircraft is disclosed. The panel comprises a frame, at least one insulation panel, and a cover panel. The frame comprises first and second opposing faces and one or more edge faces, and each edge face extends between the first and second faces. The cover panel has first and second opposing faces and each insulation panel has first and second opposing faces. One or more of the edge faces of the frame define a housing aperture and the frame is fixed to the cover panel with the first face of the frame adjacent to the second face of the cover panel.