An integrated chilling unit (200) for above-counter installation in an aircraft galley. The integrated chilling unit (200) 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 (200) 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 (204, 205).
INTEGRATED CHILLING UNIT FOR AN AIRCRAFT GALLEY
INTEGRIERTE KÜHLEINHEIT FÜR EINE FLUGZEUGBORDKÜCHE
UNITÉ DE REFROIDISSEMENT INTÉGRÉE POUR CUISINE DE BORD D'AÉRONEF
2025-03-05
Patent
Electronic Resource
English