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
05.03.2025
Patent
Elektronische Ressource
Englisch