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.
INTEGRATED CHILLING UNIT FOR AN AIRCRAFT GALLEY
2025-03-06
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |