An aircraft galley plumbing system (100) includes a potable water sub-system (102), a waste water sub-system (120), and a valve (106) in fluid communication with the potable water sub-system and the waste water sub-system. The potable water sub-system includes a plurality of potable water supply lines (104) configured to provide potable water from a potable water source to at least one galley installation. The waste water sub-system includes a plurality of drain lines (122) configured to receive waste water from the at least one galley installation, a plurality of waste water sumps (124) configured to receive waste water from the plurality of drain lines, and a main drain line (128). The potable water sub-system is configured to be filled from the potable water source when the valve is in a first operational configuration. The potable water sub-system is configured to empty into the waste water sub-system via the valve when the valve is in a second operational configuration.
AIRCRAFT GALLEY PLUMBING SYSTEM
LEITUNGSSYSTEM FÜR FLUGZEUGBORDKÜCHE
SYSTÈME DE PLOMBERIE DE CUISINE D'AÉRONEF
2021-02-03
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |