The present disclosure relates to a water supply system (100) for a plurality of water consumer units (11, 12) in an aircraft (1). The system comprises a main tank (110) configured to store a main supply of water, a main water pipe (120) connected to an outlet of the main tank, and a plurality of water networks (150, 152), each configured to conduct water from the main tank (110) to at least one of the plurality of water consumer units. The plurality of water consumer units is partitioned in a first group (11) of water consumer units (11a, 11b, 11c) and at least a second group (12) of water consumer units (12a, 12b, 12c, 12d). Each of the plurality of water networks (150, 152) comprises a conveying device (130, 132) configured to convey water to each water consumer unit (11a, 11b, 11c, 12a, 12b, 12c, 12d) of one of the groups. The water supply system further comprises a cross feed valve configured to fluidically connect or separate the plurality of water networks downstream of the conveying devices in the plurality of water networks.
WATER SUPPLY SYSTEM WITH CROSS-FEED LINK AND AIRCRAFT HAVING A WATER SUPPLY SYSTEM
RESEAU D'ALIMENTATION EN EAU COMPRENANT UNE CONDUITE D'INTERCOMMUNICATION ET AERONEF COMPRENANT UN RESEAU D'ALIMENTATION EN EAU
2024-04-27
Patent
Electronic Resource
English
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