An aircraft water supply system (10) supplies water to a water discharge port (12) in an aircraft. A cold water flow path (16) supplies cold water to the water discharge port (12). A hot water flow path (18) supplies hot water to the water discharge port (12). A first control valve (30) adjusts the flow rate of cold water flowing through the cold water flow path (16). A second control valve (32) adjusts the flow rate of hot water flowing through the hot water flow path (18). A temperature sensor (36) detects the water temperature at any point up to the water discharge port (12). A flow control unit (40) controls the opening/closing state of the first control valve (30) and the second control valve (32) based on the water temperature detected by the temperature sensor (36).
HOT AND COLD WATER SUPPLY SYSTEM FOR AIRCRAFT
WARM- UND KALTWASSERVERSORGUNGSANLAGE FÜR FLUGZEUGE
SYSTÈME D'ALIMENTATION EN EAU CHAUDE ET FROIDE POUR AÉRONEF
2022-06-08
Patent
Electronic Resource
English
IPC: | F24D DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATING SYSTEMS , Haus- oder Raumheizungssysteme, z.B. Zentralheizungssysteme / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F24H FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, IN GENERAL , Erhitzer für flüssige oder gasförmige Stoffe, z.B. Wasser- oder Lufterhitzer mit Vorrichtungen zur Wärmeerzeugung, allgemein / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen |