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A platform for research: civil engineering, architecture and urbanism
WATER SUPPLY SYSTEM FOR USE IN AN AIRCRAFT AND A METHOD FOR PREVENTING FREEZING OF WATER LINES
A water supply system for use in an aircraft, and a method for preventing blockages in a water supply system in an aircraft. The system comprises a central water tank comprising a fluid inlet and a fluid outlet, a supply conduit for permitting fluid flow from the outlet of the central water tank to a user equipment. At least a section of the supply conduit is connected and thermally coupled to an aircraft air duct so as to enable a transfer of thermal energy to the supply conduit therefrom to maintain the temperature of the water in the supply conduit above the freezing temperature thereof.
WATER SUPPLY SYSTEM FOR USE IN AN AIRCRAFT AND A METHOD FOR PREVENTING FREEZING OF WATER LINES
A water supply system for use in an aircraft, and a method for preventing blockages in a water supply system in an aircraft. The system comprises a central water tank comprising a fluid inlet and a fluid outlet, a supply conduit for permitting fluid flow from the outlet of the central water tank to a user equipment. At least a section of the supply conduit is connected and thermally coupled to an aircraft air duct so as to enable a transfer of thermal energy to the supply conduit therefrom to maintain the temperature of the water in the supply conduit above the freezing temperature thereof.
WATER SUPPLY SYSTEM FOR USE IN AN AIRCRAFT AND A METHOD FOR PREVENTING FREEZING OF WATER LINES
HEGENBART MATTHIAS (author) / ALBERS FREDERIK (author)
2024-11-07
Patent
Electronic Resource
English
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