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HIGH PRESSURE WATER SUPPLY SYSTEM AND AIRCRAFT EQUIPPED WITH SUCH SYSTEM
A high pressure water supply system for an aircraft includes a main water supply tank, water consumers, pressurization units configured to convey water from the main water supply tank to the water consumers, and a controller. One pressurization unit of the pressurization units conveys water to a first subset of water consumers of the water consumers via a corresponding high pressure water supply line, and the controller is configured to control an output pressure of the one pressurization unit depending on a hydraulic resistance length of the high pressure water supply line.
HIGH PRESSURE WATER SUPPLY SYSTEM AND AIRCRAFT EQUIPPED WITH SUCH SYSTEM
A high pressure water supply system for an aircraft includes a main water supply tank, water consumers, pressurization units configured to convey water from the main water supply tank to the water consumers, and a controller. One pressurization unit of the pressurization units conveys water to a first subset of water consumers of the water consumers via a corresponding high pressure water supply line, and the controller is configured to control an output pressure of the one pressurization unit depending on a hydraulic resistance length of the high pressure water supply line.
HIGH PRESSURE WATER SUPPLY SYSTEM AND AIRCRAFT EQUIPPED WITH SUCH SYSTEM
SCHNEIDER FRANK (author) / MÜLLER HANNES (author) / SCHREINER AXEL (author) / ALBERS FREDERIK (author)
2024-12-26
Patent
Electronic Resource
English
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