Aircraft comprising a high-pressure water supply and distribution system
AssigneeAirbus Operations GmbH
InventorsTim Lübbert, Axel Schreiner, Michael Rempe
Life of this patent
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AssigneeAirbus Operations GmbH
InventorsTim Lübbert, Axel Schreiner, Michael Rempe
Estimating the term…
An aircraft with a drinking water supply and distribution system including a water storage tank, a consumer equipment, a pressurizer, a pressure reducer and a conduit system connecting the drinking water storage tank to the consumer equipment via the pressurizer and supplying water from the at least one water storage tank to the at least one consumer equipment. The pressurizer pressurizes water in the conduit system with a peak pressure exceeding a supply water pressure threshold. The conduit system includes flexible conduits having a maximum internal diameter of less than 8 mm. The pressure reducer is provided for reducing the pressure of water supplied to the consumer equipment below a consumer water pressure threshold. The supply water pressure threshold exceeds the consumer water pressure threshold.
An aircraft with a drinking water supply and distribution system, the drinking water supply and distribution system comprising:
An aircraft with a drinking water supply and distribution system, the drinking water supply and distribution system comprising:
Dependencies are inferred from the claim text.