On-board disposal of water in aircraft fuel tanks

Aeronautics and astronautics – Aircraft structure – Fuel supply

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B64D 3700

Patent

active

048099341

ABSTRACT:
An aircraft fuel system adapted for the automatic extraction and dispersion of entrapped puddles of water in an aircraft fuel tank as a function of fuel flow supply to at least one propulsion engine. Scavenge pipes, positioned to be immersed in the puddles at their inlet openings, are connected to a venturi located within a fuel supply duct and arranged such that fuel drawn through the duct by means of a jet pump induces water extraction by suction at the venturi throat which is subsequently broken up within the jet pump and dispersed in the fuel.

REFERENCES:
patent: 2547246 (1951-04-01), Aspelin
patent: 2953156 (1960-09-01), Bryant
patent: 2961130 (1960-11-01), Adams
patent: 3693915 (1972-09-01), Uranovsky
patent: 3963040 (1976-06-01), Gezari

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