Liquid feed systems, in particular for fuel for aeronautical eng

Fluid handling – Diverse fluid containing pressure systems – Fluid separating traps or vents

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55182, F16T 100

Patent

active

045805911

ABSTRACT:
An air arrester device that can be connected into the fuel line of an airplane to interrupt the passage of a bubble of air moving through the fuel line, the device including a vertically oriented elongated container which includes an inlet duct connected to its lower end and an outlet duct which extends downwardly through its upper end and into the interior of the container, the outlet duct including at least one intake port located at about half way along the length of the container to enable fuel in the container to flow into the outlet duct and upwardly out of the container. Under negative G conditions an air bubble which has passed into the container via the inlet duct will be located below the intake ports while under normal conditions it will be located above the intake ports.

REFERENCES:
patent: 1364770 (1921-01-01), Lindberg
patent: 2860648 (1958-11-01), Harrison
patent: 3130022 (1964-04-01), Clark
patent: 3833013 (1974-09-01), Leonard
patent: 3933448 (1976-01-01), Di Peri
patent: 4243065 (1981-01-01), Garrett
patent: 4388944 (1983-06-01), Honma et al.

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