Fuel pump vent drain system

Power plants – Combustion products used as motive fluid – With safety device

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F02G 300

Patent

active

045398097

ABSTRACT:
A novel drain system for venting excess fuel from the fuel pump of a jet engine, and particularly the augmenter pump of a jet engine afterburner, is described which comprises a drain line connected at a first end to the vent valve of the fuel pump and at a second end to the main fuel supply line for the engine, for draining the excess fuel from the pump to the main fuel line, a check valve in the drain line near the second end thereof for restricting fuel flow through the drain line in a direction from the first end to the second end, and a vent line having a restriction therein defining an orifice of predetermined size connecting the drain line to an overboard dump port open to ambient.

REFERENCES:
patent: 2712218 (1955-07-01), Ritter
patent: 2814931 (1957-12-01), Johnson
patent: 2865166 (1958-12-01), Holbrook
patent: 3128598 (1964-04-01), Gordon
patent: 3738107 (1973-06-01), Miller
patent: 3793838 (1974-02-01), Nash
patent: 3841089 (1974-10-01), Clark
patent: 4038817 (1977-08-01), Snow et al.
patent: 4066386 (1978-01-01), Johnson et al.
patent: 4206595 (1980-06-01), Cole
patent: 4423595 (1984-01-01), McLean

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