Fuel nozzle assembly with integral valve assembly and inlet wash

Fluid handling – With means for separating solid material from the fluid – Hollow strainer – fluid inlet and outlet perpendicular to...

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2104331, 239112, 239113, B01D 3502

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active

046499504

ABSTRACT:
A fuel nozzle assembly with integral valve for a gas turbine engine includes an inlet fitting with a tubular wash-type fuel filter therein between a central fuel passage and an annular primary fuel manifold therearound to filter primary fuel flowing through the passage to the annular primary fuel manifold chamber on the inlet fitting. The manifold chamber is in fuel flow relation in the valve housing with a primary fuel take-off passage therein for providing primary fuel flow to a fuel nozzle.

REFERENCES:
patent: 2757800 (1956-08-01), Kucera
patent: 3129891 (1964-04-01), Vdoviak
patent: 3154095 (1964-10-01), Cleminshaw et al.
patent: 3794179 (1974-02-01), Doucet
patent: 4491272 (1985-01-01), Bradley et al.

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