Fluidic control of fuel flow

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S039281

Reexamination Certificate

active

06895758

ABSTRACT:
A fluidic apparatus for modulating the rate of fuel flow into the combustor of a gas turbine engine. The apparatus includes a fluidic oscillator device (preferably an astable fluidic oscillator, or “flip-flop”) having a supply inlet connected to a fluid fuel source and a pair of outlets one of which is connected to the combustor. The fluidic device operates to output fluid fuel from the outlets alternately, so modulating fuel flow into the combustor.

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patent: 5938421 (1999-08-01), George, II
patent: 6343927 (2002-02-01), Eroglu et al.
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patent: 0 672 862 (1995-01-01), None
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patent: 1 439 918 (1973-07-01), None
patent: 2 202 000 (1988-09-01), None
patent: 2 279 764 (1995-01-01), None

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