Fuel pulsation-suppression for gas turbine combustion system

Power plants – Combustion products used as motive fluid

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417540, F02C 722, F04B 1100

Patent

active

041854551

ABSTRACT:
Rupture of the transition piece in one or more combustors of a gas turbine, due to resonance at the transition piece natural modal frequency, is avoided by interconnecting pairs of fuel lines having sinusoidal fluctuations in fuel flow that are 180.degree. out of phase with each other through opposite ends of an accumulator containing a movable partition displaced according to relative pressure on either side of the partition.

REFERENCES:
patent: 1571781 (1926-02-01), Aldrich
patent: 1862823 (1932-06-01), Holveck
patent: 2474512 (1949-06-01), Bechtold et al.
patent: 3307492 (1967-03-01), Selwood et al.
patent: 3532029 (1970-10-01), Roschupkin et al.
patent: 4115041 (1978-09-01), Selwood

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