Fuel pulsation-suppression for gas turbine combustion system

Details Fuel pulsation-suppression for gas turbine combustion system Fuel pulsation-suppression for gas turbine combustion system

F - Mech Eng,Light,Heat,Weapons

02

C

60/164, 60/176

F02C 7/22 (2006.01)

Patent

CA 1124089

ABSTRACT OF THE DISCLOSURE 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° 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.

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