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A combustor for a gas turbine engine and related method is provided in which a plurality of combustor cans are selectively adapted with corresponding resonators. The resonators may, for example, be attached to every can in the consecutive arrangement of combustor cans, every other can, every third c

A combustor for a gas turbine engine and related method is provided in which a plurality of combustor cans are selectively adapted with corresponding resonators. The resonators may, for example, be attached to every can in the consecutive arrangement of combustor cans, every other can, every third can or the like, and may be tuned to the same or first, second, third, etc. frequencies of operation. Such selective tuning is configured to suppress one or more of out-of-phase and in-phase dynamic interaction of streams discharged from adjacent combustor cans by changing the frequencies of pressure oscillation instabilities across the arrangement of consecutive cans.

대표청구항 ▼

1. A method for suppressing the dynamic interaction among combustor cans in a gas turbine combustion engine, said method comprising the steps of: providing a plurality of consecutively arranged combustor cans for generating respective streams of combustion gases therein and collectively discharging

1. A method for suppressing the dynamic interaction among combustor cans in a gas turbine combustion engine, said method comprising the steps of: providing a plurality of consecutively arranged combustor cans for generating respective streams of combustion gases therein and collectively discharging the streams of combustion gases, the combustor cans defining a first group and a second group;providing a plurality of resonators, a first plurality of resonators coupled to the first group of combustor cans in the plurality of consecutively arranged combustor cans and a second plurality of resonators coupled to the second group of combustor cans; andselectively tuning the first plurality of resonators to suppress oscillations at a first frequency and tuning the second plurality of resonators to suppress oscillations at a second frequency different from the first frequency, such that one or more of out-of-phase and in-phase dynamic interactions of the streams discharged from adjacent combustor cans in the plurality of consecutively arranged combustor cans are suppressed. 2. The method of claim 1, wherein the first group comprises a number of combustor cans equal to half the total number in the plurality of consecutively arranged combustor cans and corresponds to every other can in the consecutive arrangement, and wherein the second group comprises a number of combustor cans equal to half the total number in the plurality of consecutively arranged combustor cans and corresponds to the remaining combustor cans in the consecutive arrangement not in said first group. 3. The method of claim 1, wherein the number of combustor cans is one of six, twelve, eighteen, and twenty-four combustor cans. 4. A method for suppressing the dynamic interaction among combustor cans in a gas turbine combustion engine, said method comprising the steps of: providing a plurality consecutively arranged combustor can for generating respective streams of combustion gases therein and collectively discharging the streams of combustion gases;providing a plurality of resonators, wherein at least one resonator is coupled to selected combustor cans in the plurality of consecutively arranged combustor cans, the selected combustor cans consisting of every other combustor can in the plurality of consecutively arranged combustor cans; andselectively tuning the plurality of resonators to suppress one or more of out-of-phase and in-phase dynamic interactions of the streams discharged from adjacent combustor cans in the plurality of consecutively arranged combustor cans. 5. A method for suppressing the dynamic interaction among combustor cans in a gas turbine combustion engine, said method comprising the steps of: providing a plurality of consecutively arranged cans for generating respective streams of combustion gases therein and collectively discharging the streams of combustion gases;providing a plurality of resonators, wherein at least one resonator is coupled to selected combustor cans in the plurality of consecutively arranged combustor cans, the selected combustor cans consisting of d to every third combustor can in the plurality of consecutively arranged combustor cans; andselectively tuning the plurality of resonators to suppress one or more of out-of-phase and in-phase dynamic interactions of the streams discharged from adjacent combustor cans in the plurality consecutively arranged combustor cans.