Fluidic control of fuel flow
View Patent ↗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.
1. A fluidic apparatus for modulating a rate of fluid fuel flowing from a fuel supply to a combustor of a gas turbine engine to attenuate vibration and noise in the combustor during combustion, comprising:
a) a fluidic oscillator device having a supply inlet passage in fluid communication with the fuel supply, a first outlet passage in fluid communication with the combustor, a second outlet passage, and a control inlet passage, all of the passages being in fluid communication with each other; and
b) a fluidic control arrangement, including a feedback line in fluid communication between the second outlet passage and the control inlet passage, for diverting at least a portion of the fuel supplied to the supply inlet passage alternately between the first and second outlet passages at an oscillation frequency determined at least in part by the feedback line.
2. The fluidic apparatus according to claim 1 , wherein the first and second outlet passages diverge away each other and meet the supply inlet passage at a common junction.
3. The fluidic apparatus according to claim 1 , wherein the arrangement diverts the fuel portion continuously between the first and second outlet passages at the oscillation frequency.
4. The fluidic apparatus according to claim 1 , wherein the feedback line includes means for introducing a time delay for the fuel portion diverted to the second outlet passage.
5. The fluidic apparatus according to claim 4 , wherein the time delay means includes at least one of a flow restrictor and a volume.
6. The fluidic apparatus according to claim 4 , wherein the time delay means includes means for adjusting the time delay to a desired value.
7. The fluidic apparatus according to claim 1 , wherein the fluidic oscillator device has an additional control inlet passage in fluid communication with all of the passages, and wherein the arrangement includes an additional feedback line in fluid communication between the first outlet passage and the additional control inlet passage and operative for introducing a time delay for the fuel portion diverted to the first outlet passage.
8. The fluidic apparatus according to claim 7 , wherein the additional feedback line includes at least one of a flow restrictor and a volume.
9. The fluidic apparatus according to claim 7 , wherein the time delay introduced by the additional feedback line is variable.
10. The fluidic apparatus according to claim 1 , wherein the fluidic oscillator device has an additional control inlet passage in fluid communication with all of the passages, and wherein the arrangement includes a bypass line in fluid communication between the supply inlet passage and the additional control inlet.
11. The fluidic apparatus according to claim 10 , wherein the bypass line includes at least one of a flow restrictor and a volume for introducing a time delay for the fuel portion flowing along the bypass line.
12. The fluidic apparatus according to claim 1 , wherein the arrangement includes a main bypass line connected between the fuel supply and the combustor to enable a remaining portion of the fuel to bypass the fluidic oscillator device.
13. The fluidic apparatus according to claim 12 , wherein the main bypass line includes at least one of a flow restrictor and a volume for introducing a time delay for the remaining portion of the fuel flowing along the main bypass line.
14. The fluidic apparatus according to claim 13 , wherein the time delay is variable.
15. The fluidic apparatus according to 12 , wherein the main bypass line is operative for controlling a proportion of the fuel that flows along the main bypass line.
16. A method of modulating a rate of fluid fuel flowing from a fuel supply to a combustor of a gas turbine engine to attenuate vibration and noise in the combustor during combustion, comprising the steps of:
a) connecting a supply inlet passage of a fluidic oscillator device to the fuel supply;
b) connecting a first outlet passage of the device to the combustor;
c) enabling fluid communication between the supply inlet passage and the first outlet passage, as well as to a second outlet passage and a control inlet passage of the device; and
d) diverting at least a portion of the fuel supplied to the supply inlet passage alternately between the first and second outlet passages at an oscillation frequency determined at least in part by a feedback line connected between the second outlet passage and the control inlet passage.
17. The method according to claim 16 , wherein the diverting step is performed continuously.
18. The method according to claim 16 , wherein the step of introducing a time delay in the feedback line.
19. The method according to claim 18 , and the step of adjusting the time delay in the feedback line.
20. The method according to claim 16 , and the step of bypassing the device by connecting a bypass line between the fuel supply and the combustor.