초록 ▼

Under certain conditions, the fuel delivery system can contribute to the formation of strong dynamic pressures in the combustor of a turbine engine. Embodiments of the invention provide a system for dynamically stiffening the fuel supply passage to suppress damaging combustion dynamics. To that end,

Under certain conditions, the fuel delivery system can contribute to the formation of strong dynamic pressures in the combustor of a turbine engine. Embodiments of the invention provide a system for dynamically stiffening the fuel supply passage to suppress damaging combustion dynamics. To that end, a Helmholtz resonator can be placed along and in branched relation to the fuel supply passage. The resonator can produce the effect of adding a pressure release opening at a selected location in the fuel line, causing a shift in the fuel line pressure wave pattern that blocks fuel flow fluctuations at the outlet of the fuel passage at the frequency of the oscillation. The pressure wave shift results in a shifting of the volume velocity wave pattern. Ideally, the resonator can be positioned along the flow path such that the volume velocity of the fuel at the fuel passage exit is minimized.

대표청구항 ▼

What is claimed is: 1. An acoustically stiffened fuel supply system for a turbine engine comprising: at least one turbine engine combustion chamber; a fuel supply passage for receiving a pressurized gas fuel therein, the passage having an outlet adapted to discharge fuel into the combustion chamber

What is claimed is: 1. An acoustically stiffened fuel supply system for a turbine engine comprising: at least one turbine engine combustion chamber; a fuel supply passage for receiving a pressurized gas fuel therein, the passage having an outlet adapted to discharge fuel into the combustion chamber, the fuel supply passage being defined at least in part by a t-shaped pipe having an open inlet end, an opposing open outlet end and an open branch end disposed therebetween, the t-shaped pipe having an internal passage, wherein the fuel in the passage has an associated volume velocity wave and an associated pressure wave, the pressure wave being substantially 90 degrees out of phase with the volume velocity wave; a plug having a plurality of openings therein, the plug being secured to the branch end so as to substantially close the open branch end, the plug including an inner surface and an outer surface, wherein the inner surface includes at least one baffle extending therefrom, whereby the baffle reduces grazing flow of fuel over the inner surface of the plug; and a housing enclosing at least a portion of the branch end so as to define a volume therebetween, wherein the openings permit fluid communication between the internal passage of the t-shaped pipe and the volume and wherein the openings are the only manner of fluid communication with the volume, whereby a resonator assembly is formed, wherein the resonator shifts the pressure wave in the fuel supply passage such that a pressure antinode occurs substantially at the outlet, whereby the volume velocity wave amplitude of the fuel is reduced at the passage outlet, such that the combustion oscillations in the combustor that are attributable to the fuel passage are suppressed. 2. The system of claim 1 wherein the fuel supply passage is defined by at least a fuel supply line and a fuel nozzle, wherein the fuel nozzle is located downstream of the fuel supply line and has a discharge face that defines the outlet of the fuel supply passage. 3. The system of claim 2 wherein the resonator assembly is provided between the fuel supply line and the fuel nozzle. 4. The system of claim 2 wherein the resonator assembly is located in the fuel supply line upstream of the fuel nozzle. 5. The system of claim 1 wherein the combustor is a diffusion-type combustor. 6. The system of claim 1 wherein at least a portion of the plug is received within the branch end. 7. The system of claim 1 wherein the volume velocity wave amplitude is reduced to substantially zero substantially at the outlet. 8. A resonator for a turbine engine fuel supply line comprising: a t-shaped pipe having opposing inlet and outlet ends and an open branch end disposed therebetween, the t-shaped pipe having an internal passage; a plug having a plurality of openings therein, the plug being secured to the branch end so as to substantially close the open branch end; and a housing enclosing at least a portion of the branch end so as to define a volume therebetween, wherein the openings in the plug permit fluid communication between the internal passage of the t-shaped pipe and the volume and wherein the openings are the only manner of fluid communication with the volume. 9. The resonator of claim 8 wherein the inlet and outlet ends are adapted for fluid connection to a fuel passage. 10. The resonator of claim 8 wherein at least a portion of the plug is received within the branch end. 11. The resonator of claim 8 wherein the plug includes an inner surface and an outer surface, wherein the inner surface includes at least one baffle extending therefrom, whereby the baffle reduces grazing flow over the inner surface of the plug. 12. The resonator of claim 11 wherein the openings in the plug are offset from the baffle. 13. The resonator of claim 8 wherein at least a portion of the housing is thermally insulated. 14. The resonator of claim 8 wherein the openings in the plug are configured to provide acoustic stiffening at a specified frequency. 15. The resonator of claim 8 wherein the branch end is substantially perpendicular to the inlet and outlet ends.