Systems and methods involving reduced thermo-acoustic coupling of gas turbine engine augmentors
A method for providing thermo-acoustic coupling of a gas turbine engine augmentor includes determining acoustic resonances and heat release phase relationships associated with the augmentor. A fuel injector of the augmentor is positioned at an axial position relative to a flame holder of the augmentor in response to the determined acoustic resonances and heat release phase relationships associated with the augmentor. Heat release and acoustic pressure oscillation cycles associated with the augmentor are out of phase by at least approximately 100 degrees.
1. A method for varying thermo-acoustic coupling of an augmentor of a gas turbine engine, comprising:
providing a fuel injector and a flame holder disposed along an axis;
positioning the fuel injector in a first axial position relative to the flame holder by mounting the fuel injector in the first axial position in the augmentor;
operating the gas turbine engine and determining an initial phase relationship between a pressure oscillation cycle of the augmentor and heat release cycle of the augmentor, wherein the initial phase relationship corresponds to the first axial position of the fuel injector relative to the flame holder;
repositioning the fuel injector to a second axial position by mounting the fuel injector in the second axial position in the augmentor, the second axial position being different than the first axial position and being relative to a flame holder of the augmentor, wherein the fuel injector is repositioned in response to the initial phase relationship, and wherein the fuel injector is repositioned to the second axial position in response to fuel delivery dynamic characteristics of the augmentor; and
controlling the fuel injector with a control system.
2. The method of claim 1 , wherein:
the fuel injector is one of multiple fuel injectors; and
the flame holder is one of multiple flame holders.
3. The method of claim 1 , wherein positioning the fuel injector in the first axial position relative to the flame holder is in response to modeling acoustic response and combustion response of an exhaust section over a plurality of augmentor operating parameters.
4. The method of claim 3 , wherein positioning the fuel injector in the first axial position relative to the flame holder is performed prior to testing the engine.
5. The method of claim 1 , wherein the heat release phase is varied in response to the control system.
6. The method of claim 5 , further comprising interfacing the control system with an electro-pneumatic valve to control fuel flow to the fuel injector.
7. The method of claim 2 , wherein the multiple of fuel injectors are arranged at different axial locations.
8. The method of claim 1 , further comprising cooling the fuel injector and the flame holder.
9. A method for varying thermo-acoustic coupling of an augmentor of a gas turbine engine, comprising:
providing a fuel injector and a flame holder disposed along an axis;
positioning the fuel injector in a first axial position relative to the flame holder by mounting the fuel injector in the first axial position in the augmentor;
operating the gas turbine engine and determining an initial phase relationship between a pressure oscillation cycle of the augmentor and heat release cycle of the augmentor, wherein the initial phase relationship corresponds to the first axial position of the fuel injector relative to the flame holder;
repositioning the fuel injector to a second axial position by mounting the fuel injector in the second axial position in the augmentor, the second axial position being different than the first axial position and being relative to the flame holder, wherein the fuel injector is repositioned in response to the initial phase relationship such that the heat release cycle and a flame pressure oscillation cycle are out of phase by at least approximately 100 degrees, the second axial position different than the first axial position; and
controlling the fuel injector with a control system.
10. The method of claim 9 , wherein the initial phase relationship corresponds to the flame pressure oscillation cycle out of phase by 45 degrees or less with the heat release cycle.
11. The method of claim 9 , wherein the fuel injector is axially further from the flame holder at the second axial position than at the first axial position.
12. The method of claim 9 , wherein the initial phase relationship is varied in response to the control system.
13. The method of claim 1 , wherein the fuel injector is a pressure-atomized fuel injector.
14. The method of claim 1 , wherein the augmentor includes phase delay behavior related to the turning and acceleration of fuel in the augmentor.
15. The method of claim 1 , wherein the distance between the first axial position and the second axial position is greater than 1 cm.