Disclosed embodiments are generally related to a combustor and a method as may be used in a turbine engine, such as a gas turbine engine, and, more particularly, to a combustor and a method involving burner mains configured to damp vibrational modes that can develop under high-frequency combustion dynamics.
A turbine engine, such as a gas turbine engine, comprises for example a compressor section, a combustor section and a turbine section. Intake air is compressed in the compressor section and then mixed with a fuel. The mixture is burned in the combustor section to produce a high-temperature and high-pressure working gas directed to the turbine section, where thermal energy is converted to mechanical energy.
During combustion of the mixture, relatively high-frequency thermo-acoustic oscillations can occur in the combustor as a consequence of normal operating conditions depending on fuel/air stoichiometry, total mass flow, and other operating conditions. These thermo-acoustic oscillations can lead to unacceptably high levels of pressure oscillations in the combustor that can result in mechanical and/or thermal fatigue to combustor hardware.
One known technique to mitigate such thermo-acoustic oscillations, involves use of Helmholtz-type resonators. See for example U.S. Pat. No. 7,080,514. Further techniques effective to reliably and cost-effectively mitigate such thermo-acoustic oscillations are desirable.
The inventors of the present invention have recognized certain issues that can arise in the context of some prior art combustors, as may be used in gas turbine engines. High-frequency combustion dynamics, as may comprise any of various acoustic vibrational modes—e.g., a transverse acoustic mode, where acoustic standing waves can propagate along a radial direction, a circumferential direction, or both radial and circumferential directions—can limit the operational envelope of the engine. In prior art combustors involving substantially symmetrical structures, the level of these vibrational modes may be exacerbated by coherent interaction of acoustic pressure oscillations and heat release oscillations (i.e., thermo-acoustic oscillations), and may result in degraded emissions performance of the combustor and may further lead to a shortened lifetime of the combustor hardware. In view of such a recognition, the present inventors propose an improved combustor and method involving burner mains (hereinafter just referred to as mains) configured to reliably and cost-effectively damp vibrational modes that can develop in the combustor. Structural asymmetries arranged in the mains are effective to reduce coherent interaction of such thermo-acoustic oscillations and, thus, effective to damp vibrational modes that can develop under the high-frequency combustion dynamics in the combustor.
In the following detailed description, various specific details are set forth in order to provide a thorough understanding of such embodiments. However, those skilled in the art will understand that embodiments of the present invention may be practiced without these specific details, that the present invention is not limited to the depicted embodiments, and that the present invention may be practiced in a variety of alternative embodiments. In other instances, methods, procedures, and components, which would be well-understood by one skilled in the art have not been described in detail to avoid unnecessary and burdensome explanation.
Furthermore, various operations may be described as multiple discrete steps performed in a manner that is helpful for understanding embodiments of the present invention. However, the order of description should not be construed as to imply that these operations need be performed in the order they are presented, nor that they are even order dependent, unless otherwise indicated. Moreover, repeated usage of the phrase “in one embodiment” does not necessarily refer to the same embodiment, although it may. It is noted that disclosed embodiments need not be construed as mutually exclusive embodiments, since aspects of such disclosed embodiments may be appropriately combined by one skilled in the art depending on the needs of a given application.
The terms “comprising”, “including”, “having”, and the like, as used in the present application, are intended to be synonymous unless otherwise indicated. Lastly, as used herein, the phrases “configured to” or “arranged to” embrace the concept that the feature preceding the phrases “configured to” or “arranged to” is intentionally and specifically designed or made to act or function in a specific way and should not be construed to mean that the feature just has a capability or suitability to act or function in the specified way, unless so indicated.
In accordance with aspects of the present invention, some of the plurality of mains (designated with the letter X) have a body having a different structural feature relative to the respective bodies of the remaining mains (not designated with any letter). The mains with the different structural feature can be selectively grouped in the carrier to form one or more sets of such mains effective to damp predefined vibrational modes in the combustor, such as without limitation, a 1R vibrational mode, as represented in the plot of pressure oscillations shown in
In one non-limiting embodiment, the annular arrangement of mains may comprise at least two concentric annuli of mains and the set of mains with the different structural feature may be a set grouped in the radially inner-most annulus of such at least two concentric annuli of mains, as illustrated in
As may be appreciated in
Without limitation,
As may be appreciated in
As a further non-limiting example,
While embodiments of the present disclosure have been disclosed in exemplary forms, it will be apparent to those skilled in the art that many modifications, additions, and deletions can be made therein without departing from the spirit and scope of the invention and its equivalents, as set forth in the following claims.
Filing Document | Filing Date | Country | Kind |
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PCT/US2014/059272 | 10/6/2014 | WO | 00 |