Assessment of Different Actuator Concepts for Acoustic Boundary Control of a Premixed CombustorSource: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 002::page 21502DOI: 10.1115/1.2969088Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In the design process, new burners are generally tested in combustion test rigs. With these experiments, computational fluid dynamics, and finite element calculations, the burners’ performance in the full-scale engine is sought to be predicted. Especially, information about the thermoacoustic behavior and the emissions is very important. As the thermoacoustics strongly depend on the acoustic boundary conditions of the system, it is obvious that test rig conditions should match or be close to those of the full-scale engine. This is, however, generally not the case. Hence, if the combustion process in the test rig is stable at certain operating conditions, it may show unfavorable dynamics at the same conditions in the engine. In previous works, the authors introduced an active control scheme, which is able to mimic almost arbitrary acoustic boundary conditions. Thus, the test rig properties can be tuned to correspond to those of the full-scale engine. The acoustic boundary conditions were manipulated using woofers. In the present study, proportional valves are investigated regarding their capabilities of being used in the control scheme. It is found that the test rig impedance can be tuned equally well. In contrast to the woofers, however, the valves could be used in industrial applications, as they are more robust and exhibit more control authority. Additionally, the control scheme is further developed and used to tune the test rig at discrete frequencies. This exhibits certain advantages compared with the case of control over a broad frequency band.
keyword(s): Combustion , Control equipment , Acoustics , Impedance (Electricity) , Reflectance , Waves , Actuators , Frequency , Boundary-value problems , Signals , Pressure AND Combustion chambers ,
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| contributor author | Mirko R. Bothien | |
| contributor author | Jonas P. Moeck | |
| contributor author | Christian Oliver Paschereit | |
| date accessioned | 2017-05-09T00:32:42Z | |
| date available | 2017-05-09T00:32:42Z | |
| date copyright | March, 2009 | |
| date issued | 2009 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-27059#021502_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/140493 | |
| description abstract | In the design process, new burners are generally tested in combustion test rigs. With these experiments, computational fluid dynamics, and finite element calculations, the burners’ performance in the full-scale engine is sought to be predicted. Especially, information about the thermoacoustic behavior and the emissions is very important. As the thermoacoustics strongly depend on the acoustic boundary conditions of the system, it is obvious that test rig conditions should match or be close to those of the full-scale engine. This is, however, generally not the case. Hence, if the combustion process in the test rig is stable at certain operating conditions, it may show unfavorable dynamics at the same conditions in the engine. In previous works, the authors introduced an active control scheme, which is able to mimic almost arbitrary acoustic boundary conditions. Thus, the test rig properties can be tuned to correspond to those of the full-scale engine. The acoustic boundary conditions were manipulated using woofers. In the present study, proportional valves are investigated regarding their capabilities of being used in the control scheme. It is found that the test rig impedance can be tuned equally well. In contrast to the woofers, however, the valves could be used in industrial applications, as they are more robust and exhibit more control authority. Additionally, the control scheme is further developed and used to tune the test rig at discrete frequencies. This exhibits certain advantages compared with the case of control over a broad frequency band. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Assessment of Different Actuator Concepts for Acoustic Boundary Control of a Premixed Combustor | |
| type | Journal Paper | |
| journal volume | 131 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2969088 | |
| journal fristpage | 21502 | |
| identifier eissn | 0742-4795 | |
| keywords | Combustion | |
| keywords | Control equipment | |
| keywords | Acoustics | |
| keywords | Impedance (Electricity) | |
| keywords | Reflectance | |
| keywords | Waves | |
| keywords | Actuators | |
| keywords | Frequency | |
| keywords | Boundary-value problems | |
| keywords | Signals | |
| keywords | Pressure AND Combustion chambers | |
| tree | Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 002 | |
| contenttype | Fulltext |