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contributor authorMirko R. Bothien
contributor authorJonas P. Moeck
contributor authorChristian Oliver Paschereit
date accessioned2017-05-09T00:32:42Z
date available2017-05-09T00:32:42Z
date copyrightMarch, 2009
date issued2009
identifier issn1528-8919
identifier otherJETPEZ-27059#021502_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/140493
description abstractIn 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleAssessment of Different Actuator Concepts for Acoustic Boundary Control of a Premixed Combustor
typeJournal Paper
journal volume131
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2969088
journal fristpage21502
identifier eissn0742-4795
keywordsCombustion
keywordsControl equipment
keywordsAcoustics
keywordsImpedance (Electricity)
keywordsReflectance
keywordsWaves
keywordsActuators
keywordsFrequency
keywordsBoundary-value problems
keywordsSignals
keywordsPressure AND Combustion chambers
treeJournal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 002
contenttypeFulltext


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