A Micro Gas Turbine Based Test Rig for Educational PurposesSource: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 002::page 24502DOI: 10.1115/1.3157099Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The Thermochemical Power Group of the University of Genoa, Italy, has developed a new “Gas Turbine” laboratory to introduce undergraduate students to the Gas Turbines and Innovative Cycles course, and Ph.D.s to advanced experimental activities in the same field. In the laboratory a general-purpose experimental rig, based on a modified commercial 100 kW recuperated micro gas turbine, was installed and fully instrumented. One of the main objectives of the laboratory is to provide both students and researchers with several experimental possibilities to obtain data related to the gas turbine steady-state, transient, and dynamic performance, including the effect of interaction between the turbomachines (especially the compressor), and more complex innovative gas turbine cycle configurations, such as recuperated, humid air, and hybrid (with high temperature fuel cells). The facility was partially funded by two Integrated Projects of the EU VI Framework Program (Felicitas and LARGE-SOFC) and the Italian Government (PRIN project), and it was designed with a high flexibility approach including: flow control management, cogenerative and trigenerative applications, downstream compressor volume variation, grid-connected or stand-alone operations, recuperated or simple cycles, and room temperature control. The paper also shows, as an example of the possibilities offered by the rig, experimental data obtained by both Master and Ph.D. students. The tests presented here are essential for understanding commercial gas turbines and microturbine performance, control strategy development, and theoretical model validation.
keyword(s): Machinery , Compressors , Cycles , Students , Micro gas turbines , Vessels , Pipes , Gas turbines , Steady state , Control systems , Undergraduate students AND Microturbines ,
|
Show full item record
| contributor author | Mario L. Ferrari | |
| contributor author | Matteo Pascenti | |
| contributor author | Loredana Magistri | |
| contributor author | Aristide F. Massardo | |
| date accessioned | 2017-05-09T00:37:53Z | |
| date available | 2017-05-09T00:37:53Z | |
| date copyright | February, 2010 | |
| date issued | 2010 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-27094#024502_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/143288 | |
| description abstract | The Thermochemical Power Group of the University of Genoa, Italy, has developed a new “Gas Turbine” laboratory to introduce undergraduate students to the Gas Turbines and Innovative Cycles course, and Ph.D.s to advanced experimental activities in the same field. In the laboratory a general-purpose experimental rig, based on a modified commercial 100 kW recuperated micro gas turbine, was installed and fully instrumented. One of the main objectives of the laboratory is to provide both students and researchers with several experimental possibilities to obtain data related to the gas turbine steady-state, transient, and dynamic performance, including the effect of interaction between the turbomachines (especially the compressor), and more complex innovative gas turbine cycle configurations, such as recuperated, humid air, and hybrid (with high temperature fuel cells). The facility was partially funded by two Integrated Projects of the EU VI Framework Program (Felicitas and LARGE-SOFC) and the Italian Government (PRIN project), and it was designed with a high flexibility approach including: flow control management, cogenerative and trigenerative applications, downstream compressor volume variation, grid-connected or stand-alone operations, recuperated or simple cycles, and room temperature control. The paper also shows, as an example of the possibilities offered by the rig, experimental data obtained by both Master and Ph.D. students. The tests presented here are essential for understanding commercial gas turbines and microturbine performance, control strategy development, and theoretical model validation. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Micro Gas Turbine Based Test Rig for Educational Purposes | |
| type | Journal Paper | |
| journal volume | 132 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3157099 | |
| journal fristpage | 24502 | |
| identifier eissn | 0742-4795 | |
| keywords | Machinery | |
| keywords | Compressors | |
| keywords | Cycles | |
| keywords | Students | |
| keywords | Micro gas turbines | |
| keywords | Vessels | |
| keywords | Pipes | |
| keywords | Gas turbines | |
| keywords | Steady state | |
| keywords | Control systems | |
| keywords | Undergraduate students AND Microturbines | |
| tree | Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 002 | |
| contenttype | Fulltext |