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    Hydrogen Enriched Combustion Testing of Siemens Industrial SGT 400 at Atmospheric Conditions

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 002::page 21502
    Author:
    Lam, Kam
    ,
    Geipel, Philipp
    ,
    Larfeldt, Jenny
    DOI: 10.1115/1.4028209
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to further extend the turbine fuel flex capability, a test under atmospheric conditions of a fullscale SGT400 burner was performed to study the combustion behavior when operating on hydrogen enriched natural gas (NG). A high speed camera was installed in the rig to investigate the flame dynamics on different operation conditions. NOx emissions were measured for all presented conditions. The combustion system was instrumented with thermocouples on all the key locations to allow flame position monitoring and to avoid flame attachment on the hardware. Further measurements included static pressure probes to monitor combustor pressure drop. The test was conducted in a systematic matrix format to include the most important combustion parameters in order to identify their individual effects on the combustion behaviors. The quantity of hydrogen in natural gas, fuel split, air preheat temperature, air reference velocity and flame temperature were the combustion related variables studied in the presented test campaign. The volumetric hydrogen quantity could be increased to 30% maintaining stable operation for all measured conditions. Higher hydrogen contents up to 80 vol. % were reached without flash back tendency. A glowing spark igniter prevented testing at even higher hydrogen contents. Hydrogen enriched gas showed higher NOx emissions and improved blowout limit. Hydrogen blending in the fuel also reduced the combustor pressure drop, lowered the prechamber temperature and raised the pilot tip temperature.
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      Hydrogen Enriched Combustion Testing of Siemens Industrial SGT 400 at Atmospheric Conditions

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    http://yetl.yabesh.ir/yetl1/handle/yetl/157853
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    contributor authorLam, Kam
    contributor authorGeipel, Philipp
    contributor authorLarfeldt, Jenny
    date accessioned2017-05-09T01:17:28Z
    date available2017-05-09T01:17:28Z
    date issued2015
    identifier issn1528-8919
    identifier othergtp_137_02_021502.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/157853
    description abstractIn order to further extend the turbine fuel flex capability, a test under atmospheric conditions of a fullscale SGT400 burner was performed to study the combustion behavior when operating on hydrogen enriched natural gas (NG). A high speed camera was installed in the rig to investigate the flame dynamics on different operation conditions. NOx emissions were measured for all presented conditions. The combustion system was instrumented with thermocouples on all the key locations to allow flame position monitoring and to avoid flame attachment on the hardware. Further measurements included static pressure probes to monitor combustor pressure drop. The test was conducted in a systematic matrix format to include the most important combustion parameters in order to identify their individual effects on the combustion behaviors. The quantity of hydrogen in natural gas, fuel split, air preheat temperature, air reference velocity and flame temperature were the combustion related variables studied in the presented test campaign. The volumetric hydrogen quantity could be increased to 30% maintaining stable operation for all measured conditions. Higher hydrogen contents up to 80 vol. % were reached without flash back tendency. A glowing spark igniter prevented testing at even higher hydrogen contents. Hydrogen enriched gas showed higher NOx emissions and improved blowout limit. Hydrogen blending in the fuel also reduced the combustor pressure drop, lowered the prechamber temperature and raised the pilot tip temperature.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHydrogen Enriched Combustion Testing of Siemens Industrial SGT 400 at Atmospheric Conditions
    typeJournal Paper
    journal volume137
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4028209
    journal fristpage21502
    journal lastpage21502
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 002
    contenttypeFulltext
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