• Title/Summary/Keyword: DLN Combustor

Search Result 13, Processing Time 0.016 seconds

Hydrogen Enriched Gas Turbine: Core Technologies and R&D Trend (수소혼소용 가스터빈의 요소기술 및 국내외 기술개발 동향)

  • JOO, YONGJIN;KIM, MIYEONG;PARK, JUNGKEUK;PARK, SEIK;SHIN, JUGON
    • Transactions of the Korean hydrogen and new energy society
    • /
    • v.31 no.4
    • /
    • pp.351-362
    • /
    • 2020
  • Recently, renewable power is rapidly increasing globally due to extensive effort to mitigate climate change and conventional power generation industry faces new challenges. The gas turbine technology has potentials to expand its role in future power generation based on the intrinsic characteristics such as fuel diversity and fast load following ability. Hydrogen is one of the most promising fuel in terms of reducing emissions and storing variable renewable energy and replacing hydrocarbon fuel with hydrogen has become very popular. Therefore, this paper presents the core technologies to combust hydrogen added fuel efficiently in gas turbines and the analysis of domestic and international R&D trends.

Stabilization of Abnormal Combustion of Dry Low NOx Gas Turbine Combustor for Power Generation (발전용 저 NOx 가스터빈의 연소 불안정 안정화에 관한 연구)

  • 정재모;안달홍;박정규
    • Journal of Energy Engineering
    • /
    • v.13 no.2
    • /
    • pp.144-151
    • /
    • 2004
  • Stabilization and reduction of combustion noise and NOx emission from dry low NOx combustor of GE MS7001F gas turbine were achieved. Dry low NOx gas turbines that adopt the lean premixed combustion technology frequently generate the flame instability and high NOx emissions if not adequately tuned. Dynamic pressure oscillation during the combustion mode transfer increased as ambient temperature decreased with frequency of 80㎐ and magnitude of 4-9 psi. Effects of both combustor tuning for uniform fuel flow with burner nozzles and fuel pre-filling into transfer fuel valves on stabilisation of the dry low NOx combustor were very significant. Dynamic pressure oscillation during the combustion mode change was decreased up to 2.5 psi. Also, NOx emission from GE7F DLN-1 combustor can be maintained as low as 35-43ppm (15% O$_2$) in base load operation of 150 MW.

A Study on NOx Emission Characteristics of An Industrial Gas Turbine (산업용 가스터빈의 NOx 배출 특성에 관한 연구)

  • Jeong, Jai-Mo;Park, Jung-Kyu
    • Journal of the Korean Society of Combustion
    • /
    • v.9 no.1
    • /
    • pp.11-17
    • /
    • 2004
  • The purposes of this study are to analyze nitrogen oxides(NOx) formation mechanism and to reduce abnormal NOx emissions in gas turbines. Industrial gas turbines emissions have potential to negative affect to the atmosphere in many different ways such as photochemical smog, acid rain and global warming. In conventional gas turbine combustors, one of the main pollutants such as nitrogen oxide(NOx) species, are principally formed from combustion process of fuel with oxygen in the primary combustion zone, and their emission levels are highly depend on peak temperatures in the combustor. In order to examine the characteristics and the effect of NOx formation, we used gas turbine of which commercial operating in Korea. From the examination, it has been found that NOx emissions are relatively high at low load(output) and during combustion mode change. Also, the effect of Air/Fuel ratio was considered. As the Air/Fuel ratio was increased in Lean-Lean mode, the NOx emission was decreased. The results of this study indicated that NOx emission levels are highly depend on peak temperature and pressure of combustion process in the combustor.

  • PDF