A-5 低カロリーガス対応マイクロガスタービンの開発(マイクロガスタービン・燃焼器,一般講演)

• 金子 成彦

  東大院

書誌事項

タイトル別名

• A-5 Development of MGT fueled by low calorific gas

抄録

A two-axis, recuperated cycle micro-gas turbine (MGT) system for biomass gas is developed. The rated specifications of the MGT are as follows, pressure ratio of 2.7, turbine inlet temperature of 1120K, and output power of 5kW. The system consists of three components: the MGT power-generating system, control system and mock biomass gas supply system. Since the gaseous fuel converted from biomass has a low heat quantity, the combustor is designed to achieve both high combustion efficiency and low NOx emission for lower calorific fuel. In the combustor, a stable tubular flame combustion of city gas in the first stage supplies burned gas, which has enthalpy and activated radicals, to the second stage and enables stable ignition and combustion of biomass gas and air premixture. In addition, because the gas composition of biomass gas is also affected by the sources, the gasification method, and the gasifying condition, the system controller is required to absorb fuel fluctuation while meeting the demanded output. Hence, the H infinity algorithm is employed as a system controller because of its robustness against disturbances from the unpredictable fuel component fluctuation. Using this MGT system, an operation test was carried out with mock biomass gases. The rotational speed of the power turbine could be kept almost constant with both mock fermentation gas and pyrolysis gas as the second-stage fuel, and NOx emission was 50ppm when load was increased to a rated power of 5kW.

収録刊行物

• ガスタービン定期講演会講演論文集

  ガスタービン定期講演会講演論文集 (37), 37-41, 2009-10-21

  公益社団法人日本ガスタービン学会

キーワード

• Micro gas turbine
• Multi-stage combustor
• Flameless combustion
• Biomass gas
• H infinity control

詳細情報

• CRID: 1570854177035215744
• NII論文ID: 110008901730
• NII書誌ID: AN10255898
• ISSN: 09191941
• 本文言語コード: ja
• データソース種別:
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