Volume 30 Issue 9
Sep.  2015
Turn off MathJax
Article Contents
WEI Shu-ming, SUO Jian-qin. Aero-derivative industrial gas turbine dual fuel lean premixed low emission combustion technology[J]. Journal of Aerospace Power, 2015, 30(9): 2049-2057. doi: 10.13224/j.cnki.jasp.2015.09.001
Citation: WEI Shu-ming, SUO Jian-qin. Aero-derivative industrial gas turbine dual fuel lean premixed low emission combustion technology[J]. Journal of Aerospace Power, 2015, 30(9): 2049-2057. doi: 10.13224/j.cnki.jasp.2015.09.001

Aero-derivative industrial gas turbine dual fuel lean premixed low emission combustion technology

doi: 10.13224/j.cnki.jasp.2015.09.001
  • Received Date: 2014-05-28
  • Publish Date: 2015-09-28
  • Development of aero-derivative gas turbine dual fuel low emission combustion technology was studied, and major technical approaches to the success of the development were summarized. Range of fuel-air ratio of dual fuel combustor, effect of fuel-air ratio on CO and NOx emission, and design of transition operation were discussed; considerations in designing dual fuel low emission combustion were summarized comprehensively. By study of a variety of dual fuel lean premixed fuel-air modules, as well as long-term and lasting research and development on combustion test, the result shows that, the designed dual fuel combustion can meet the requirements of low pollution in the range of 50%-100% operation, and such low emission combustion technology and design of transient operation are practicable and can be directly used into the typical product of aero-engine.

     

  • loading
  • [1]
    金如山.航空燃气轮机燃烧室[M].北京:宇航出版社,1988.
    [2]
    Lefebvre A H,Ballal D R.Gas turbine combustion[M].Boca Raton,Florida:The Chemical Rubber Company,1999.
    [3]
    金如山,索建秦.民用飞机低污染发动机研发策略[R].贵阳:中国航空学会第七届动力年会,2010.
    [4]
    金如山.某国航空发动机研发体系[R].贵阳:中国航空学会第七届动力年会,2010.
    [5]
    金如山.发动机独立自主研发体系的建设[R].贵阳:中国航空学会第七届动力年会,2010.
    [6]
    张川,索建秦,金如山.民用飞机低污染燃烧室的技术成熟度划分[J].航空工程进展,2010,1(1):85-89. ZHANG Chuan,SUO Jianqin,JIN Rushan.Technology readiness level scale for low emission combustor of civil aircraft[J].Advances in Aeronautical Science and Engineering,2010,1(1):85-89.(in Chinese)
    [7]
    Klein S,Austrem I,Mowill J.The development of an ultra low emissions liquid fuel combustor for the OPRA OP16 gas turbine[R].ASME Paper GT-2002-30107,2002.
    [8]
    Ichira F.Development of a gas turbine lean-premixed low-NOx combustor for cogeneration systems with variable heat-powerratio[R].London,UK:Energy Technology Research Institute Annual Technical Report Digest No.8,1998.
    [9]
    Røkke P E,Hustad J E,Røkke N A.Technology update on gas turbine dual fuel dry low emission combustion systems[R].ASME Paper GT2003-38112,2003.
    [10]
    Stegmair L J.Development of an aero-derivative gas turbine dry low emissions combustion system trans.of the ASME[J].Journal of Engineering for Gas Turbine and Power,1994,16(3):542-546.
    [11]
    International Civil Aviation Organization.International standards and recommended practices[M].Montreal,Canada:International Civil Aviation Organization,2013.
    [12]
    中国民用航空管理局.CCAR-34涡轮发动机飞机燃油排泄和排气排出物规定[S].北京:中国民用航空总局,2002.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1193) PDF downloads(808) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return