SYSTEM AND METHOD FOR GENERATING ELECTRIC ENERGY
    4.
    发明申请
    SYSTEM AND METHOD FOR GENERATING ELECTRIC ENERGY 有权
    用于产生电能的系统和方法

    公开(公告)号:US20150260053A1

    公开(公告)日:2015-09-17

    申请号:US14418066

    申请日:2013-07-29

    申请人: FINNO ENERGY OY

    发明人: Timo Erämaa

    摘要: An object of the present invention is to provide a method and a system for implementing the method so as to alleviate the disadvantages of a reciprocating combustion engine and gas turbine in electric energy production. The invention is based on the idea of arranging a combustion chamber (10) outside a gas turbine (22) and providing compressed air to the combustion chamber (10) in order to carry out a combustion process in controlled and optimal conditions.

    摘要翻译: 本发明的目的是提供一种实现该方法的方法和系统,以减轻往复式内燃发动机和燃气轮机在电能生产中的缺点。 本发明基于将燃烧室(10)布置在燃气涡轮机(22)的外面并且向燃烧室(10)提供压缩空气以在受控和最佳条件下执行燃烧过程的想法。

    System and method for generating electric energy

    公开(公告)号:US10378437B2

    公开(公告)日:2019-08-13

    申请号:US15310231

    申请日:2015-05-20

    申请人: Finno Energy Oy

    摘要: An object of the present invention is to provide a method and a system for implementing the method so as to alleviate the disadvantages of a reciprocating combustion engine and gas turbine in electric energy production. The invention is based on the idea of arranging a combustion chamber (10) outside a turbine (22) and providing compressed air from serially connected compressors to the combustion chamber in order to carry out a combustion process supplemented with high pressure steam pulses. The combustion chamber (10) is arranged to receive compressed air from each compressing stage of the serially connected compressors (24) for gradually increasing the amount of compressed air in the combustion chamber (10).

    Intermittent injection system for a gas turbine combustor

    公开(公告)号:US11286866B2

    公开(公告)日:2022-03-29

    申请号:US16334313

    申请日:2017-09-13

    申请人: Finno Energy Oy

    IPC分类号: F02C9/26 F02C3/30 F02C5/00

    摘要: The gas turbine comprises a compressor, a combustor, and a turbine. The method comprises: compressing air with the compressor and feeding compressed air continuously to the combustor, feeding fuel to the combustor, continuously firing the mixture of fuel and gas in the combustor, feeding combustion gases from the combustor to the turbine, and supplying at least a portion of the total amount of fuel that is supplied to the combustor intermittently.