BRENNERANORDNUNG FÜR EINE BRENNKAMMER, ZUGEHÖRIGE BRENNKAMMER SOWIE VERFAHREN ZUM VERBRENNEN EINES BRENNSTOFFS
    42.
    发明公开
    BRENNERANORDNUNG FÜR EINE BRENNKAMMER, ZUGEHÖRIGE BRENNKAMMER SOWIE VERFAHREN ZUM VERBRENNEN EINES BRENNSTOFFS 审中-公开
    FOR燃烧室,相关的燃烧室炉装置和方法燃料燃烧

    公开(公告)号:EP1926936A1

    公开(公告)日:2008-06-04

    申请号:EP06792956.2

    申请日:2006-08-23

    Inventor: KARL, Jürgen

    Abstract: The invention relates to a burner arrangement for a combustion chamber (12) in addition to an associated combustion chamber (12), in particular a gas turbine combustion chamber or a steam generator combustion chamber, comprising a plurality of burners (8), which are equipped for the combustion of fuel which contains carbon by supplying pure oxygen, which is effective as an oxidation agent. The aim of the invention is to obtain a burner arrangement which has a particularly high energetic degree of efficiency and particularly low residue emissions and at the same time maintains the construction and operation thereof simple and economical and reverts to suitable fuelling concepts. Also, the acceptable material temperatures of the encircling walls (6) surrounding the combustion chamber (12) must not be exceeded. The inventive first burner (8) is embodied in such a manner that the ratio (?), per time unit, of the amount of oxygen guided therein, in normal operation, for the stochiometrically required amount of oxygen is greater than for a second burner (8) which is arranged downstream from the direction of the flow of flue gas (14).

    Gas turbine combustion system
    45.
    发明专利
    Gas turbine combustion system 有权
    燃气涡轮机燃烧系统

    公开(公告)号:JP2014016146A

    公开(公告)日:2014-01-30

    申请号:JP2013143565

    申请日:2013-07-09

    Abstract: PROBLEM TO BE SOLVED: To enable operation with reduced CO emissions.SOLUTION: A gas turbine combustion system includes a gas turbine. The gas turbine includes: at least one compressor; at least one combustion chamber for generating working gas, which is connected to receive compressed air from the compressor; and at least one turbine connected to receive working gas from the combustion chamber. The combustion chamber consists of a single can-combustor or comprises a plurality of individual or interdependent can-combustors arranged in an annular can-architecture. The can-combustor has at least one premixed burner. The ignition of a mixture starts at the premixed burner outlet and the flame is stabilized in the region of the premixed burner outlet by means of a backflow zone. The can-combustor comprises a plurality of premixed burners arranged uniformly or is divided in at least two groups within the can-combustor.

    Abstract translation: 要解决的问题:使CO 2排放减少的操作。解决方案:燃气轮机燃烧系统包括燃气轮机。 燃气轮机包括:至少一个压缩机; 用于产生工作气体的至少一个燃烧室,其被连接以从压缩机接收压缩空气; 以及至少一个涡轮连接以从燃烧室接收工作气体。 燃烧室由单个罐式燃烧器组成,或包括多个单独的或相互依赖的罐式燃烧器,它们以环形罐结构布置。 罐式燃烧器具有至少一个预混燃烧器。 混合物的点燃从预混燃烧器出口开始,并且通过回流区在火焰稳定在预混燃烧器出口的区域。 罐式燃烧器包括均匀排列的多个预混燃烧器,或者在罐式燃烧器内分成至少两组。

    가스터빈 연소 시스템
    46.
    发明公开
    가스터빈 연소 시스템 有权
    燃气涡轮机燃烧系统

    公开(公告)号:KR1020140007286A

    公开(公告)日:2014-01-17

    申请号:KR1020130079571

    申请日:2013-07-08

    Abstract: The present invention relates to a gas turbine combustion system, wherein a gas turbine comprises at least one compressor, at least one combustion chamber for generating working gas, wherein at least one combustion chamber is connected to receive compressed air from the compressor, and at least one turbine connected to receive the working gas from the combustion chamber. The combustion chamber consists of an individual can-combustor or comprising a plurality of can-combustors arranged in an annular can-architecture, wherein the can-combustor having at least one premixed burner. The ignition of a mixture starts at a premixed burner outlet and the flame is stabilized in a region of the premixed burner outlet by means of a backflow zone. The can-combustor comprises a plurality of premixed burners arranged uniformly or divided at least in two groups within the can-combustor.

    Abstract translation: 燃气轮机燃烧系统技术领域本发明涉及一种燃气轮机燃烧系统,其中燃气轮机包括至少一个压缩机,至少一个用于产生工作气体的燃烧室,其中至少一个燃烧室被连接以从压缩机接收压缩空气,并且至少 一个涡轮连接以从燃烧室接收工作气体。 燃烧室由单独的罐式燃烧器组成或包括以环形罐结构布置的多个罐式燃烧器,其中罐式燃烧器具有至少一个预混燃烧器。 混合物的点火开始于预混燃烧器出口,并且火焰通过回流区稳定在预混燃烧器出口的区域中。 罐式燃烧器包括多个预混合燃烧器,其均匀地排列或者在罐内燃烧器内至少分成两组。

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