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    • 2. 发明公开
    • 가스 터빈 시스템에서 연료 성분의 변화를 보상하기 위한방법 및 장치
    • 用于补充燃气组合物在气体涡轮机系统中的变化的方法和装置
    • KR1020060096435A
    • 2006-09-11
    • KR1020067007616
    • 2004-10-11
    • 지멘스 악티엔게젤샤프트
    • 베렌브링크,페터블로메이어,말테
    • F02C9/34F02C9/26
    • F02C9/34F05D2270/08F05D2270/081
    • The invention relates to a method for compensating variations in fuel composition in a gas turbine system consisting of at least two parallel-operated burner stages, wherein the fuel supply to at least two of the burner stages is adjusted in response to variations in fuel composition, wherein the fuel split between the burner stages, i.e. the relative increase in speed of the fuel supplied to the burner stages, is adjusted to a target value or maintained at a target value during adjustment of the fuel supply. The target value can, for example, be a constant or a function of one or several variables. More particularly, the gas turbine system can comprise a pilot burner stage and a main burner stage. When the fuel supply is adjusted, the fuel split between the pilot burner stage and the main burner stage is adjusted to a target value or maintained at a target value.
    • 本发明涉及一种用于补偿由至少两个平行操作的燃烧器级构成的燃气轮机系统中的燃料组成变化的方法,其中至少两个燃烧器级的燃料供应是根据燃料组成的变化进行调整的, 其中在燃料级之间分配的燃料,即供应到燃烧器级的燃料的速度的相对增加在调节燃料供应期间被调整到目标值或维持在目标值。 例如,目标值可以是常数或一个或多个变量的函数。 更具体地,燃气轮机系统可以包括引燃燃烧器级和主燃烧器级。 当调节燃料供应时,将引燃燃烧器级和主燃烧器级之间的燃料分配调节到目标值或维持在目标值。