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    • 9. 发明申请
    • FUEL NOZZLE HAVING A SWIRL DUCT AND METHOD FOR PRODUCING A FUEL NOZZLE
    • 燃油喷嘴涡流导道和方法生产燃料喷嘴
    • WO2009095100A3
    • 2010-05-27
    • PCT/EP2008065135
    • 2008-11-07
    • SIEMENS AGKRIEGER TOBIASPFEIFFER ELMAR
    • KRIEGER TOBIASPFEIFFER ELMAR
    • F23D11/10
    • F23D11/107
    • The invention relates to a method for producing a fuel nozzle (1), wherein at least one swirl duct (4) is mounted in an outer jacket surface (5) of a pin (3) and/or in an inner surface (6) of a sleeve (2), and the pin (3) is attached in the sleeve (2) so that the outer jacket surface (5) of the pin (3) is connected to the inner surface (6) of the sleeve (2). The invention further relates to a fuel nozzle (1) comprising a pin (3) having an outer jacket surface (5) and a sleeve (2) having an inner surface (6), wherein the pin (3) is disposed in the sleeve (2). The outer jacket surface (5) of the pin (3) and/or the inner surface (6) of the sleeve (2) comprises at least one swirl duct (4). A burner (107) is further disclosed, comprising a fuel nozzle (1) according to the invention. A gas turbine (100) is further disclosed, comprising a burner (107) according to the invention.
    • 提供了一种方法,用于制造燃料喷嘴(1)是可用的,其引入的至少一个涡流管(4)中的外侧面(5)的销(3)和/或在其内表面(6)的套筒(2)的 是和在套筒(2)的销(3)被安装为使得所述外侧面(5)的销(3)与内表面(6)的套(2)相连。 另外,一个燃料喷嘴(1)中所描述的是一个销(3)具有外套表面(5)和(2)具有内表面的套筒(6),其中,所述销(3)在所述套筒(2) 布置。 所述外部侧面(5)的销(3)和/或内表面(6)的套筒(2)包括至少一个涡流管(4)。 此外,燃烧器(107)根据本发明(1)中所公开的燃料喷嘴。 此外,燃气涡轮机(100)中描述,其包括根据本发明(107)的燃烧器。
    • 10. 发明申请
    • METHOD FOR MONITORING THE OPERATION OF A GAS TURBINE
    • 方法燃气涡轮机的监视运行
    • WO2014032875A2
    • 2014-03-06
    • PCT/EP2013065732
    • 2013-07-25
    • SIEMENS AG
    • BOETTCHER ANDREASKAUFMANN PETERKRIEGER TOBIASVAN KAMPEN JAAP
    • G01H1/00
    • G01M15/14G01H1/003G01H17/00
    • The invention relates to a method for monitoring the operation of a gas turbine 10, in which component vibrations are detected during the operation of the gas turbine 10 by an acceleration sensor 40 arranged on the component, a plurality of signal sections being determined by means of a plurality of frequency bands fb from the signal 39 forwarded and processed by the acceleration sensor 40. To avoid an unnecessary shutdown of the gas turbine 10 to perform an inspection which subsequently proves unnecessary, thereby increasing the availability of the gas turbine 10, the invention proposes determining a total vibration period by adding together the vibration periods of signal sections during which the amplitudes of the signal sections concerned are greater than a frequency band-specific threshold.
    • 一种用于监控燃气轮机本发明涉及一种用于监视燃气涡轮机10的操作的方法,其中,10次部件的振动是由设置在所述燃气轮机的操作期间的成分加速度传感器40检测出的操作方法,以及中继和从加速度传感器40调节后的信号的 39通过多个频带fb的手段被确定的多个信号部分。 到燃气涡轮机10用于执行不必要的事后检查,以避免,从而增加燃气涡轮机10的可用性的不必要的停机,所以建议振荡的整体周期由信号部分的那些振荡周期的总和,在此期间,各信号部分的幅度大于确定 是作为频带指定的限制。