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    • 5. 发明专利
    • System and method of analyzing combustion condition
    • 分析燃烧条件的系统与方法
    • JP2005274108A
    • 2005-10-06
    • JP2004092459
    • 2004-03-26
    • Tokyo Gas Co Ltd東京瓦斯株式会社
    • MOGI TORU
    • F23N5/24F23N5/08F23N5/16
    • PROBLEM TO BE SOLVED: To provide a system and a method of analyzing combustion condition capable of detecting the generation of oscillating combustion in combustion equipment such as a boiler, a suction type water heating/cooling device and a water heater.
      SOLUTION: Combustion noise (fluctuation of pressure) and emission intensity fluctuation (fluctuation of heat generation) of flames burning in combustion equipment are measured at the same time, and relative function of both the two measurement values are analyzed to determine existence of combustion noise due to oscillating vibration and whether combustion condition is transferring condition, wherein probability of instability in combustion is high, or not.
      COPYRIGHT: (C)2006,JPO&NCIPI
    • 要解决的问题:提供一种能够检测在诸如锅炉,吸入式水加热/冷却装置和热水器的燃烧设备中产生振荡燃烧的燃烧条件的系统和方法。 解决方案:同时测量燃烧设备中燃烧的燃烧的燃烧噪声(压力波动)和发射强度波动(发热波动),并分析两个测量值的相对函数,以确定 由于振荡振动引起的燃烧噪声以及燃烧条件是否转移,其中燃烧不稳定的概率高或不高。 版权所有(C)2006,JPO&NCIPI
    • 6. 发明专利
    • Combustion vibration analysis method and its device, and analysis program using the same
    • 燃烧振动分析方法及其装置及其分析程序
    • JP2005048638A
    • 2005-02-24
    • JP2003205021
    • 2003-07-31
    • Tokyo Electric Power Co Inc:TheToshiba Corp東京電力株式会社株式会社東芝
    • TSUCHIYA TOSHIAKISHIODA KAZUNORIMAEDA FUKUOYAMANAKA CHIKAU
    • F02C9/00F23N5/16F23N5/24F23R3/00
    • PROBLEM TO BE SOLVED: To provide a combustion vibration analysis method and its device relating to combustion vibration control to be induced with pressure fluctuation in a combustion process in a combustor, and to provide a medium on which an analysis program is recorded for executing a computer using the analysis method.
      SOLUTION: The combustion chamber 13 is divided into a plurality of cavities which are connected together via communication pipes 29. A flame as a vibration exciting source is placed in at least one cavity 27 of the cavities to serve as a pressure source to be fluctuated in a vibration exciting frequency. A resonator 22 is installed via a throat in one cavity of the combustion chamber 13 divided into the plurality of cavities 27, 28. Combustion vibration to be excited as acoustic vibration in the combustion chamber 13 is represented by Helmholz vibration where pressure in the cavity and the resonator 22 and flow rates in the connection pipes and the throat are fluctuated in a certain frequency. In accordance with the sizes of the cavities 27, 28, the resonator 22, the communication pipes 29 and the throat, the frequency response property of the Helmholz vibration to the vibration exciting frequency of the pressure source is calculated to evaluate the vibration damping effect of the resonator 22 and derive the frequency response property of the pressure and the flow rates from numeric calculation.
      COPYRIGHT: (C)2005,JPO&NCIPI
    • 要解决的问题:提供一种燃烧振动分析方法及其与燃烧器中的燃烧过程中的压力波动引起的燃烧振动控制有关的装置,并且提供记录分析程序的介质, 使用分析方法执行计算机。 解决方案:燃烧室13被分成多个通过连通管29连接在一起的空腔。作为振动激励源的火焰被放置在空腔的至少一个空腔27中,用作压力源 在振动激励频率波动。 谐振器22通过喉部安装在燃烧室13的分成多个空腔27,28的一个腔中。作为燃烧室13中的声振动被激发的燃烧振动由Helmholz振动表示,其中空腔中的压力和 谐振器22和连接管和喉部中的流量在一定频率波动。 根据空腔27,28,谐振器22,连通管29和喉部的尺寸,计算出亥姆霍兹振动对压力源的振动激振频率的频率响应特性,以评估振动阻尼效应 谐振器22并且从数值计算得出压力和流速的频率响应特性。 版权所有(C)2005,JPO&NCIPI
    • 10. 发明专利
    • Gas turbine control device, gas turbine system, and gas turbine control method
    • 气体涡轮控制装置,气体涡轮机系统和气体涡轮机控制方法
    • JP2003314301A
    • 2003-11-06
    • JP2002121643
    • 2002-04-24
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • NOMURA MASUMITOYAMA KOZO
    • F02C9/00F02C9/16F02C9/28F23N5/16
    • PROBLEM TO BE SOLVED: To provide a gas turbine control device for suppressing combustion vibration generated in a gas turbine, and for improving combustion stability. SOLUTION: The gas turbine control device is provided with a frequency analyzing part 12 for analyzing a frequency of a pressure or a vibration of acceleration in a combustor of the gas turbine and outputting an analysis result for each frequency band which divides a result of a frequency analysis into a plurality of frequency bands, a combustion characteristic grasping part 23 for grasping a characteristic of the combustion vibration of the gas turbine on the basis of the analysis result for each frequency band and a process quantity of the gas turbine, and a control part 11 for controlling at least one of a flow rate of fuel or a flow rate of air supplied to the combustor on the basis of the characteristic of the combustion vibration grasped by the combustion characteristic grasping part. COPYRIGHT: (C)2004,JPO
    • 解决的问题:提供一种用于抑制在燃气轮机中产生的燃烧振动并提高燃烧稳定性的燃气轮机控制装置。 解决方案:燃气轮机控制装置设置有频率分析部分12,用于分析燃气轮机的燃烧器中的加速度的压力或振动的频率,并输出分割结果的每个频带的分析结果 对多个频带进行频率分析,根据各频带的分析结果和燃气轮机的处理量来掌握燃气轮机的燃烧振动特性的燃烧特性把持部23,以及 控制部11,其根据由燃烧特性把持部掌握的燃烧振动的特性来控制供给到燃烧器的燃料流量或空气流量中的至少一个。 版权所有(C)2004,JPO