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    • 81. 发明专利
    • Injection nozzle for turbomachine
    • 喷油嘴注射喷嘴
    • JP2012017971A
    • 2012-01-26
    • JP2011147836
    • 2011-07-04
    • General Electric Co ゼネラル・エレクトリック・カンパニイ
    • UHM JONG HOJOHNSON THOMAS EKIM KWANWOO
    • F23R3/28F23R3/10F23R3/32
    • F23R3/28F23D14/62F23D14/82F23G2900/54402F23R2900/00002
    • PROBLEM TO BE SOLVED: To provide an injection nozzle for a turbomachine.SOLUTION: The injection nozzle assemblies (38, 39, 40) operably connected with a combustor (6) of a turbomachine (2) includes a first end portion (80) that extends to second end portions (82, 166, 224, 324), and a plurality of tube elements (90, 175, 230, 330) provided at the second end portions (82, 166, 224, 324). Each of the plurality of tube elements (90, 175, 230, 330) defining a fluid passage includes a body having first end sections (132, 198, 244, 344) that extend to second end section (134, 200, 245, 345). The second end sections (134, 200, 245, 345) project beyond the second end portions (82, 166, 224, 324) of the injection nozzle assemblies (38, 39, 40).
    • 要解决的问题:提供一种用于涡轮机的喷嘴。 解决方案:与涡轮机(2)的燃烧器(6)可操作地连接的喷嘴组件(38,39,40)包括延伸到第二端部(82,166,224)的第一端部(80) ,324)和设置在第二端部(82,166,224,324)处的多个管元件(90,175,230,330)。 限定流体通道的多个管元件(90,175,230,330)中的每一个包括具有延伸到第二端部(134,200,245,345)的第一端部段(132,198,244,344)的主体, )。 第二端部段(134,200,455,345)突出超过喷嘴组件(38,39,40)的第二端部部分(82,166,224,324)。 版权所有(C)2012,JPO&INPIT
    • 88. 发明授权
    • Rotary furnace burner
    • 旋转炉燃烧器
    • US08393893B2
    • 2013-03-12
    • US12520661
    • 2007-12-20
    • Ernst SchröderAlexander Knoch
    • Ernst SchröderAlexander Knoch
    • F24D17/01F24C6/04F23G7/12F23G5/20
    • F23D1/00F23C6/047F23D17/00F23D2201/10F23G5/20F23G7/12F23G2900/54402
    • In order to provide a rotary-furnace burner in which the quantity fraction of cost-effective particulate secondary fuels to be used as energy carriers can be increased and the configuration of the burner flame can be influenced, even during the operation of the burner, it is proposed, according to the invention, to arrange an expansion chamber open towards the burner mouth and having a widened cross section, as compared with the tube or individual tubes in the burner in front of the issue of the tube or tubes for blowing out the secondary fuels, and to make the axial length and the volume of the expansion chamber variable, during the operation of the burner, by means of the axial displacement of the secondary-fuel tubes, so that the particulate secondary fuel particles blown out at the burner mouth with a considerably reduced velocity do not fly past the burner flame, but, instead, burn out in the flame.
    • 为了提供一种旋转炉燃烧器,其中可以增加用作能量载体的成本有效的颗粒二次燃料的数量分数,并且即使在燃烧器的操作期间也可以影响燃烧器火焰的构造, 根据本发明,提出了一种膨胀室,其朝向燃烧器口敞开并具有加宽的横截面,与管或管的前面的管或各个管相比,用于吹出 二次燃料,并且通过辅助燃料管的轴向位移,在燃烧器的操作期间使膨胀室的轴向长度和体积可变,使得在燃烧器处吹出的颗粒二次燃料颗粒 嘴巴速度明显降低,不能飞过燃烧器火焰,而是在火焰中燃烧。