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    • 32. 发明专利
    • Combustor
    • COMBUSTOR
    • JPS5731714A
    • 1982-02-20
    • JP10375180
    • 1980-07-30
    • Hitachi Ltd
    • RIYOUDORI MICHIOSHINOZAKI TADASHIIWAI KAZUMIYAMAZAKI SHIGEYUKIMIMURA JITSUO
    • F23D11/00F23D11/44
    • PURPOSE: To impart a fast-heating characteristic at a firing and to improve a rising at the start of a heating operation in the combustor with a carburetor by a structure wherein a heavy heat pipe is arranged between a combustion chamber and the carburetor.
      CONSTITUTION: Between the combustion chamber 4 and the carburetor 7, a gravity type heat pipe 10 for heating a vaporization chamber 8 of the carburetor 7 is arranged. The heat pipe 10 is embedded at the horizontal part at the lower end into the lower part of a burner 5 in the combustion chamber 4 and at the rising part at the upper end into the carburetor 7. At the firing of the burner 5, a heater 9 of the carburetor 7 is supplied with electric power to heat the carburetor 7. In this instance, the carburetor 7 is separated from the side wall 1 of the combustion chamber 4 and a pipe 10 has only a small thickness and hence a small heat capacity. Further, the pipe 10 does not transmit the heat from the upper end to the lower end. Therefore, the heat generated by the heater 9 is not transmitted to the combustion chamber 4, whereas the vaporization chamber 8 reaches immediately a desired temperature. This produces the instant vaporization of a mixture of fuel and air upon being introduced into the vaporization chamber 8, and the vaporized mixture is then fed to the burner 5.
      COPYRIGHT: (C)1982,JPO&Japio
    • 目的:为了赋予燃烧时的快速加热特性,并且通过具有燃料室和化油器之间的重型热管的结构,通过化油器在燃烧器的加热运转开始时提高上升。 构成:在燃烧室4和化油器7之间配置有用于加热汽化器7的蒸发室8的重力式热管10。 热管10在下端的水平部分嵌入燃烧室4中的燃烧器5的下部,并且在上端的上升部分嵌入化油器7.在燃烧器5的点火时, 化油器7的加热器9被供给电力以加热化油器7.在这种情况下,化油器7与燃烧室4的侧壁1分离,管道10仅具有小的厚度,因此具有小的热量 容量。 此外,管道10不将热量从上端传递到下端。 因此,加热器9产生的热量不会传递到燃烧室4,而蒸发室8立即达到期望的温度。 这会在引入蒸发室8时产生燃料和空气的混合物的即时蒸发,然后将蒸发的混合物进料到燃烧器5。
    • 36. 发明专利
    • GAS TURBINE COMBUSTION EQUIPMENT
    • JPH09178185A
    • 1997-07-11
    • JP34031395
    • 1995-12-27
    • HITACHI LTD
    • KOIZUMI HIROMIIWAI KAZUMI
    • F02C7/22F23C1/08F23R3/12F23R3/28F23R3/36
    • PROBLEM TO BE SOLVED: To secure necessary air flow by branching a part of the air for combustion to supply to a combustor from a manifold arranged at the top part of a combustor barrel and by supplying it to the air swirling path of the pilot burner of a high calorie gas combustor. SOLUTION: Air flow 21 blasted from a compressor flows between a flow sleeve 2 and a liner 3. The air flow 22 is distributed as the air for combustion 24 that is supplied cooling the liner 3 and as swirler air 22 for the combustion of low calorie gas that is arranged for a fuel nozzle 4, and to the air path 23 for combustion of pilot burner through an air manifold 6 that is branched from the head part of the combustor barrel. High calorie gas 11 is supplied to the fuel nozzle 4, blown out and ignited inside the combustor. The air 23 equalized inside the manifold 6 is supplied to the air path 7 inside the fuel nozzle body 5 through a connecting pipe 8. At the exit part of the fuel nozzle 4, the air 23 is blown out as a swirling flow. Therefore, without the complexity of the structure of fuel nozzle, the quantity of the air is secured and the manufacturing cost is reduced drastically.