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    • 7. 发明授权
    • Tail pipe of gas turbine combustor and gas turbine combustor having the
same tail pipe
    • 具有相同尾管的燃气轮机燃烧器尾气管和燃气轮机燃烧器
    • US5983641A
    • 1999-11-16
    • US846579
    • 1997-04-30
    • Shigemi MandaiTetsuo GoraSatoshi TanimuraYoshichika Sato
    • Shigemi MandaiTetsuo GoraSatoshi TanimuraYoshichika Sato
    • F01D9/02F02C3/14F23R3/42
    • F01D9/023
    • In a tail pipe of gas turbine combustor, the portion just in front of the outlet 104 of tail pipe of gas turbine combustor has a shape such as to be inclined with respect to the axial direction so that the direction changes from the rearward direction to the direction toward the rear in the substantially axial direction, and at this portion, the position of center of curvature 103 in the axial direction on the rotor side lies on the upstream side from the position of center of curvature 102 on the casing side, a bent portion of tail pipe serves as a suction duct, and the occurrence of a negative pressure zone is prevented. Also, by using the tail pipe, a combustor inner tube or a burner provided on the upstream side of the tail pipe having a straight or substantially straight axis is disposed so that the axis of the combustion inner tube or the burner makes an angle with respect to the axis of the tail pipe in such a manner that combustion gas collides with the back side of the tail pipe.
    • 在燃气轮机燃烧器的尾管中,刚好在燃气轮机燃烧器尾管出口104前方的部分具有相对于轴向方向倾斜的形状,使得该方向从向后方向变为 在该部分上,转子侧轴向的曲率中心位置103位于壳体侧的曲率中心位置102的上游侧,弯曲的方向 尾管的一部分用作吸气管,并且防止了负压区的发生。 此外,通过使用尾管,设置在具有直的或基本上直的轴线的尾管的上游侧设置的燃烧器内管或燃烧器,使得燃烧内管或燃烧器的轴线相对于 以尾气管的轴线的方式使得燃烧气体与尾管的背面碰撞。