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    • 1. 发明申请
    • METHOD AND APPARATUS FOR REDUCING TOTAL PRESSURE LOSS IN A TURBINE ENGINE
    • 减少涡轮发动机总压损失的方法和装置
    • WO2004106717A3
    • 2005-06-02
    • PCT/US2004014536
    • 2004-05-28
    • COMBUSTION SCI & ENG INCHAMMER ANDREW JBATTAGLIOLI JOHN L
    • HAMMER ANDREW JBATTAGLIOLI JOHN L
    • F01D25/30
    • F01D25/30
    • A method and apparatus for reducing total pressure loss in the exhaust of a combustion device via an axial diffuser having no turning vanes, support struts, rods, or other obstructions to exhaust flow. The axial diffuser includes an inner wall and an outer wall each having a turn radius and forming an annular cross section having increasing cross-sectional area in the downstream direction of flow, the flow being transitioned from axial to radial direction thereby. The diffuser is supported in the plenum by rods, struts or a cradle; from a stand surrounding the axial diffuser via struts or rods; or from existing diffuser support structure by web stiffeners. The diffuser flow path turn radius of the outer wall ranges from about 50-95% of the radial distance from the inner wall to a wall of the exhaust plenum, and of the inner wall ranges from about 10-70% of this distance.
    • 一种用于通过轴向扩散器减少燃烧装置的排气中的总压力损失的方法和装置,所述轴向扩散器没有转动叶片,支撑支柱,杆或其它阻碍物排出流动。 轴向扩散器包括内壁和外壁,每个外壁具有转弯半径并且形成具有在下游流动方向上具有增加的横截面面积的环形横截面,该流动从轴向向径向过渡。 扩散器通过杆,支柱或支架支撑在增压室中; 通过支柱或杆从围绕轴向扩散器的支架上; 或通过腹板加强件从现有的扩散器支撑结构。 外壁的扩散器流路转弯半径在从内壁到排气室的壁的径向距离的约50-95%的范围内,并且内壁的范围为该距离的约10-70%。
    • 2. 发明申请
    • METHOD AND APPARATUS FOR REDUCING TOTAL PRESSURE LOSS IN A TURBINE ENGINE
    • 减少涡轮发动机总压损失的方法和装置
    • WO2004106717A2
    • 2004-12-09
    • PCT/US2004/014536
    • 2004-05-28
    • COMBUSTION SCIENCE & ENGINEERING, INC.HAMMER, Andrew, J.BATTAGLIOLI, John, l.
    • HAMMER, Andrew, J.BATTAGLIOLI, John, l.
    • F02C
    • F01D25/30
    • A method and apparatus for reducing total pressure loss in the exhaust of a combustion device via an axial diffuser having no turning vanes, support struts, rods, or other obstructions to exhaust flow. The axial diffuser includes an inner wall and an outer wall each having a turn radius and forming an annular cross section having increasing cross-sectional area in the downstream direction of flow, the flow being transitioned from axial to radial direction thereby. The diffuser is supported in the plenum by rods, struts or a cradle; from a stand surrounding the axial diffuser via struts or rods; or from existing diffuser support structure by web stiffeners. The diffuser flow path turn radius of the outer wall ranges from about 50-95% of the radial distance from the inner wall to a wall of the exhaust plenum, and of the inner wall ranges from about 10-70% of this distance.
    • 一种用于通过轴向扩散器减少燃烧装置的排气中的总压力损失的方法和装置,所述轴向扩散器没有转动叶片,支撑支柱,杆或其它阻碍物排出流动。 轴向扩散器包括内壁和外壁,每个外壁具有转弯半径并且形成具有在下游流动方向上具有增加的横截面面积的环形横截面,该流动从轴向向径向过渡。 扩散器通过杆,支柱或支架支撑在增压室中; 通过支柱或杆从围绕轴向扩散器的支架上; 或通过腹板加强件从现有的扩散器支撑结构。 外壁的扩散器流路转弯半径在从内壁到排气室的壁的径向距离的约50-95%的范围内,并且内壁的范围为该距离的约10-70%。