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    • 8. 发明申请
    • AIR TURBINE FOR COMBUSTION ENGINE
    • 用于燃烧发动机的空气涡轮机
    • WO2002066799A1
    • 2002-08-29
    • PCT/US2002/004452
    • 2002-02-15
    • CUMMINGS, CraigSUTERA, Anthony, J.
    • CUMMINGS, CraigSUTERA, Anthony, J.
    • F01N1/02
    • F01N13/004F01N1/02F01N1/06F01N1/08F01N1/088F01N1/12F01N1/166F01N13/007F01N2470/04F01N2590/02F02D2009/0283F02M35/1211F02M35/1216F02M35/1222F02M35/1227Y02T10/146
    • An air turbine apparatus (10) for use with a combustion engine either as a muffler or as an air intake device is comprised of a housing (12) defining an expansion chamber (20) and an airfoil (50) positioned within the housing (12). The airfoil (50) includes a central aperture (52) extending longitudinally there through that is in fluid communication with both the inlet (18) and the outlet (16) of the housing (12). The airfoil (50) is configured to allow gases flowing through the inlet (18) to flow between the outer edge of the airfoil (50) and the housing (12) and through the aperture (52) of the airfoil (50). In addition, the air travelling through the housing (12) is caused to spin as it travels through the housing (12). This rotational flow increased the rate of flow of gases through the air turbine device (10). An induction tube (22) is provided between the airfoil (50) and the outlet (16) of the housing (12) to encourage turbulent flow of gases without restricting flow to produce a muffling effect and thus a dampening of noise from the combustion engine.
    • 用作消声器或作为进气装置的内燃机使用的空气涡轮机装置(10)包括限定膨胀室(20)的壳体(12)和定位在壳体(12)内的翼型件 )。 机翼(50)包括沿其纵向延伸的中心孔(52),其通过与壳体(12)的入口(18)和出口(16)流体连通。 机翼(50)构造成允许流过入口(18)的气体在翼型件(50)的外边缘和壳体(12)之间并通过翼型件(50)的孔口(52)流动。 此外,通过壳体(12)行进的空气在其穿过壳体(12)时被旋转。 该旋转流量增加了气体通过空气涡轮机装置(10)的流量。 感应管(22)设置在机翼(50)和壳体(12)的出口(16)之间,以促进气体的湍流而不限制流动,从而产生消声效应,从而减轻来自内燃机 。