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    • 4. 发明授权
    • Method for modulating turbocharger braking
    • 调节涡轮增压器制动的方法
    • US07644584B2
    • 2010-01-12
    • US11605970
    • 2006-11-30
    • Matthew Edward LeustekChristopher Ronald Gehrke
    • Matthew Edward LeustekChristopher Ronald Gehrke
    • F02B33/44F02B37/16F02B37/12F02D23/00F01N3/00
    • F02B37/16F02B37/24F02D9/06Y02T10/144
    • A method for operating an internal combustion engine includes compressing intake air using a compressor, supplying the compressed intake air to at least one combustion chamber of the engine, operating the at least one combustion chamber to output exhaust gas, and directing the exhaust gas to an inlet of a turbine configured to drive the compressor. The method also includes directing the exhaust gas from an outlet of the turbine to an exhaust system, bypassing at least a portion of the compressed intake air around the at least one combustion chamber, and adjusting a geometry of the turbine from a first configuration to a second configuration. The turbine is in the second configuration when the at least the portion of the compressed intake air is bypassed around the at least one combustion chamber.
    • 用于操作内燃机的方法包括使用压缩机压缩进气,将压缩的进气供应到发动机的至少一个燃烧室,操作至少一个燃烧室以输出废气,并将排气引导到 构造成驱动压缩机的涡轮机的入口。 该方法还包括将废气从涡轮机的出口引导到排气系统,绕过至少一个燃烧室周围的压缩进气的至少一部分,以及将涡轮机的几何形状从第一构型调整到 第二配置。 当压缩进气的至少一部分围绕至少一个燃烧室旁路时,涡轮机处于第二构造。
    • 6. 发明申请
    • Method for modulating turbocharger braking
    • 调节涡轮增压器制动的方法
    • US20080127643A1
    • 2008-06-05
    • US11605970
    • 2006-11-30
    • Matthew Edward LeustekChristopher Ronald Gehrke
    • Matthew Edward LeustekChristopher Ronald Gehrke
    • F02B33/34
    • F02B37/16F02B37/24F02D9/06Y02T10/144
    • A method for operating an internal combustion engine includes compressing intake air using a compressor, supplying the compressed intake air to at least one combustion chamber of the engine, operating the at least one combustion chamber to output exhaust gas, and directing the exhaust gas to an inlet of a turbine configured to drive the compressor. The method also includes directing the exhaust gas from an outlet of the turbine to an exhaust system, bypassing at least a portion of the compressed intake air around the at least one combustion chamber, and adjusting a geometry of the turbine from a first configuration to a second configuration. The turbine is in the second configuration when the at least the portion of the compressed intake air is bypassed around the at least one combustion chamber.
    • 用于操作内燃机的方法包括使用压缩机压缩进气,将压缩的进气供应到发动机的至少一个燃烧室,操作至少一个燃烧室以输出废气,并将排气引导到 构造成驱动压缩机的涡轮机的入口。 该方法还包括将废气从涡轮机的出口引导到排气系统,绕过至少一个燃烧室周围的压缩进气的至少一部分,以及将涡轮机的几何形状从第一构型调整到 第二配置。 当压缩进气的至少一部分围绕至少一个燃烧室旁路时,涡轮机处于第二构造。