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    • 4. 发明申请
    • EXHAUST MANIFOLD OF AN INTERNAL COMBUSTION ENGINE
    • 内燃机的排气歧管
    • US20110016859A1
    • 2011-01-27
    • US12921430
    • 2009-03-11
    • Oliver Schumnig
    • Oliver Schumnig
    • F01N1/00F04D29/42
    • F01N13/10F01N13/1816F02B37/00
    • The invention relates to an exhaust manifold (18) of an interna! combustion engine (20), with a number of exhaust pipe bends (1) corresponding to the number of cylinders of the internal combustion engine (20), said exhaust pipe bends being brought together at one end into an input flange (2) which can be fastened to the internal combustion engine (20), and being brought together at the other end; with a supply gas duct (21) which is connected at one end to a collector component (4) and at the other end to a rotor space (15) of a turbine housing (17) of a turbine of an exhaust-gas turbocharger; and with at least one compensator (19′) for compensating for thermal stresses in at least one exhaust pipe bend (1) and the supply gas duct (21), wherein the at least one compensator (19′) is designed as a component which is integrated in at least one exhaust pipe component (1).
    • 本发明涉及一种内部的排气歧管(18) 内燃机(20),具有与内燃机(20)的气缸数相对应的多个排气管弯头(1),所述排气管弯头一端接合到输入法兰(2)中,所述输入法兰 被固定在内燃机(20)上,并在另一端组合在一起; 与供气管道(21)一端连接到集电器部件(4),另一端连接到排气涡轮增压器的涡轮机的涡轮机壳体(17)的转子空间(15); 以及用于补偿至少一个排气管弯头(1)和供气管道(21)中的热应力的至少一个补偿器(19'),其中所述至少一个补偿器(19')被设计为 集成在至少一个排气管部件(1)中。
    • 6. 发明申请
    • TURBOCHARGER
    • 涡轮增压器
    • US20100047054A1
    • 2010-02-25
    • US12444757
    • 2007-10-23
    • Klaus-Peter DörleOliver Schumnig
    • Klaus-Peter DörleOliver Schumnig
    • F04D15/00
    • F02B37/16B22C9/101B22D17/00F01D9/026F01D17/105F02B37/02F02B39/00F05D2220/40F05D2230/211F05D2250/314Y02T10/144
    • The invention relates to a turbocharger (1) having a turbine (2); and having a compressor (3) connected to the turbine (2) by means of a bearing housing (4), the compressor comprising a compressor housing (5), which has a reference surface (BF) perpendicular to a turbocharger axis (AL), and a valve flange (6) equipped with a valve seat (11) for a wastegate valve and a connecting channel (9) to a compressor inlet (7), wherein the valve flange (6) has a flange surface (8) that is disposed at a calculable angle (α) to the reference surface (BF) in a tilted manner, and wherein the connecting channel (9) has a channel axis (AK), which is disposed at a calculable angle (β) in a tilted manner.
    • 本发明涉及一种具有涡轮机(2)的涡轮增压器(1)。 并且具有通过轴承箱(4)连接到所述涡轮机(2)的压缩机(3),所述压缩机包括压缩机壳体(5),所述压缩机壳体具有垂直于涡轮增压器轴线(AL)的参考表面(BF) ,以及配备有用于废气门阀的阀座(11)和与压缩机入口(7)的连接通道(9)的阀法兰(6),其中阀法兰(6)具有凸缘表面(8),凸缘表面 以倾斜的方式配置到参考表面(BF)的可计算角度(α),并且其中连接通道(9)具有通道轴线(AK),该通道轴线(AK)以可计算的角度(& bgr)设置在 倾斜的方式。
    • 7. 发明授权
    • Exhaust manifold of an internal combustion engine
    • 内燃机的排气歧管
    • US09151208B2
    • 2015-10-06
    • US12921430
    • 2009-03-11
    • Oliver Schumnig
    • Oliver Schumnig
    • F01N1/00F01N13/10F01N13/18F02B37/00
    • F01N13/10F01N13/1816F02B37/00
    • The invention relates to an exhaust manifold (18) of an interna! combustion engine (20), with a number of exhaust pipe bends (1) corresponding to the number of cylinders of the internal combustion engine (20), said exhaust pipe bends being brought together at one end into an input flange (2 ) which can be fastened to the internal combustion engine (20), and being brought together at the other end; with a supply gas duct (21) which is connected at one end to a collector component (4) and at the other end to a rotor space (15) of a turbine housing (17) of a turbine of an exhaust-gas turbocharger; and with at least one compensator (19′) for compensating for thermal stresses in at least one exhaust pipe bend (1) and the supply gas duct (21), wherein the at least one compensator (19′) is designed as a component which is integrated in at least one exhaust pipe component (1).
    • 本发明涉及一种内部的排气歧管(18) 内燃机(20),具有对应于内燃机(20)的气缸数量的多个排气管弯头(1),所述排气管弯头一端接合到输入法兰(2)中,该输入法兰 被固定在内燃机(20)上,并在另一端组合在一起; 与供气管道(21)一端连接到集电器部件(4),另一端连接到排气涡轮增压器的涡轮机的涡轮机壳体(17)的转子空间(15); 以及用于补偿至少一个排气管弯头(1)和供气管道(21)中的热应力的至少一个补偿器(19'),其中所述至少一个补偿器(19')被设计为 集成在至少一个排气管部件(1)中。
    • 8. 发明申请
    • EXHAUST-GAS TURBOCHARGER
    • 排气涡轮增压器
    • US20110142604A1
    • 2011-06-16
    • US12959479
    • 2010-12-03
    • Oliver SchumnigFrank Scherrer
    • Oliver SchumnigFrank Scherrer
    • F04D29/08
    • F01D25/24F02C6/12F05D2220/40F05D2260/30F05D2260/33
    • The invention relates to an exhaust-gas turbocharger (1) having a compressor housing (3), having a bearing housing (28) which can be connected at one end to the compressor housing (3) by means of a first fastening device (19), and having a turbine housing (2) which can be connected to the bearing housing (28) at the other end of the latter by means of a second fastening device (20), with the compressor housing (3), the bearing housing (28) and the turbine housing (2) extending along an exhaust-gas turbocharger longitudinal axis (R), wherein the second fastening device (20) is designed as a plug-and-twist connecting device, and a seal (25) is provided between the turbine housing (2) and the bearing housing (28).
    • 本发明涉及一种具有压缩机壳体(3)的排气涡轮增压器(1),其具有轴承壳体(28),该轴承壳体可以通过第一紧固装置(19)在一端连接到压缩机壳体(3) ),并且具有涡轮机壳体(2),所述涡轮机壳体(2)可以通过第二紧固装置(20)与所述压缩机壳体(3)连接到所述轴承壳体(28)的另一端,所述轴承壳体 (28)和所述涡轮机壳体(2)沿着排气涡轮增压器纵向轴线(R)延伸,其中所述第二紧固装置(20)被设计为插头和扭转连接装置,并且密封件(25)是 设置在涡轮壳体(2)和轴承壳体(28)之间。
    • 9. 发明授权
    • Exhaust-gas turbocharger
    • 排气涡轮增压器
    • US09115599B2
    • 2015-08-25
    • US12959479
    • 2010-12-03
    • Oliver SchumnigFrank Scherrer
    • Oliver SchumnigFrank Scherrer
    • F01D25/24F02C6/12
    • F01D25/24F02C6/12F05D2220/40F05D2260/30F05D2260/33
    • The invention relates to an exhaust-gas turbocharger (1) having a compressor housing (3), having a bearing housing (28) which can be connected at one end to the compressor housing (3) by means of a first fastening device (19), and having a turbine housing (2) which can be connected to the bearing housing (28) at the other end of the latter by means of a second fastening device (20), with the compressor housing (3), the bearing housing (28) and the turbine housing (2) extending along an exhaust-gas turbocharger longitudinal axis (R), wherein the second fastening device (20) is designed as a plug-and-twist connecting device, and a seal (25) is provided between the turbine housing (2) and the bearing housing (28).
    • 本发明涉及一种具有压缩机壳体(3)的排气涡轮增压器(1),其具有轴承壳体(28),该轴承壳体可以通过第一紧固装置(19)在一端连接到压缩机壳体(3) ),并且具有涡轮机壳体(2),所述涡轮机壳体(2)可以通过第二紧固装置(20)与所述压缩机壳体(3)连接到所述轴承壳体(28)的另一端,所述轴承壳体 (28)和所述涡轮机壳体(2)沿着排气涡轮增压器纵向轴线(R)延伸,其中所述第二紧固装置(20)被设计为插头和扭转连接装置,并且密封件(25)是 设置在涡轮壳体(2)和轴承壳体(28)之间。