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    • 2. 发明申请
    • CYLINDER LINER AND A METHOD FOR IMPROVED OIL DISTRIBUTION IN A CYLINDER LINER
    • 气缸衬管和一种改进的气缸分配在缸筒内的方法
    • WO2013178247A1
    • 2013-12-05
    • PCT/EP2012/059999
    • 2012-05-29
    • CHRIS-MARINE ABGUSTAFSSON, AndersGRUNDITZ, Daniel
    • GUSTAFSSON, AndersGRUNDITZ, Daniel
    • F02F1/00F02F1/20F16J10/04
    • F02F1/004F02F1/20
    • The invention relates to a cylinder liner (2') for a piston engine, such as a large two-stroke crosshead engine. The cylinder liner (2') comprises an inside surface (1'), at least one groove (3') formed in said inside surface (1'), said at least one groove (3') having an upper and a lower end portion (4', 5'), wherein a first angle (α') is formed between a geometric line (U) extending along said inside surface (1') and a groove surface (6') in said upper end portion (4'), and a second angle (β') is formed between the geometric line (U) extending along said inside surface (1') and the groove surface (6') in said lower end portion (5'). The cylinder liner (2') is characterized in that said second angle (β') is significantly larger than said first angle (α'). The invention also relates to a method for distributing oil along an inside surface of a cylinder liner.
    • 本发明涉及一种用于活塞发动机的气缸套(2'),例如大的二冲程十字头发动机。 气缸套(2')包括内表面(1'),形成在所述内表面(1')中的至少一个凹槽(3'),所述至少一个凹槽(3')具有上端和下端 (4',5'),其中在沿着所述内表面(1')延伸的几何线(U)和所述上端部分(4)中的槽表面(6')之间形成第一角度(α' '),并且在沿着所述内表面(1')延伸的几何线(U)和所述下端部分(5')中的槽表面(6')之间形成第二角度(β')。 气缸套(2')的特征在于所述第二角度(β')明显大于所述第一角度(α')。 本发明还涉及沿着气缸套的内表面分配油的方法。
    • 7. 发明申请
    • TURBO COMPRESSOR SYSTEM FOR INTERNAL COMBUSTION ENGINE COMPRISING TWO SERIALLY PLACED TURBO UNITS WITH THEIR ROTATION AXES ESSENTIALLY CONCENTRIC
    • 用于内燃机的涡轮压缩机系统,包括两个串联的涡轮机组,其旋转轴基本上集中
    • WO2004101971A1
    • 2004-11-25
    • PCT/SE2004/000729
    • 2004-05-11
    • VOLVO LASTVAGNAR ABGOBERT, UlrichSUNDIN, LarsISING, MagnusGRUNDITZ, DanielANDERSSON, PerGISELMO, KentKRAUSCHE, Sebastian
    • GOBERT, UlrichSUNDIN, LarsISING, MagnusGRUNDITZ, DanielANDERSSON, PerGISELMO, KentKRAUSCHE, Sebastian
    • F02B37/013
    • F02B37/013F01N13/107F02B29/04F02B37/004F02B37/025F05B2220/40F05B2250/311Y02T10/144
    • The invention relates to a turbocharger system for an internal combustion engine (10) having at least one exhaust line (15, 16) for evacuating exhaust gases from the combustion chamber (11) of the engine and at least one inlet line (12) for supplying air to said combustion chamber. A high-pressure turbine (17) interacts with a high-pressure compressor (19) and hereupon forms a high-pressure turbo unit (18) with a common rotation axis. A low-pressure turbine (21) interacts with a low-pressure compressor (23) and hereupon forms a low-pressure turbo unit (22) with a common rotation axis, for extracting energy from the exhaust flow of the engine and pressurizing the inlet air of the engine. The low-pressure turbine (21) is of the axial type. The high-pressure turbo unit and the low-pressure turbo unit are serially placed with the rotation axes essentially concentric and with the high-pressure turbine (17) and the low-pressure turbine (21) placed adjacent to each other and coupled together by an intermediate piece configured as a flow duct. This is arranged to allow a certain eccentricity between the two rotation axes. The low-pressure turbo unit (22) is attached to one part of the internal combustion engine (10), whilst the high-pressure turbo unit (18) is attached to another part of the engine (10).
    • 本发明涉及一种用于内燃机(10)的涡轮增压器系统,其具有用于从发动机的燃烧室(11)排出废气的至少一个排气管线(15,16)和至少一个入口管线(12),用于 向所述燃烧室供应空气。 高压涡轮机(17)与高压压缩机(19)相互作用,于是形成具有公共旋转轴线的高压涡轮机单元(18)。 低压涡轮机(21)与低压压缩机(23)相互作用,由此形成具有共同旋转轴线的低压涡轮机组件(22),用于从发动机的排气流中提取能量并对入口 发动机的空气。 低压涡轮机(21)为轴向型。 高压涡轮单元和低压涡轮单元串联放置,旋转轴基本上是同心的,并且高压涡轮机(17)和低压涡轮机(21)彼此相邻放置并且通过 构成为流路的中间件。 这被设置为允许两个旋转轴之间的一定偏心。 低压涡轮单元(22)附接到内燃机(10)的一部分,而高压涡轮单元(18)附接到发动机(10)的另一部分。