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    • 6. 发明授权
    • Turbocharging system for internal combustion engine
    • 内燃机涡轮增压系统
    • US08635869B2
    • 2014-01-28
    • US13146084
    • 2009-09-15
    • Byeongil AnMotoki Ebisu
    • Byeongil AnMotoki Ebisu
    • F02B37/12
    • F02B37/007F02B37/002F02B37/004F02B37/013F02B37/22Y02T10/144
    • A two-stage turbo system provided with an internal combustion engine includes, two turbo-superchargers driven by exhaust gas from the engine, control valves for switching between the flow path of intake gas sucked into the engine and the flow path of exhaust gas, and a control device for controlling the control valves and the turbo-superchargers. The two turbo-superchargers have the same turbine capacity, function respectively as the high-pressure side turbo-supercharger on the exhaust path upstream side and the low-pressure side turbo-supercharger on the exhaust path downstream side, and have, by switching between the flow paths by using the control valves, a series mode in which the two turbo-superchargers are serially connected to each other, a one-stage supercharging mode in which gas flows only to the high-pressure-side turbo-supercharger or only to the low-pressure-side turbo-supercharger, and a parallel mode in which the two turbo-superchargers are connected in parallel to each other.
    • 设置有内燃机的二级涡轮系统包括:由来自发动机的排气驱动的两个涡轮增压器,用于在吸入发动机的进气流和废气流路之间切换的控制阀,以及 用于控制控制阀和涡轮增压器的控制装置。 两个涡轮增压器具有相同的涡轮容量,分别作为排气通道上游侧的高压侧涡轮增压器和排气通道下游侧的低压侧涡轮增压器,并且通过在 通过使用控制阀的流路,其中两个涡轮增压器彼此串联连接的串联模式,其中气体仅流向高压侧涡轮增压器的单级增压模式或仅仅流向 低压侧涡轮增压器以及两个涡轮增压器彼此并联连接的并联模式。
    • 7. 发明申请
    • TURBOCHARGING SYSTEM FOR INTERNAL COMBUSTION ENGINE
    • 内燃机涡轮增压系统
    • US20110296828A1
    • 2011-12-08
    • US13146084
    • 2009-09-15
    • Byeongil AnMotoki Ebisu
    • Byeongil AnMotoki Ebisu
    • F02B37/12F02B37/013F02B37/00
    • F02B37/007F02B37/002F02B37/004F02B37/013F02B37/22Y02T10/144
    • A two-stage turbo system using small-sized turbo-superchargers and simply configured. A two-stage turbo system provided with an internal combustion engine (1), two turbo-superchargers (2A, 2B) driven by exhaust gas from the internal combustion engine (1), control valves (V1-V5) for switching between the flow path of intake gas sucked into the internal combustion engine (1) and the flow path of exhaust gas from the internal combustion engine (1), and a control device for controlling the control valves (V1-V5) and the turbo-superchargers (2A, 2B). The two turbo-superchargers (2A, 2B) have the same turbine capacity, function respectively as the high-pressure side turbo-supercharger (2A) on the exhaust path upstream side and the low-pressure side turbo-supercharger (2B) on the exhaust path downstream side, and have, by switching between the flow paths by using the control valves (V1-V5), a series mode in which the two turbo-superchargers (2A, 2B) are serially connected to each other, a one-stage supercharging mode in which gas flows only to the high-pressure-side turbo-supercharger (2A) or only to the low-pressure-side turbo-supercharger (2B), and a parallel mode in which the two turbo-superchargers (2A, 2B) are connected in parallel to each other.
    • 采用小型涡轮增压器的两级涡轮增压系统,配置简单。 具有内燃机(1)的两级涡轮系统,由内燃机(1)排气驱动的两个涡轮增压器(2A,2B),用于在内燃机(1)之间切换的控制阀(V1-V5) 吸入内燃机(1)的进气通路和来自内燃机(1)的废气流路,以及控制阀(V1-V5)和涡轮增压器(2A)的控制装置 ,2B)。 两个涡轮增压器(2A,2B)分别具有与排气通路上游侧的高压侧涡轮增压器(2A)和低压侧涡轮增压器(2B)相同的涡轮容量功能 排气通道下游侧,并且通过使用控制阀(V1-V5)在流路之间切换,使两个涡轮增压器(2A,2B)彼此串联连接的串联模式, 气体仅流到高压侧涡轮增压器(2A)或仅流向低压侧涡轮增压器(2B)的级增压模式,以及并联模式,其中两个涡轮增压器(2A ,2B)彼此并联连接。
    • 9. 发明授权
    • Variable geometry turbine
    • 可变几何涡轮机
    • US09028202B2
    • 2015-05-12
    • US13807258
    • 2011-08-31
    • Takao YokoyamaHiroshi SuzukiMotoki EbisuToyotaka Yoshida
    • Takao YokoyamaHiroshi SuzukiMotoki EbisuToyotaka Yoshida
    • F01D17/16F02C6/12F02B37/24
    • F01D17/165F02B37/24F02C6/12F05D2220/40
    • A variable geometry turbine includes a fluid space formed by a nozzle mount and a nozzle plate; and a plurality of nozzle vanes arranged in the fluid space at certain intervals in the circumferential direction so as to partition the fluid space. The nozzle vanes are supported by shafts on the nozzle mount, in such a manner as to be capable of turning. The flow rate of the discharged fluid can be adjusted by opening or closing the cross-sectional area of a flow path formed by the adjacent nozzle vanes. The nozzle plate is provided with plate projections protruding toward the nozzle vanes further than, at least, end surfaces of the nozzle vanes, so as to cover the spaces between leading edges of the nozzle vanes and trailing edges of the nozzle vanes adjacent thereto, when the nozzle vanes are at a closed position.
    • 可变几何涡轮机包括由喷嘴座和喷嘴板形成的流体空间; 以及沿圆周方向以一定间隔布置在流体空间中的多个喷嘴叶片,以便分隔流体空间。 喷嘴叶片以能够转动的方式由喷嘴座上的轴支撑。 可以通过打开或关闭由相邻喷嘴叶片形成的流路的横截面积来调节排出流体的流量。 喷嘴板设置有板突起,其比喷嘴叶片的至少端表面突出,以覆盖喷嘴叶片的前缘和与其相邻的喷嘴叶片的后缘之间的空间, 喷嘴叶片处于关闭位置。