Exhaust system
    2.
    发明授权

    公开(公告)号:US11988177B2

    公开(公告)日:2024-05-21

    申请号:US18138344

    申请日:2023-04-24

    发明人: Tomoya Ozawa

    摘要: An exhaust system includes a supercharger, a first communication path, a negative pressure generator, and an exhaust sensor. The supercharger includes a turbine and compressor. The turbine is provided in an exhaust pipe of an engine. The compressor is provided in an intake pipe and coupled to the turbine by a shaft. The supercharger supercharges intake air using energy of exhaust air. The first communication path communicates with the exhaust pipe on a downstream side of the turbine and communicates with the intake pipe on an upstream side of the compressor. The exhaust pipe and the intake pipe communicate through the first communication path. The negative pressure generator is interposed in the first communication path and generates a negative pressure. The exhaust sensor is provided in the first communication path between a location where the first communication path is coupled to the exhaust pipe and the negative pressure generator.

    VALVE FOR A DUAL-VOLUTE TURBINE
    4.
    发明公开

    公开(公告)号:US20240060446A1

    公开(公告)日:2024-02-22

    申请号:US18123036

    申请日:2023-03-17

    申请人: BorgWarner Inc.

    发明人: Ivan Injac

    IPC分类号: F02B37/18 F02B37/22 F01D17/10

    摘要: A valve (100) controls a volute connecting opening (240) and a bypass opening (250) of a dual-volute turbine (200). The valve (100) has valve closing body (110), a lever arm (120) and a spindle (130). The valve closing body (110) has a main body (111) and a collar (112). The valve (100) is of a monoblock design with the valve closing body (110), the lever arm (120) and the spindle (130) being made of a single part.

    Turbocharger turbine assembly
    5.
    发明授权

    公开(公告)号:US11821357B2

    公开(公告)日:2023-11-21

    申请号:US17564713

    申请日:2021-12-29

    IPC分类号: F02B37/24 F01D17/16 F02B37/22

    摘要: A turbine housing assembly can include a turbine housing that defines a rotational axis for a turbine wheel; and a cartridge receivable by the turbine housing, where the cartridge includes a nozzle wall component with an upper nozzle surface and a plate component with a lower nozzle surface, where the upper nozzle surface and the lower nozzle surface define a nozzle space, and vanes positioned in the nozzle space, where the vanes are pivotable between a closed vanes position of 0 percent open and a fully open vanes position of 100 percent open, and where, for a vanes position of at least 50 percent open and less than 75 percent open, an axial dimension of the nozzle space increases with respect to decreasing radius as measured from the rotational axis.

    TURBOCHARGER TURBINE ASSEMBLY
    8.
    发明公开

    公开(公告)号:US20230203983A1

    公开(公告)日:2023-06-29

    申请号:US17564713

    申请日:2021-12-29

    IPC分类号: F02B37/24 F01D17/16 F02B37/22

    摘要: A turbine housing assembly can include a turbine housing that defines a rotational axis for a turbine wheel; and a cartridge receivable by the turbine housing, where the cartridge includes a nozzle wall component with an upper nozzle surface and a plate component with a lower nozzle surface, where the upper nozzle surface and the lower nozzle surface define a nozzle space, and vanes positioned in the nozzle space, where the vanes are pivotable between a closed vanes position of 0 percent open and a fully open vanes position of 100 percent open, and where, for a vanes position of at least 50 percent open and less than 75 percent open, an axial dimension of the nozzle space increases with respect to decreasing radius as measured from the rotational axis.

    Annular disk for turbocharger speed control

    公开(公告)号:US11668230B2

    公开(公告)日:2023-06-06

    申请号:US17248516

    申请日:2021-01-28

    申请人: Caterpillar Inc.

    IPC分类号: F02B37/22

    CPC分类号: F02B37/22 F02D2250/34

    摘要: An annular disk comprises a front surface, a rear surface, an outer surface, and an inner surface. The front surface has a front opening within a front plane. The rear surface has a rear opening within a rear plane. The rear opening, which has a diameter that is smaller than a diameter of the front opening, communicates with the front opening to define a bore for guiding an exhaust stream flowing from a turbocharger to an exhaust outlet. The outer surface connects the front surface to the rear surface and includes an outer angled portion, an outer radial portion, and an outer axial portion. The inner surface includes an inner angled portion, an inner axial portion, and an inner radial portion extending between the inner angled portion and the inner axial portion. The inner radial portion is configured to obstruct a portion of the exhaust stream to increase back pressure.