Internal Combustion Engine Cylinder Head with Tubular Apparatus for Intake and Exhaust

    公开(公告)号:US20180320630A1

    公开(公告)日:2018-11-08

    申请号:US15916770

    申请日:2018-03-09

    Applicant: XIACAMERI

    Abstract: An apparatus for intake and exhaust of an engine includes: an outer tube including an outer-tube close end, an outer-tube open end, and a first outer-tube aperture set including a first aperture and a first outer-tube aperture group, an inner tube positioned in the outer tube about a concentric line, including an inner-tube close end, an inner-tube open end, and a first inner-tube aperture set including a second aperture and a first inner-tube aperture group, in which the inner-tube close end is proximate to the outer-tube close end, and a shaft connected to the inner-tube open end for rotating the inner tube in the outer tube about the concentric line, in which when the inner tube rotates, the second aperture sweeps across a portion of the first aperture and the first inner-tube aperture group sweeps across a portion of the first outer-tube aperture group.

    SECONDARY AIR INTRODUCTION DEVICE
    4.
    发明申请

    公开(公告)号:US20180291791A1

    公开(公告)日:2018-10-11

    申请号:US15943273

    申请日:2018-04-02

    Abstract: There is provided a secondary air introduction device configured to introduce air into an exhaust port provided in a cylinder head of an engine by using a negative pressure in the exhaust port. A back-flow restriction member is provided between a reed valve and the exhaust port in an air introduction passage, and includes a plate part intersecting with an extension direction of the air introduction passage. The plate part has an air passing region in which the air flowing through the air introduction passage from an air intake unit toward the exhaust port is enabled to pass therethrough and a back-flow cutoff region in which exhaust air, which flows in a direction of directly colliding with at least a valve body of the reed valve, of exhaust air flowing back through the air introduction passage from the exhaust port is cut off.

    CYLINDER HEAD OF MULTI-CYLINDER ENGINE
    6.
    发明申请

    公开(公告)号:US20170362992A1

    公开(公告)日:2017-12-21

    申请号:US15525459

    申请日:2015-11-10

    Inventor: Satoko TOFUKUJI

    Abstract: A first coolant flow passage is provided to extend in a longitudinal direction of a cylinder head. In at least one of cross sections perpendicular to the longitudinal direction, the first coolant flow passage is located between a flat plane including central axes of a plurality of combustion chambers and parallel to the longitudinal direction and a central line plane including central lines of a plurality of intake ports. In at least one of cross sections perpendicular to the longitudinal direction, at least a portion of a second coolant flow passage is located between the combustion chamber and the first coolant flow passage. A coolant at a temperature lower than that of a coolant flowing in the second coolant flow passage flows in the first coolant flow passage.

    VALVE SEATS FOR CYLINDER HEADS IN AIRCRAFT ENGINES
    8.
    发明申请
    VALVE SEATS FOR CYLINDER HEADS IN AIRCRAFT ENGINES 审中-公开
    气动发动机气缸盖阀座

    公开(公告)号:US20160076480A1

    公开(公告)日:2016-03-17

    申请号:US14802986

    申请日:2015-07-17

    Applicant: David ENDRIGO

    Inventor: David ENDRIGO

    Abstract: Intake and exhaust valve seat inserts for aircraft cylinder heads. The inserts are configured for low pressure loss as inlet air and hot exhaust gas passes through the respective valve seat inserts. In an embodiment, the intake and exhaust valve seat inserts may have a plurality of faces or facets, at prescribed angles, in order to minimize pressure loss of gases passing therethrough. In an embodiment, rather than a plurality of faces or facets, the intake valve seat sidewall, and/or the exhaust valve seat sidewall may be provided in the configuration of a smooth curve approximating a set of selected angles, as if the component were made with a plurality of facets.

    Abstract translation: 用于飞机气缸盖的进气阀和排气阀座。 插入件配置为低压力损失,因为入口空气和热排气通过相应的阀座插入件。 在一个实施例中,进气和排气阀座插入件可以以规定的角度具有多个面或小面,以便使通过其中的气体的压力损失最小化。 在一个实施例中,不是多个面或小面,所以进气阀座侧壁和/或排气阀座侧壁可以以接近一组选定角度的平滑曲线的构造来提供,好像该组件被制成 具有多个面。

    INTERNAL COMBUSTION ENGINE HAVING A SPACER SLEEVE WITH A CENTERING DEVICE
    9.
    发明申请
    INTERNAL COMBUSTION ENGINE HAVING A SPACER SLEEVE WITH A CENTERING DEVICE 有权
    具有中心装置的间隔套筒的内燃机

    公开(公告)号:US20150337754A1

    公开(公告)日:2015-11-26

    申请号:US14410540

    申请日:2013-06-14

    Abstract: An internal combustion engine is provided. The internal combustion engine includes at least one cylinder head and at least one exhaust pipe having at least one flange, whereby the flange has at least two flange fastening holes that have at least two fastening screws for fastening the exhaust pipe to the cylinder head of the internal combustion engine, whereby the exhaust pipe can be arranged so as to be connected to the cylinder head by means of the fastening screws in such a way that it can be dismantled, whereby at least one centering device is provided essentially in the area of the flange holes.

    Abstract translation: 提供内燃机。 所述内燃机包括至少一个气缸盖和至少一个具有至少一个凸缘的排气管,由此所述凸缘具有至少两个凸缘紧固孔,所述至少两个凸缘紧固孔具有至少两个用于将所述排气管紧固到所述气缸盖的紧固螺钉 内燃机,由此排气管可以被布置成通过紧固螺钉连接到气缸盖,使得其可以被拆卸,由此至少一个定心装置基本上设置在该内燃机的区域中 法兰孔。

    DIRECT FUEL INJECTION SYSTEM
    10.
    发明申请
    DIRECT FUEL INJECTION SYSTEM 审中-公开
    直接燃油喷射系统

    公开(公告)号:US20140020653A1

    公开(公告)日:2014-01-23

    申请号:US13551419

    申请日:2012-07-17

    Abstract: A system in an internal combustion engine is provided. The system a combustion chamber, a first exhaust port in fluidic communication with the combustion chamber, a second exhaust port in fluidic communication with the combustion chamber, and a direct fuel injector positioned between the first and second exhaust port and fluidly communicating directly with the combustion chamber.

    Abstract translation: 提供内燃机中的系统。 该系统是燃烧室,与燃烧室流体连通的第一排气口,与燃烧室流体连通的第二排气口和定位在第一和第二排气口之间并与燃烧直接流体连通的直接燃料喷射器 房间。

Patent Agency Ranking