Inferred oil responsiveness using pressure sensor pulses
    6.
    发明授权
    Inferred oil responsiveness using pressure sensor pulses 有权
    推测使用压力传感器脉冲的油响应性

    公开(公告)号:US08079335B2

    公开(公告)日:2011-12-20

    申请号:US12561702

    申请日:2009-09-17

    IPC分类号: F01L1/34

    CPC分类号: F01L1/34 F01L2001/34423

    摘要: A system and method for controlling an internal combustion engine include determining oil responsiveness based on pressure variations associated with oil pump pulses in response to a stimulus, and controlling the engine based on the determined oil responsiveness. The stimulus may be a change in oil temperature, engine speed, or commanded pump pressure, for example. The system and method may also use the rate of change of mean oil pressure to determine the oil responsiveness or measure of oil viscosity. Oil responsiveness may be used to control hydraulic actuators, such as variable cam timing devices, or valve deactivation devices.

    摘要翻译: 用于控制内燃机的系统和方法包括响应于刺激而基于与油泵脉冲相关联的压力变化来确定油响应性,以及基于所确定的油响应性来控制发动机。 刺激可能是例如油温,发动机转速或指令泵压力的变化。 系统和方法还可以使用平均油压的变化率来确定油的响应性或油粘度的测量。 油响应性可用于控制液压致动器,例如可变凸轮定时装置或阀停用装置。

    Methods and apparatus for decreasing combustor emissions with spray bar assembly
    7.
    发明授权
    Methods and apparatus for decreasing combustor emissions with spray bar assembly 失效
    用喷杆组件减少燃烧室排放的方法和装置

    公开(公告)号:US06540162B1

    公开(公告)日:2003-04-01

    申请号:US09604985

    申请日:2000-06-28

    IPC分类号: A62C208

    摘要: A combustor for a gas turbine engine operates with high combustion efficiency, and low nitrous oxide emissions during engine operations. The combustor includes at least one trapped vortex cavity, a fuel delivery system including two fuel circuits, and a fuel spray bar assembly. A pilot fuel circuit supplies fuel to the trapped vortex cavity and a main fuel circuit supplies fuel to the combustor. The fuel spray bar assembly includes a spray bar and a heat shield. The spray bar is sized to fit within the heat shield. The heat shield includes aerodynamically-shaped upstream and downstream sides.

    摘要翻译: 用于燃气涡轮发动机的燃烧器以高燃烧效率运行,并且在发动机运行期间运行低一氧化二氮排放。 燃烧器包括至少一个被捕获的涡流腔,包括两个燃料回路的燃料输送系统和燃料喷射杆组件。 导向燃料回路将燃料供给到被捕获的涡流空腔,主燃料回路将燃料供给燃烧器。 燃料喷射杆组件包括喷射杆和隔热罩。 喷杆尺寸适合装在隔热罩内。 隔热罩包括空气动力学形状的上游侧和下游侧。

    MULTI-PIECE TWIN SCROLL TURBINE
    10.
    发明申请
    MULTI-PIECE TWIN SCROLL TURBINE 审中-公开
    多级双滚动涡轮机

    公开(公告)号:US20130189093A1

    公开(公告)日:2013-07-25

    申请号:US13356523

    申请日:2012-01-23

    IPC分类号: F01D1/02 B23P15/00

    摘要: A turbine is provided. The turbine includes a housing radially extending around a turbine rotor including a first piece defining a portion of a first scroll passage boundary and a second piece having an interface wall contiguous with an interface wall of the first piece, the second piece coupled to the first piece and including a divider defining another portion of the first scroll passage boundary and a portion of a second scroll passage boundary.

    摘要翻译: 提供涡轮机。 涡轮机包括围绕涡轮机转子径向延伸的壳体,包括限定第一涡旋通道边界的一部分的第一部件和具有与第一部件的界面壁邻接的界面壁的第二部件,第二部件联接到第一部件 并且包括限定第一涡旋通道边界的另一部分和第二涡卷通道边界的一部分的分隔件。