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    MULTIPLE DIFFUSING COOLING HOLE
    12.
    发明申请
    MULTIPLE DIFFUSING COOLING HOLE 审中-公开

    公开(公告)号：US20170152750A1

    公开(公告)日：2017-06-01

    申请号：US15237416

    申请日：2016-08-15

    Applicant: United Technologies Corporation

    Inventor： JinQuan Xu

    IPC: F01D5/18 ,  F01D9/06 ,  F23R3/06

    CPC classification number: F01D5/186 ,  F01D9/065 ,  F05D2240/81 ,  F05D2260/202 ,  F23R3/06 ,  F23R2900/03042 ,  Y02T50/676

    Abstract: A gas turbine engine component includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet, a first diffusing section extending downstream from the metering section, and a second diffusing section extending downstream from the first diffusing section to the outlet. The second diffusing section includes first and second lobes, each lobe diverging longitudinally and laterally relative to the metering section, and a trailing edge.

    Airfoil Assembly with Paired Endwall Contouring
    17.
    发明申请
    Airfoil Assembly with Paired Endwall Contouring 有权
    具有配对端壁轮廓的翼型组件

    公开(公告)号：US20140212260A1

    公开(公告)日：2014-07-31

    申请号：US13718213

    申请日：2012-12-18

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： JinQuan Xu

    IPC: F01D9/04

    CPC classification number: F01D9/041 ,  F01D5/143 ,  Y02T50/673

    Abstract: An airfoil assembly is disclosed. The airfoil assembly may comprise a series of airfoils such as vanes radially extending between an ID endwall and a substantially concentric OD endwall. The airfoils are circumferentially spaced apart and define a plurality of fluid flow passages between adjacent airfoils. The ID endwall and the OD endwall define contoured regions to optimize fluid flow through the passages. A geometric relationship between the ID endwall contoured regions and the OD endwall contoured regions assures that the throat area generally increases or decreases in the direction of fluid flow.

    Abstract translation: 公开了一种翼型组件。 翼型组件可以包括一系列翼型件，例如在ID端壁和基本上同心的OD端壁之间径向延伸的叶片。 翼型件在周向间隔开并且在相邻翼型之间限定多个流体流动通道。 ID端壁和OD端壁定义轮廓区域以优化通过通道的流体流动。 ID端壁轮廓区域和OD端壁轮廓区域之间的几何关系确保了喉部区域在流体流动方向上通常增加或减小。

    Cooled fuel injector system for a gas turbine engine and method for operating the same
    19.
    发明授权
    Cooled fuel injector system for a gas turbine engine and method for operating the same 有权

    公开(公告)号：US10400674B2

    公开(公告)日：2019-09-03

    申请号：US14707790

    申请日：2015-05-08

    Applicant: United Technologies Corporation

    Inventor： JinQuan Xu

    IPC: F02C7/18 ,  F23R3/28 ,  F02C6/08 ,  F02C7/224

    Abstract: A cooled fuel injector system of a combustor section of a gas turbine engine is provided. At least a part of the fuel injector system is exposed to core gas flow traveling through the engine. The cooled fuel injector system includes a source of a first cooling fluid and a fuel injector system component. The first cooling fluid is at a temperature lower than a temperature of the core gas flow proximate the fuel injector system. The fuel injector system component includes a vascular engineered structure lattice (VESL) structure, which VESL structure is in fluid communication with the source of the cooling fluid.

    Multi-lobed cooling hole
    20.
    发明授权
    Multi-lobed cooling hole 有权

    公开(公告)号：US10329920B2

    公开(公告)日：2019-06-25

    申请号：US14775015

    申请日：2014-03-11

    Applicant: United Technologies Corporation

    Inventor： JinQuan Xu

    IPC: F01D5/08 ,  F01D5/18 ,  F01D9/06

    Abstract: A gas turbine engine component subjected to a flow of high temperature gas includes a wall having first and second surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first surface, an outlet located at the second surface, a metering section extending downstream from the inlet, and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe diverging longitudinally and laterally from the metering section and having a first downstream end adjacent the outlet and spaced from the inlet by a first distance, a second lobe diverging longitudinally from the metering section and having a second downstream end adjacent the outlet and spaced from the inlet by a second distance different from the first, and a transition region positioned between the lobes, the transition region having a third downstream end adjacent the outlet.

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