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    GAS TURBINE ENGINE SPLINE ARRANGEMENT
    301.
    发明申请
    GAS TURBINE ENGINE SPLINE ARRANGEMENT 审中-公开
    气体涡轮发动机排列安排

    公开(公告)号：WO1995030098A1

    公开(公告)日：1995-11-09

    申请号：PCT/US1995004989

    申请日：1995-04-24

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： UNITED TECHNOLOGIES CORPORATION ,  BRACKONESKI, Russell, F. ,  BUONO, Dennis, F. ,  ABRAHAMIAN, John, P.

    IPC: F16D01/06

    CPC classification number: F16D1/06 ,  F01D5/026 ,  F16D2001/103 ,  Y10T403/18 ,  Y10T403/7026

    Abstract: A hollow drive shaft (20) with external splines (26) drives a hollow driven shaft (14) which has internal splines (32). The driven shaft (14) thickness is uniformly tapered in the spline area, while the drive shaft (20) has a constant thickness through part of the spline area, and then a uniformly reducing thickness toward the unloaded end. The teeth of the external spline are crowned with the peak toward the loaded end of the drive spline (26). A flat is located at this peak.

    Abstract translation: 具有外花键（26）的中空驱动轴（20）驱动具有内花键（32）的中空从动轴（14）。 驱动轴（14）的厚度在花键区域中均匀地变细，而驱动轴（20）通过花键区域的一部分具有恒定的厚度，然后朝向卸载端均匀地减小厚度。 外花键的齿部朝向驱动花键（26）的装载端顶部加上顶点。 一个单位位于这个高峰。

    COUPLING SYSTEM FOR A PLANETARY GEAR TRAIN
    303.
    发明申请
    COUPLING SYSTEM FOR A PLANETARY GEAR TRAIN 审中-公开
    一种行车齿轮联动系统

    公开(公告)号：WO1995027860A1

    公开(公告)日：1995-10-19

    申请号：PCT/US1995004471

    申请日：1995-04-07

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： UNITED TECHNOLOGIES CORPORATION ,  SHERIDAN, William, G. ,  PAGLUICA, Gino, J.

    IPC: F16H01/28

    CPC classification number: F16H1/2809 ,  F01D5/02 ,  F01D5/026 ,  F05D2240/62 ,  Y02T50/671

    Abstract: A coupling system including a sun gear coupling (32) and a ring gear coupling (158) for connecting the sun gear (36) and the ring gear housing (50) of a planetary gear train (26) to an external shaft (24) and an external mechanical ground (56) respectively are each characterized by undulant cross sections for accommodating parallel and angular misalignments. A ring gear deflection limiter (158), antirotation spline (190) and vibration damper are also included for enhanced operation.

    Abstract translation: 一种联接系统，包括用于将行星齿轮系（26）的太阳齿轮（36）和齿圈壳体（50）连接到外部轴（24）的太阳齿轮联轴器（32）和齿圈联接器（158） 和外部机械接地（56）分别以起伏的横截面为特征，用于容纳平行和角度不对准。 还包括齿圈偏转限制器（158），防旋转花键（190）和减振器，以增强操作性能。

    TURBINE SHROUD SEGMENT WITH SERPENTINE COOLING CHANNELS
    304.
    发明申请
    TURBINE SHROUD SEGMENT WITH SERPENTINE COOLING CHANNELS 审中-公开
    涡轮风冷部分与SERPENTINE冷却通道

    公开(公告)号：WO1995027126A1

    公开(公告)日：1995-10-12

    申请号：PCT/US1995003567

    申请日：1995-03-21

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： UNITED TECHNOLOGIES CORPORATION ,  THOMPSON, Ralph, J. ,  KANE, Daniel, E.

    IPC: F01D11/08

    CPC classification number: F01D11/08 ,  F01D25/12 ,  Y02T50/675

    Abstract: A turbine shroud segment (64) fixed by hooks (72) in the stator of a gas turbine engine includes a serpentine cooling channel (78, 82) along at least one axial edge of the segment. In a particular embodiment, a turbine shroud segment (64) includes a leading edge serpentine cooling channel (78) and a trailing edge serpentine cooling channel (82). Both serpentine channels (78, 82) include ducts (86, 92) that extend to the serpentine channels (78, 82) from a point inward of adjacent retaining hooks (72). Cooling fluid flowing onto the outward surface of the segments flows through the ducts (86, 92) and along the serpentine channels (78, 82) to cool the leading and trailing edges of the segments.

    Abstract translation: 通过钩（72）固定在燃气涡轮发动机的定子中的涡轮机护罩段（64）包括沿着该段的至少一个轴向边缘的蛇形冷却通道（78,82）。 在特定实施例中，涡轮机护罩段（64）包括前缘蛇形冷却通道（78）和后缘蛇形冷却通道（82）。 两个蛇形通道（78,82）包括从邻近的保持钩（72）内部的点延伸到蛇形通道（78,82）的管道（86,92）。 流过分段的外表面的冷却流体流过管道（86,92）并且沿着蛇形通道（78,82）流动以冷却段的前缘和后缘。

    COOLED TURBINE BLADE
    305.
    发明申请
    COOLED TURBINE BLADE 审中-公开
    冷却涡轮叶片

    公开(公告)号：WO1995026459A1

    公开(公告)日：1995-10-05

    申请号：PCT/US1995003573

    申请日：1995-03-21

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： UNITED TECHNOLOGIES CORPORATION ,  ZELESKY, Mark, F.

    IPC: F01D05/18

    CPC classification number: F01D5/187

    Abstract: Turbine blade (10) has a plurality of trailing edge discharge openings (28) discharging cooling air. The blade trailing edge has an increasing thickness "E" toward the tip end (16). Discharge openings with the shortened pressure wall "L" have lesser distances "L" toward the tip end.

    Abstract translation: 涡轮叶片（10）具有排出冷却空气的多个后缘排放口（28）。 叶片后缘朝向顶端（16）具有增加的厚度“E”。 具有缩短的压力壁“L”的排出开口具有较小的距离“L”朝向末端。

    TURBINE VANE WITH A PLATFORM CAVITY HAVING A DOUBLE FEED FOR COOLING FLUID
    306.
    发明申请
    TURBINE VANE WITH A PLATFORM CAVITY HAVING A DOUBLE FEED FOR COOLING FLUID 审中-公开
    涡轮风扇带有一个用于冷却流体的双重进料口的平台

    公开(公告)号：WO1995026458A1

    公开(公告)日：1995-10-05

    申请号：PCT/US1995003383

    申请日：1995-03-16

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： UNITED TECHNOLOGIES CORPORATION ,  CALDERBANK, John, C.

    IPC: F01D05/18

    CPC classification number: F01D5/187 ,  F05D2240/10 ,  F05D2240/81

    Abstract: A turbine vane for a gas turbine engine includes a platform with a cavity along the trailing edge having a double feed arrangement for injecting cooling fluid into the cavity. Various construction details are developed that provide a cavity having improved heat transfer due to the elimination of dead zones. In a particular embodiment, a turbine vane includes a platform cavity having a first inlet located on the pressure side of the platform and forward of an attachment rail and a second inlet located on the suction side and forward of the attachment rail. The cavity includes a plurality of trip strips and a plurality of film cooling passages. The trip strips extend from the corners of the cavity and are angled to encourage cooling fluid to flow into the corners. The film cooling passages direct the exiting cooling fluid to form a film of cooling fluid over the platform flow surface.

    Abstract translation: 用于燃气涡轮发动机的涡轮叶片包括具有沿着后缘的空腔的平台，具有用于将冷却流体注入空腔的双重进给装置。 开发了各种构造细节，其提供了由于消除死区而具有改进的热传递的空腔。 在特定实施例中，涡轮叶片包括平台腔，该平台腔具有位于平台的压力侧上的第一入口和连接轨道的前部，以及位于吸入侧和连接轨道前方的第二入口。 空腔包括多个跳闸条和多个膜冷却通道。 脱扣条从腔体的角部延伸并且成角度以促使冷却流体流入拐角。 薄膜冷却通道引导排出的冷却流体在平台流动表面上形成冷却流体膜。

    FLUID/LIQUID SEPARATOR
    308.
    发明申请
    FLUID/LIQUID SEPARATOR 审中-公开
    流体/液体分离器

    公开(公告)号：WO1995026223A1

    公开(公告)日：1995-10-05

    申请号：PCT/US1995003247

    申请日：1995-03-16

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： UNITED TECHNOLOGIES CORPORATION ,  KRAMER, Robert, W.

    IPC: B01D17/038

    CPC classification number: B04B1/00 ,  B01D17/0217 ,  B01D17/045 ,  B04B2001/2075 ,  B04B2001/2083 ,  Y10S494/90 ,  Y10S494/901

    Abstract: A rotating drum (12) divided in axial spaced compartments with one of the compartments includes paddles (14) and coalescing material (16) to separate the fluid from the liquid and the other compartment includes stationary oil pumping (20) and water pumping means (30) and an energy recovery means (26) for effectively separating fluid such as oil from liquid such as water. Another embodiment includes a simplified version of the fluid/liquid separator adapted for zero gravity environment and includes means for purging the lines from air prior to pumping the liquid. An electrical sensing circuit including conductivity sensors (18) or an electronic controller including pressure sensors serve to control the rate of removal of the separated component or controlling said purging means.

    Abstract translation: 分隔成具有其中一个隔室的轴向间隔隔室的旋转滚筒（12）包括桨叶（14）和聚结材料（16），以将流体与液体分离，另一隔室包括固定的油泵送（20）和水泵装置 30）和能量回收装置（26），用于有效地将诸如油的液体与液体如水分离。 另一个实施例包括适于零重力环境的流体/液体分离器的简化版本，并且包括用于在泵送液体之前从空气中吹扫管线的装置。 包括电导率传感器（18）或包括压力传感器的电子控制器的电感测电路用于控制分离组件的移除速度或控制所述清洗装置。

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