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    BIFURCATED AIR INLET HOUSING FOR A GAS TURBINE ENGINE
    1.
    发明申请
    BIFURCATED AIR INLET HOUSING FOR A GAS TURBINE ENGINE 审中-公开
    用于气体涡轮发动机的双向空气入口壳体

    公开(公告)号：WO2014165364A1

    公开(公告)日：2014-10-09

    申请号：PCT/US2014/031828

    申请日：2014-03-26

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： JONES, Anthony C. ,  LYDON, Patrick M. ,  THAYALAKHANDAN, Nagamany ,  ALEXANDER, Eric J.

    IPC: F02C7/04 ,  F02C7/057 ,  F02C7/06 ,  F02C9/16

    CPC classification number: F02C7/04 ,  B64D33/02 ,  B64D2033/0273 ,  F02C3/04 ,  F02C7/06 ,  F05D2220/323 ,  F05D2250/51 ,  F05D2250/80 ,  F05D2250/82

    Abstract: A gas turbine engine has a nose cone with a nose cone upstream end and an inlet housing including a plurality of separate flow paths at a housing upstream end which is downstream of the nose cone upstream end. The inlet housing includes a mixing portion downstream of the housing upstream end which mixes airflow from the separate flow paths, such that the airflow is generally around 360 degrees of a rotational axis of the gas turbine engine. A rotor and a turbine drive a shaft to drive the rotor with the shaft including a bearing mounted at a location downstream of the nose cone upstream end.

    Abstract translation: 燃气涡轮发动机具有鼻锥体，其具有鼻锥上游端，并且入口壳体在壳体上游端处包括多个分离的流动路径，其在鼻锥上游端的下游。 入口壳体包括在壳体上游端下游的混合部分，其混合来自分离的流动路径的气流，使得气流通常大约为燃气涡轮发动机的旋转轴线的360度。 转子和涡轮机驱动轴以驱动转子，其中轴包括安装在鼻锥上游端下游位置的轴承。

    SYSTEM AND METHOD FOR AFT MOUNT OF GAS TURBINE ENGINE
    2.
    发明申请
    SYSTEM AND METHOD FOR AFT MOUNT OF GAS TURBINE ENGINE 审中-公开
    用于汽轮机发动机尾部安装的系统和方法

    公开(公告)号：WO2014172000A3

    公开(公告)日：2014-10-23

    申请号：PCT/US2014/015124

    申请日：2014-02-06

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： ALEXANDER, Eric J.

    IPC: F02C7/20 ,  F16M5/00 ,  F16F7/00

    Abstract: The present disclosure is applicable to all vehicles having an engine mounted therein. In one embodiment, an aft mount system for a gas turbine engine is disclosed. The aft mount system includes a vehicle chassis and at least one flexible mounting member disposed within the vehicle chassis, wherein when a gas turbine engine is received within the vehicle chassis, an exhaust portion of the gas turbine engine is substantially mounted within the vehicle chassis through engagement with the at least one flexible mounting member.

    Abstract translation: 本公开适用于其中安装有发动机的所有车辆。 在一个实施例中，公开了用于燃气涡轮发动机的后安装系统。 后安装系统包括车辆底盘和设置在车辆底盘内的至少一个柔性安装构件，其中当燃气涡轮发动机容纳在车辆底盘内时，燃气涡轮发动机的排气部分基本上通过车辆底盘 与至少一个柔性安装构件接合。

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