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    GEARBOX MOUNTING ASSEMBLY
    2.
    发明申请
    GEARBOX MOUNTING ASSEMBLY 审中-公开
    齿轮安装总成

    公开(公告)号：WO2014137575A1

    公开(公告)日：2014-09-12

    申请号：PCT/US2014/016757

    申请日：2014-02-18

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： MARTIN, Octavio ,  NIGGEMEIER, Chris J.

    IPC: F02C7/36 ,  F01D15/12

    CPC classification number: F02C7/32 ,  F01D25/28 ,  F02C3/04 ,  F05D2220/32 ,  F05D2260/36 ,  F05D2260/4031 ,  Y02T50/671

    Abstract: An accessory gearbox mounting assembly includes a gearbox bracket engaged to a case bracket mounted on an engine case. The case bracket includes a first boss receivable within a first cavity of the engine case and a locator opening through the first boss. The gearbox bracket is mountable to a gearbox case and includes a pin receivable within the locator opening for transferring load from the gearbox bracket to the case bracket.

    Abstract translation: 附件齿轮箱安装组件包括与安装在发动机壳体上的壳体托架接合的齿轮箱支架。 壳体托架包括可容纳在发动机壳体的第一腔内的第一凸台和通过第一凸台开口的定位器。 齿轮箱支架可安装到齿轮箱壳体上，并包括可定位器开口内的销子，用于将负载从齿轮箱支架传送到壳体托架。

    MID-TURBINE FRAME WITH OIL SYSTEM MOUNTS
    3.
    发明申请
    MID-TURBINE FRAME WITH OIL SYSTEM MOUNTS 审中-公开
    具有油系统的中涡轮框架

    公开(公告)号：WO2014011982A1

    公开(公告)日：2014-01-16

    申请号：PCT/US2013/050263

    申请日：2013-07-12

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： MARTIN, Octavio ,  FARAH, Jorge, I.

    IPC: F02C7/00 ,  F02C7/36 ,  F02C7/32

    CPC classification number: F02C7/20 ,  F01D25/18 ,  F01D25/28 ,  F02C7/32 ,  Y02T50/671 ,  Y10T29/49234

    Abstract: A gas turbine engine includes a combustor, a first turbine section in fluid communication with the combustor, a second turbine section in fluid communication with the first turbine section, and a mid-turbine frame located axially between the first turbine section and the second turbine section. An oil system includes a first oil system component that houses oil. A first connector mechanically connects the first oil system component to the mid-turbine frame.

    Abstract translation: 燃气涡轮发动机包括燃烧器，与燃烧器流体连通的第一涡轮机部分，与第一涡轮机部分流体连通的第二涡轮机部分和轴向位于第一涡轮机部分和第二涡轮部分之间的中间涡轮机机架 。 油系统包括容纳油的第一油系组件。 第一连接器将第一油系统部件机械地连接到中涡轮机架。

    BOSS-MOUNTED GEARBOX LINK COMPRISING A BRACKET WITH AN INTEGRATED SHEAR NECK
    8.
    发明公开
    BOSS-MOUNTED GEARBOX LINK COMPRISING A BRACKET WITH AN INTEGRATED SHEAR NECK 审中-公开
    包括带有一体式剪钳的支架的BOSS挂接式齿轮箱链接

    公开(公告)号：EP3287624A1

    公开(公告)日：2018-02-28

    申请号：EP17187570.1

    申请日：2017-08-23

    Applicant: United Technologies Corporation

    Inventor： MARTIN, Octavio

    IPC: F02C7/32

    CPC classification number: F16H57/025 ,  F01D25/28 ,  F02C7/32 ,  F05D2220/323 ,  F05D2260/30 ,  F05D2260/311 ,  F16H57/032 ,  Y02T50/671

    Abstract: Aspects of the disclosure are directed to a system (200) associated with an aircraft engine (10), comprising a gearbox (204), a link (210) coupled to the gearbox (204), and a bracket (216) coupled to the link (210), where the bracket (216) includes at least one notch (436a) formed in the bracket (216) to provide a pilot for a fuse trigger, and where a portion (446a, 446b) of the bracket (216) contained within the at least one notch (436a, 436b) breaks away from the bracket (216) when the system (200) experiences a load that is less than a nominal load associated with a fan blade out event of the aircraft engine (10).

    Abstract translation: 本公开的多个方面针对与飞机发动机（10）相关联的系统（200），所述系统包括变速箱（204），联接到齿轮箱（204）的联杆（210）以及联接到 其中所述支架（216）包括形成在所述支架（216）中的至少一个凹口（436a）以提供用于保险丝触发器的引导器，并且其中所述支架（216）的一部分（446a，446b） 当所述系统（200）经受小于与所述飞机发动机（10）的风扇叶片断开事件相关联的额定负载时，所述至少一个凹口（436a，436b）中的至少一个凹口（436a，436b） 。

    MID-TURBINE FRAME WITH OIL SYSTEM MOUNTS
    9.
    发明公开
    MID-TURBINE FRAME WITH OIL SYSTEM MOUNTS 审中-公开
    带油系统支架的中型涡轮机机架

    公开(公告)号：EP2872762A1

    公开(公告)日：2015-05-20

    申请号：EP13817570.8

    申请日：2013-07-12

    Applicant: United Technologies Corporation

    Inventor： MARTIN, Octavio ,  FARAH, Jorge, I.

    IPC: F02C7/00 ,  F02C7/36 ,  F02C7/32

    CPC classification number: F02C7/20 ,  F01D25/18 ,  F01D25/28 ,  F02C7/32 ,  Y02T50/671 ,  Y10T29/49234

    Abstract: A gas turbine engine includes a combustor, a first turbine section in fluid communication with the combustor, a second turbine section in fluid communication with the first turbine section, and a mid-turbine frame located axially between the first turbine section and the second turbine section. An oil system includes a first oil system component that houses oil. A first connector mechanically connects the first oil system component to the mid-turbine frame.

    Abstract translation: 燃气涡轮发动机包括燃烧器，与燃烧器流体连通的第一涡轮部分，与第一涡轮部分流体连通的第二涡轮部分以及轴向位于第一涡轮部分和第二涡轮部分之间的中间涡轮机框架 。 油系统包括容纳油的第一油系统组件。 第一连接器将第一机油系统部件机械连接至中间涡轮机机架。

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