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    SEALS FOR A CIRCUMFERENTIAL STOP RING IN A TURBINE EXHAUST CASE
    1.
    发明申请
    SEALS FOR A CIRCUMFERENTIAL STOP RING IN A TURBINE EXHAUST CASE 有权
    在涡轮机排气箱中的环形止动环的密封

    公开(公告)号：US20140248128A1

    公开(公告)日：2014-09-04

    申请号：US13730899

    申请日：2012-12-29

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Matthew Budnick ,  Conway Chuong ,  Jonathan A. Scott

    IPC: F01D11/00

    CPC classification number: F01D11/005 ,  F01D25/162 ,  F01D25/246

    Abstract: A turbine seal system comprises an annular structural frame, a circumferential ring, a fairing and a seal. The circumferential ring is joined to the annular structural frame. The fairing is disposed within the annular structural frame and is engaged with the circumferential ring to limit circumferential rotation of the fairing with respect to the annular structural frame. The seal extends between the fairing and the circumferential ring. In one embodiment, the structural component comprises a ring-strut-ring turbine exhaust case.

    Abstract translation: 涡轮密封系统包括环形结构框架，圆周环，整流罩和密封件。 周向环连接到环形结构框架。 整流罩设置在环形结构框架内并与周向环接合以限制整流罩相对于环形结构框架的周向旋转。 密封件在整流罩和周向环之间延伸。 在一个实施例中，结构部件包括环形支撑环式涡轮机排气箱。

    Case coupling and assembly
    2.
    发明授权
    Case coupling and assembly 有权

    公开(公告)号：US10801367B2

    公开(公告)日：2020-10-13

    申请号：US16110710

    申请日：2018-08-23

    Applicant: United Technologies Corporation

    Inventor： Jonathan A. Scott ,  Darren M. Smith

    IPC: F01D25/24 ,  F01D21/00 ,  F02K1/80 ,  F01D25/28

    Abstract: A system and method for coupling cases associated with an engine of an aircraft. A first case includes a first plurality of threads. A second case includes a second plurality of threads. A coupler includes a third plurality of threads and a fourth plurality of threads. An interface is configured to align the first case and the second case before the first plurality of threads engage the third plurality of threads or the second plurality of threads engage the fourth plurality of threads.

    TURBINE CASE COUPLING
    4.
    发明申请
    TURBINE CASE COUPLING 审中-公开
    涡轮机联轴器

    公开(公告)号：US20160298492A1

    公开(公告)日：2016-10-13

    申请号：US14685144

    申请日：2015-04-13

    Applicant: United Technologies Corporation

    Inventor： Darren M. Smith ,  Jonathan A. Scott

    IPC: F01D25/24

    CPC classification number: F01D25/24 ,  F02K1/80 ,  F05D2250/25 ,  F05D2250/281 ,  F05D2260/30 ,  F16B7/06 ,  F16B7/185 ,  F16B33/004 ,  F16B41/002 ,  Y10T403/7067

    Abstract: Aspects of the disclosure are directed to a first case including a first plurality of threads, a second ease including a second plurality of threads, an interface configured to provide for at least one of anti-rotation or alignment with respect to the first case and the second ease, and a nut including a third plurality of threads configured to engage with the first plurality of threads and a fourth plurality of threads configured to engage with the second plurality of threads.

    Abstract translation: 本公开的方面涉及包括第一多个线程的第一情况，包括第二多个线程的第二容易性，被配置为提供相对于第一壳体的抗旋转或对准中的至少一个的接口，以及 以及包括构造成与所述第一多个螺纹接合的第三多个螺纹的螺母和被配置成与所述第二多个螺纹接合的第四多个螺纹。

    CASE COUPLING AND ASSEMBLY
    6.
    发明申请
    CASE COUPLING AND ASSEMBLY 审中-公开
    案例联系和组装

    公开(公告)号：US20160369655A1

    公开(公告)日：2016-12-22

    申请号：US14746322

    申请日：2015-06-22

    Applicant: United Technologies Corporation

    Inventor： Jonathan A. Scott ,  Darren M. Smith

    IPC: F01D25/24 ,  F01D21/00 ,  F01D25/26

    CPC classification number: F01D25/243 ,  F01D21/003 ,  F01D25/26 ,  F02K1/80 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2230/64 ,  F05D2250/281 ,  F05D2260/30 ,  Y02T50/671

    Abstract: Aspects of the disclosure are directed to coupling cases associated with an engine of an aircraft. A first case includes a first plurality of threads. A second case includes a second plurality of threads. A coupler includes a third plurality of threads and a fourth plurality of threads. An interface is configured to align the first case and the second case before the first plurality of threads engage the third plurality of threads or the second plurality of threads engage the fourth plurality of threads.

    Abstract translation: 本公开的方面涉及与飞行器的发动机相关联的联接情况。 第一种情况包括第一组多个线程。 第二种情况包括第二组多个线程。 联接器包括第三多个螺纹和第四多个螺纹。 接口被配置为在第一多个螺纹接合第三多个螺纹之前对准第一壳体和第二壳体，或者第二多个螺纹接合第四多个螺纹。

    CASE COUPLING AND ASSEMBLY
    7.
    发明申请
    CASE COUPLING AND ASSEMBLY 审中-公开

    公开(公告)号：US20190010826A1

    公开(公告)日：2019-01-10

    申请号：US16110710

    申请日：2018-08-23

    Applicant: United Technologies Corporation

    Inventor： Jonathan A. Scott ,  Darren M. Smith

    IPC: F01D25/24 ,  F02K1/80 ,  F01D21/00 ,  F01D25/26

    Abstract: A system and method for coupling cases associated with an engine of an aircraft. A first case includes a first plurality of threads. A second case includes a second plurality of threads. A coupler includes a third plurality of threads and a fourth plurality of threads. An interface is configured to align the first case and the second case before the first plurality of threads engage the third plurality of threads or the second plurality of threads engage the fourth plurality of threads.

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