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    COMBUSTOR MOUNTING STRUCTURES FOR GAS TURBINE ENGINES
    1.
    发明申请
    COMBUSTOR MOUNTING STRUCTURES FOR GAS TURBINE ENGINES 有权

    公开(公告)号：US20210003284A1

    公开(公告)日：2021-01-07

    申请号：US16585836

    申请日：2019-09-27

    Applicant: United Technologies Corporation

    Inventor： Milton A. Fong ,  Russell B. Hanson ,  Eric D. Gray ,  Michael D. Collier ,  Nathan K. Galle ,  Salvatore Siciliano

    IPC: F23R3/60 ,  F02C3/14

    Abstract: Combustor mounting structures for gas turbine engines are described. The combustor mounting structures include a shell portion defining an outer ring arranged at an outer radius relative to a central axis, a combustor connection element defining an inner ring arranged at an inner radius that is less than the outer radius relative to the central axis, and a plurality of struts extending radially between and connecting the shell portion to the combustor connection element, wherein one or more flow apertures are defined between the shell portion and the combustor connection element in a radial direction and between adjacent struts of the plurality of struts in a circumferential direction.

    Deep rolling tool with force adjustment
    2.
    发明授权
    Deep rolling tool with force adjustment 有权
    深度滚动工具，带力调节

    公开(公告)号：US09566638B2

    公开(公告)日：2017-02-14

    申请号：US14567562

    申请日：2014-12-11

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Justin R. Hawkes ,  Eric D. Gray ,  Tahany I. El-Wardany ,  Daniel V. Viens

    IPC: B21H7/16 ,  B23P9/02 ,  B21B27/02 ,  B21B31/02 ,  B21B31/16

    CPC classification number: B21H7/16 ,  B21B27/02 ,  B21B31/02 ,  B21B31/16 ,  B23P9/02

    Abstract: A device and methods are provided for deep rolling. In one embodiment, a deep rolling tool for applying compressive stress with rolling elements includes a flexible fork having a base section and a plurality of fork arms and a plurality of rolling elements, wherein each rolling element is mounted to a fork arm with eccentric roller bushings, wherein each rolling element is mounted at the distal end of a fork arm, and wherein the rolling elements are configured to apply a compressive stress to articles received by the deep rolling tool.

    Abstract translation: 为深层轧制提供了一种装置和方法。 在一个实施例中，用于用滚动元件施加压缩应力的深度滚动工具包括具有基部和多个叉臂和多个滚动元件的柔性叉，其中每个滚动元件安装到具有偏心辊套的叉臂 其中，每个滚动元件安装在叉臂的远端，并且其中所述滚动元件构造成对由所述深滚动工具接收的物品施加压缩应力。

    Airfoil with Thickened Root and Fan and Engine Incorporating Same
    5.
    发明申请
    Airfoil with Thickened Root and Fan and Engine Incorporating Same 审中-公开
    具有较厚根和风机的机翼和引擎相同

    公开(公告)号：US20160003048A1

    公开(公告)日：2016-01-07

    申请号：US14761738

    申请日：2013-12-18

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Eric D. Gray ,  Razvan Virgil Florea ,  Mark B. Stucky ,  Ray-Sing Lin

    IPC: F01D5/14 ,  F01D5/02 ,  F02C3/04

    Abstract: In accordance with one aspect of the disclosure, an airfoil is disclosed. The airfoil may include a platform and a blade extending from the platform. The blade may have a root proximate the platform and a tip radially outward from the platform. The root may have a greater thickness than a cross-section at about a quarter-span of the blade or greater.

    Abstract translation: 根据本公开的一个方面，公开了一种翼型件。 翼型件可以包括从平台延伸的平台和叶片。 叶片可以具有靠近平台的根部和从平台径向向外的尖端。 根部可以具有比叶片大约四分之一跨度处的横截面更大的厚度或更大的厚度。

    Non-contact seal with non-straight spring beam(s)
    6.
    发明授权
    Non-contact seal with non-straight spring beam(s) 有权

    公开(公告)号：US10830081B2

    公开(公告)日：2020-11-10

    申请号：US15651261

    申请日：2017-07-17

    Applicant: United Technologies Corporation

    Inventor： Conway Chuong ,  Tara L. D'Ambruoso ,  Dwayne K. Mecklenburg ,  Peter E. Gunderson ,  Eric D. Gray

    IPC: F01D11/02 ,  F16J15/44

    Abstract: An assembly includes a plurality of seal shoes, a seal base and a plurality of spring elements. The seal shoes are arranged around an axis in an annular array. The seal base circumscribes the annular array of the seal shoes. Each of the spring elements is radially between and connects a respective one of the seal shoes to the seal base. A first of the spring elements includes a first mount, a second mount and a spring beam. The first mount is connected to the first seal shoe. The second mount is connected to the seal base and disposed a circumferential distance away from the first mount. The spring beam extends longitudinally along a non-straight centerline between and connected to the first mount and the second mount.

    Tandem tip blade
    9.
    发明授权
    Tandem tip blade 有权

    公开(公告)号：US10151322B2

    公开(公告)日：2018-12-11

    申请号：US15160165

    申请日：2016-05-20

    Applicant: United Technologies Corporation

    Inventor： Dmytro Mykolayovych Voytovych ,  Alexander Staroselsky ,  Eric D. Gray

    IPC: F02C3/04 ,  F04D29/32 ,  F02K3/06 ,  F04D29/38 ,  F01D5/14 ,  F01D5/22

    Abstract: A tandem tip blade includes a main blade body, a front blade and a rear blade. The front blade extends from a main body end. Each of a front blade pressure and a front blade suction side extends between a front blade leading edge and a front blade trailing edge and a front blade tip extending from the front blade pressure side to the front blade suction side. The rear blade extends from the main body end. Each of a rear blade pressure side and a rear blade suction side extends between a rear blade leading edge and a rear blade trailing edge, and a rear blade tip extending from the rear blade pressure side to the rear blade suction side.

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