MANIPULATION OF TURBOMACHINE COMBUSTORS
    23.
    发明申请
    MANIPULATION OF TURBOMACHINE COMBUSTORS 审中-公开
    涡轮搅拌机的操作

    公开(公告)号:US20160376926A1

    公开(公告)日:2016-12-29

    申请号:US15258552

    申请日:2016-09-07

    IPC分类号: F01D25/28

    摘要: Embodiments of the present disclosure relate to the manipulation of turbomachine combustors. An apparatus according to the present disclsoure can include: a bracket body including an operative head configured to removably attach a turbomachine combustor; a rotatable joint rotatably coupled to the bracket body through a gear bearing, wherein the gear bearing is configured to rotate the bracket body relative to the rotatable joint; and a suspended member rotatably coupled to the rotatable joint at a first end, and coupled to a suspension joint at a second end, wherein the rotatable joint rotates the gear bearing and the bracket body relative to the suspended member to center the gear bearing about a predetermined axis of rotation.

    摘要翻译: 本公开的实施例涉及涡轮机燃烧器的操作。 根据本发明的装置可以包括:托架主体,其包括构造成可移除地附接涡轮机燃烧器的操作头部; 可旋转接头,其通过齿轮轴承可旋转地联接到所述支架主体,其中所述齿轮轴承构造成相对于所述可旋转接头旋转所述支架主体; 以及悬挂构件,其在第一端处可旋转地联接到所述可旋转接头,并且在第二端处联接到悬架接头,其中所述可旋转接头相对于所述悬挂构件旋转所述齿轮轴承和所述支架主体,以使所述齿轮轴承围绕 预定的旋转轴。

    Axial Retention Assembly for Combustor Components of a Gas Turbine Engine

    公开(公告)号:US20210047967A1

    公开(公告)日:2021-02-18

    申请号:US16539164

    申请日:2019-08-13

    IPC分类号: F02C7/20 F01D25/28

    摘要: The present subject matter is directed to an axial retention assembly for combustor components of a gas turbine engine. The axial retention assembly may include a combustor having include a liner defining a liner aperture extending therethrough. Additionally, the combustor may further include a sleeve defining a sleeve aperture extending therethrough, with the sleeve positioned radially outward from and at least partially circumferentially positioned around the liner. Furthermore, the axial retention assembly may include a frame having a mounting projection positioned within the sleeve aperture. Moreover, the axial retention assembly may include a clamp plate adjustably coupled to the frame. In addition, the axial retention assembly may include a clamp plate adjustment rod extending through the liner aperture and threadingly engaging the clamp plate such that relative movement between the liner and the sleeve along the axial centerline is reduced.

    TURBOMACHINE COMPONENT HANDLING ASSEMBLY
    25.
    发明申请

    公开(公告)号:US20190010026A1

    公开(公告)日:2019-01-10

    申请号:US15635363

    申请日:2017-06-28

    IPC分类号: B66C1/10 B66C1/62 F02C7/20

    摘要: The present disclosure is directed to a component handling assembly. The component handling assembly includes a base member, an arm pivotably coupled to the base member, and a beam rotatably coupled to the base member. The component handling assembly also includes a counterweight rotatably coupled to a first end of the beam. The component handling assembly further includes a coupling assembly coupled to a second end of the beam. The coupling assembly is configured for coupling to a component. Rotating the counterweight in a first direction rotates the beam, the coupling assembly, and the component in a second direction.

    TOOL AND METHOD FOR DECOUPLING CROSS-FIRE TUBE ASSEMBLIES IN GAS TURBINE ENGINES

    公开(公告)号:US20180100654A1

    公开(公告)日:2018-04-12

    申请号:US15289412

    申请日:2016-10-10

    IPC分类号: F23R3/60

    摘要: A tool for decoupling a telescoping tube from a first liner of a gas turbine engine is disclosed. The tool includes a rod partially positioned in a telescoping tube passage. The rod includes a first portion having a non-circular cross-section and a threaded second portion positioned in a second combustion chamber. A plug couples to the rod and engages a first side surface of the telescoping tube. A base defining a base passage extending therethrough is positioned in a second combustion chamber. The base passage includes a first portion having a non-circular cross-section. The first portion of the rod is at least partially positioned in the first portion of the base passage. A handle threadingly couples to the rod. Rotating the handle in a first direction moves the handle along the rod toward the first combustor to decouple the telescoping tube from the first liner.

    FIXTURE AND METHOD FOR INSTALLING TURBINE BUCKETS
    29.
    发明申请
    FIXTURE AND METHOD FOR INSTALLING TURBINE BUCKETS 审中-公开
    用于安装涡轮马桶的装置和方法

    公开(公告)号:US20160201556A1

    公开(公告)日:2016-07-14

    申请号:US14594379

    申请日:2015-01-12

    IPC分类号: F02C1/00

    摘要: A fixture and method for installing turbine buckets is disclosed. The fixture is adapted for mounting a plurality of turbine buckets with dovetails to a rotor wheel of a turbomachine that is separated from an adjacent rotor wheel by a spacer wheel, the rotor wheel and the spacer wheel each having a plurality of circumferentially aligned dovetail slots, the fixture includes: a turbine bucket holder having a dovetail that is configured to engage with one of the dovetail slots of the spacer wheel. The profile of a bucket holder dovetail slot substantially aligns the dovetail of the turbine bucket with a dovetail slot of the rotor wheel for at least partial transfer of a turbine bucket thereto.

    摘要翻译: 公开了一种用于安装涡轮机叶片的固定装置和方法。 该固定装置适用于将具有燕尾榫的多个涡轮机叶片安装到涡轮机的转子轮上,涡轮机通过间隔轮与相邻的转子轮分开,转子轮和间隔轮每个具有多个周向对准的燕尾槽, 所述固定装置包括:涡轮机桶保持器,其具有燕尾形构造成与所述间隔轮的所述燕尾槽中的一个啮合。 铲斗保持器燕尾槽的轮廓基本上对准涡轮机桶的燕尾榫与转子轮的燕尾槽,用于将涡轮机桶至少部分地传递到其上。