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公开(公告)号：US10414005B2
公开(公告)日：2019-09-17
申请号：US15302239
申请日：2014-04-09
申请人： General Electric Company , Adrian Adam Klejc , Stuart Craig Hanson , John William Herbold , James Bradford Holmes , Sandra Beverly Kolvick , Thomas Alan Mogle, II , Robert Edward Huth , Lukasz Sajdak
发明人： Adrian Adam Klejc , Stuart Craig Hanson , John William Herbold , James Bradford Holmes , Sandra Beverly Kolvick , Thomas Alan Mogle, II , Robert Edward Huth , Lukasz Sajdak
摘要： An apparatus and method for servicing a combustion liner in a combustion case of a turbine is provided. The apparatus includes an elongated bar having a handle at one end and a force applying member at an opposing end of the elongated bar. An attachment member is configured for attachment to a flange of the combustion case. The attachment member is also configured for pivotal attachment to the elongated bar. The apparatus is configured to apply a radially outward force on a downstream portion of the combustion liner when a radially inward force is applied to the handle.
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公开(公告)号：US11746678B1
公开(公告)日：2023-09-05
申请号：US17977062
申请日：2022-10-31
IPC分类号： F01D25/28
CPC分类号： F01D25/285 , F05D2230/64 , F05D2230/68 , F05D2230/70 , F05D2250/75 , F05D2260/31
摘要： An apparatus configured to support a diffuser segment during removal from and installation into an assembly. The apparatus includes a body having two or more supports and at least two clamp rods. The clamp rods each extend from a first end to a second end. The body defines a pocket extending between the supports on a first side of the clamp rods. An end clamp releasably mates with the second end of each clamp rod. The end clamp has a foot extending into the first side of the clamp rod. A wheel is received within each support. The pocket and the foot of each end clamp releasably retain a diffuser segment and the wheels rotate to allow the diffuser segment to be removed without damaging a surface coating of the diffuser segment.
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公开(公告)号：US20230101193A1
公开(公告)日：2023-03-30
申请号：US17490339
申请日：2021-09-30
摘要： A tool for removing a coating from an interior surface of a component. The tool includes a rotary device; a grinding attachment attached to the rotary device; a tool holder configured to: set an axial position of the grinding attachment coupled to the rotary device over the coating on the interior surface of the component; and set a radial position of the grinding attachment coupled to the rotary device, the radial position defining a cutting depth of the grinding attachment into the coating on the interior surface of the component; and a wheel assembly coupled to the tool holder for guiding the tool holder about an interior perimeter of the component.
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公开(公告)号：US10969106B2
公开(公告)日：2021-04-06
申请号：US16539164
申请日：2019-08-13
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.
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公开(公告)号：US20150147151A1
公开(公告)日：2015-05-28
申请号：US14088720
申请日：2013-11-25
发明人： Thomas Alan Mogle, II , Kyle Joseph Conger , Michael Alan Davi , Stuart Craig Hanson , Robert Joseph Rohrssen
CPC分类号： F01D25/285 , B25B11/02 , B25H1/0007 , B64D27/26 , B64D2027/262 , B66F3/22 , B66F7/22 , F02C7/20 , F05D2220/32 , F05D2230/60 , F16M11/125 , Y10T29/4978
摘要： Methods for the positioning of equipment are disclosed. One method of the present disclosure can include substantially aligning an equipment support structure with an equipment fixture point of a casing structure; adjusting the equipment support structure to have a selected height and a selected angle; sliding the equipment support structure across a platform having the selected height and the selected angle to reach the equipment fixture point; and coupling a piece of equipment to one of the equipment support structure and the equipment fixture point.
摘要翻译： 公开了设备定位的方法。 本公开的一种方法可以包括将设备支撑结构与壳体结构的设备固定点基本上对准; 调整设备支撑结构以选择高度和选定角度; 将设备支撑结构滑过具有所选高度和所选角度的平台以到达设备固定点; 并将一件设备连接到设备支撑结构和设备固定点之一。
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公开(公告)号：US12025022B2
公开(公告)日：2024-07-02
申请号：US17734466
申请日：2022-05-02
IPC分类号： F01D25/28
CPC分类号： F01D25/285 , F05D2230/70
摘要： Tooling assemblies and methods are provided. A tooling assembly includes a first plate, a second plate spaced apart from the first plate, and one or more members extending between the first plate and the second plate. The tooling assembly further includes a plurality of blocks mounted to the one or more members and arranged in one or more rows between the first plate and the second plate. The at least one block in the plurality of blocks defines an opening that corresponds with an exterior shape of a mounting portion of the rotor blade.
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公开(公告)号：US20210047967A1
公开(公告)日：2021-02-18
申请号：US16539164
申请日：2019-08-13
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.
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公开(公告)号：US10472990B2
公开(公告)日：2019-11-12
申请号：US15345588
申请日：2016-11-08
摘要： Various embodiments include apparatuses for performing maintenance on a gas turbine (GT) nozzle, along with related methods. One apparatus can include: a nozzle engagement sled for releasably engaging the nozzle, the nozzle engagement sled including: a sled body; a locking member coupled with the sled body, the locking member sized to complement a slot in the nozzle; a sled slot within a side of the sled body, the sled slot for engaging a rail within the GT; and at least one wheel for transporting the sled body within the GT.
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9.发明申请公开(公告)号：US20180223694A1
公开(公告)日：2018-08-09
申请号：US15425063
申请日：2017-02-06
摘要： Methods of replacing flex seals in exhaust frames of turbine systems are disclosed. The method may include removing a section of an outer casing of an exhaust frame to form an opening within the outer casing. The section may be formed within a flow path of the exhaust frame. The method may also include removing the flex seal from the exhaust frame via the opening formed within the outer casing, inserting a distinct flex seal within the exhaust frame via the opening formed within the outer casing, and covering the opening formed within the outer casing of the exhaust frame.
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公开(公告)号：US20160221091A1
公开(公告)日：2016-08-04
申请号：US14612865
申请日：2015-02-03
CPC分类号： B23D47/02 , B23D47/08 , F01D25/246 , F05D2230/10
摘要： A cutting tool for cutting a blade mount ring segment from a ring segment slot in a turbomachine casing having a plurality of ring segment slots along an inclined surface is provided. The cutting tool includes a motor; a cutting blade driven by the motor to cut the ring segment; and a support element for supporting the motor. A guide for guiding a cutting tool circumferentially relative to the ring segment includes: a rip fence extending from the support element and including a slide member for slidingly engaging a respective empty ring slot that is axially displaced in the turbomachine casing from the slot in which the ring segment is positioned, and at least one incline compensating member coupled to the support element for slidingly engaging the inclined surface of the turbomachine casing and positioning the support element such that the cutting element of the cutting tool cuts the ring segment.
摘要翻译： 提供了一种用于从涡轮机壳体中的环形段狭槽切割刀片安装环段的切削工具，其具有沿着倾斜表面的多个环形段狭槽。 切割工具包括电机; 由电机驱动的切割刀片切割环段; 以及用于支撑马达的支撑元件。 用于相对于所述环段周向引导切削工具的引导件包括：从所述支撑元件延伸并且包括滑动构件的滑动构件，所述滑动构件用于与所述涡轮机壳体中轴向移位的相应的空环槽滑动接合， 环段被定位，并且至少一个倾斜补偿构件联接到支撑元件，用于滑动地接合涡轮机壳体的倾斜表面并定位支撑元件，使得切割工具的切割元件切割环形段。
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