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公开(公告)号：US20150174837A1
公开(公告)日：2015-06-25
申请号：US14568443
申请日：2014-12-12
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Don Mark Lipkin , Jonathan Matthew Lomas , Thomas Robert Reid , Jacob John Kittleson
IPC: B29C73/02
CPC classification number: B29C73/025 , B29K2103/04 , B29L2031/08
Abstract: A turbine component patch delivery system can include a support arm and a deposition tool supported by the support arm. The deposition tool can include a reservoir configured to house a turbine component patch material and a dispenser configured to dispense the turbine component patch material from the reservoir onto a surface of a turbine component.
Abstract translation: 涡轮机部件补片输送系统可以包括由支撑臂支撑的支撑臂和沉积工具。 沉积工具可以包括构造成容纳涡轮机部件补片材料的储存器和配置成将涡轮机部件补片材料从储存器分配到涡轮机部件的表面上的分配器。
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公开(公告)号：US11773752B2
公开(公告)日：2023-10-03
申请号：US17668643
申请日：2022-02-10
Applicant: General Electric Company
Inventor： Thomas Alan Mogle, II , Sandra Beverly Kolvick , Daryl Paul Capriotti
CPC classification number: F01D25/285 , F01D5/3007 , F01D25/246 , F05D2230/644 , F05D2240/14 , F05D2260/30
Abstract: a tooling assembly for installation relative to a first and second turbomachine component is provided. The tooling assembly includes an axial mounting portion removably couplable to the first turbomachine component. The axial mounting portion includes a first plate, a second plate spaced apart from the first plate, and at least one turnbuckle assembly that extends between, and is coupled to, the first plate and the second plate. At least one of the first plate and the second plate include a radial compression portion. The radial compression portion includes a compression bar radially movable relative to the axial mounting portion and configured to contact the second turbomachine component.
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公开(公告)号：US20230250735A1
公开(公告)日：2023-08-10
申请号：US17668643
申请日：2022-02-10
Applicant: General Electric Company
Inventor： Thomas Alan Mogle, II , Sandra Beverly Kolvick , Daryl Paul Capriotti
CPC classification number: F01D25/285 , F01D5/3007 , F01D25/246 , F05D2230/644 , F05D2240/14 , F05D2260/30
Abstract: a tooling assembly for installation relative to a first and second turbomachine component is provided. The tooling assembly includes an axial mounting portion removably couplable to the first turbomachine component. The axial mounting portion includes a first plate, a second plate spaced apart from the first plate, and at least one turnbuckle assembly that extends between, and is coupled to, the first plate and the second plate. At least one of the first plate and the second plate include a radial compression portion. The radial compression portion includes a compression bar radially movable relative to the axial mounting portion and configured to contact the second turbomachine component.
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24.发明授权公开(公告)号：US10934893B2
公开(公告)日：2021-03-02
申请号：US15779317
申请日：2015-12-31
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Sandra Beverly Kolvick , Jeffrey Scott LeBegue , Ansley Michelle Heard , Jesse Ellis Barton , Paul Robert Fernandez , Adrian Adam Klejc
Abstract: A combustor assembly lift system (200) comprises an exterior lift frame (220) comprising a base portion (222) and an arm portion (224), wherein the arm portion extends away from a base portion to form an interior, and, an interior combustor assembly engagement frame (240) at least partially disposed in the interior of the exterior lift frame and configured to temporarily secure to at least a portion of a combustor assembly. The interior combustor assembly engagement frame is connected to the base portion of the exterior lift frame.
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公开(公告)号：US10885689B2
公开(公告)日：2021-01-05
申请号：US16029143
申请日：2018-07-06
Applicant: General Electric Company
IPC: G06T11/00 , G06T11/60 , G06F40/169
Abstract: The present disclosure generally relates to a system that includes a processor configured to execute an augmented reality (AR) translator and visualizer system. The AR translator and visualizer system is configured to receive a language file that includes content, determine a background in the language file, remove the background, and retrieve the content from the language file. Moreover, the AR translator and visualizer system is configured to overlay the content onto a real world view via a display to form AR content that includes the content merged with the real world view. Furthermore the AR translator and visualizer system is configured to cause the system to display the real world view overlaid with the content via the display.
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Patent Agency Ranking
公开(公告)号：US10760434B2
公开(公告)日：2020-09-01
申请号：US15802859
申请日：2017-11-03
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Kevin Leon Bruce , Antoine Mastroianni
Abstract: A fixture for transferring turbine blades may include: a first body having an arcuate radially inward surface shaped to contact a rotor of a turbomachine, and a radially outward surface including a plurality of dovetail slots therein shaped to engage the dovetails of the plurality of turbine blades; and a first alignment aperture extending axially through the first body relative to a centerline axis, and positioned for alignment with a portion of the rotor wheel such that the plurality of dovetail slots of the first body are substantially axially aligned with the plurality of dovetail slots of the rotor wheel for at least partial transfer of the turbine blade thereto from the fixture, wherein the dovetails of the plurality of turbine blades are slidably removable from the plurality of dovetail slots of the first body for guided insertion into the plurality of dovetail slots of the rotor wheel.
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公开(公告)号：US10724385B2
公开(公告)日：2020-07-28
申请号：US15806479
申请日：2017-11-08
Applicant: General Electric Company
Inventor： Hubert Karol Wojtowicz , Adrian Adam Klejc , Sandra Beverly Kolvick
Abstract: Embodiments of the present disclosure relate to the installation or removal of turbine blades at a turbine blade base thereof. An apparatus according to the present disclosure can include: an operative head configured to engage an axial sidewall of a turbine blade base; and a mount removably coupled to a portion of a turbomachine assembly by a coupler, wherein the operative head is slidably coupled to the mount such that the operative selectively engages the axial sidewall of the turbine blade base, and wherein the operative head is shaped to impart an axial and a circumferential force against the turbine blade base.
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公开(公告)号：US10704421B2
公开(公告)日：2020-07-07
申请号：US15367863
申请日：2016-12-02
Applicant: General Electric Company
Inventor： Thomas Alan Mogle, II , Sandra Beverly Kolvick , Troy Lee Smith
Abstract: This disclosure provides tools for installing and removing a combustion liner in a combustion casing. A mounting frame has fasteners positioned circumferentially around an end casing surface of the combustion casing and removably attaches the mounting frame to the combustion casing. A positioning member has pushing surfaces and pulling surfaces distributed circumferentially around the combustion liner. An axial positioning mechanism engages the mounting frame and the positioning member along a common axis. The axial positioning mechanism incrementally positions the positioning member relative to the mounting frame by adjusting a positioning distance between the mounting frame and the positioning member.
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公开(公告)号：US10125634B2
公开(公告)日：2018-11-13
申请号：US14964780
申请日：2015-12-10
Applicant: General Electric Company
Inventor： Thomas Michael Merlau , Stuart Craig Hanson , Sandra Beverly Kolvick , Thomas Alan Mogle, II , Loy Milton Miller, Jr.
Abstract: A combustor assembly alignment system comprises an alignment plate comprising a plurality of alignment plate holes that align with a plurality of combustor assembly flange holes, an alignment plate securement system configured to secure the alignment plate to a combustor assembly flange by passing through a first alignment plate hole of the alignment plate and a first combustor assembly flange hole of the combustor assembly flange, and an alignment tube that extends away from the alignment plate, wherein a hollow interior of the alignment tube aligns with a second combustor assembly flange hole when the alignment plate is secured to the combustor assembly flange.
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公开(公告)号：US20180087407A1
公开(公告)日：2018-03-29
申请号：US15277354
申请日：2016-09-27
Applicant: General Electric Company
Inventor： Maxwell Evan Miller , Jason Matthew Clark , Sandra Beverly Kolvick
CPC classification number: F01D25/285 , F01D5/005 , F01D5/02 , F01D25/243 , F05D2230/72 , F05D2260/02
Abstract: A fixture for restraining a wheel of a turbomachine is provided. The fixture includes a dovetail section adapted for insertion into a dovetail slot of the wheel, and a mounting section located adjacent to, or formed integrally with, the dovetail section. At least one coupling ring is attached to a top of the mounting section. The at least one coupling ring is adapted to be secured to a stationary anchoring point via a restraint.
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