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公开(公告)号：US11014205B2
公开(公告)日：2021-05-25
申请号：US15730961
申请日：2017-10-12
Applicant: General Electric Company
Inventor： Hubert Karol Wojtowicz , Sandra Beverly Kolvick , Wayne David Sullivan
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：US20190338677A1
公开(公告)日：2019-11-07
申请号：US16516847
申请日：2019-07-19
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Daryl Paul Capriotti , Ansley Michelle Heard , Rachel Kate King , Travis Edwin Lipstein , Maithri Muddasani , Tewodros Fiseha Wondimu
Abstract: Mounting apparatuses for turbine airfoils of turbine systems are disclosed. The mounting apparatuses may include a body portion configured to be at least partially positioned between a first airfoil and a second airfoil of the turbine system, and an adjustable, first retention component formed on a first side of the body portion. The adjustable, first retention component may be configured to contact a portion of a suction side of the first airfoil of the turbine system. The mounting apparatuses may also include a second retention component formed on a second side of the body portion, opposite the first side. The second retention component may be configured to contact a portion of a pressure side of the second airfoil of the turbine system.
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公开(公告)号：US20190293405A1
公开(公告)日：2019-09-26
申请号：US15933614
申请日：2018-03-23
Applicant: General Electric Company
Inventor： Travis Edwin Lipstein , Sandra Beverly Kolvick
Abstract: A system and method for determining eccentricity of a casing and a rotor of a gas turbine includes a plurality of stationary distance detectors coupled to the casing at known circumferential positions and a rotating distance detector coupled to the rotor or a blade in or near an axial plane defined by the stationary distance detectors. The stationary distance detectors transmit wireless signals to one another to determine a first series of distance measurements between each pair of stationary distance detectors. The rotating distance detector transmits wireless signals to each of the stationary distance detectors, as the rotor is spun, to generate a second series of distance measurements. The measurements are transmitted, over a wireless local area network, to a remote computing device that processes the distance measurements into an eccentricity plot. An optional base station may be used to generate the wireless network.
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公开(公告)号：US10273814B2
公开(公告)日：2019-04-30
申请号：US14988223
申请日：2016-01-05
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Jean-Philippe Guillard , James Bradford Holmes , Wayne David Sullivan
Abstract: A tool for installing a turbomachine component in a first dovetail slot of a first component mount is provided. The tool may include a tool mount having a body for selective fixing in a second dovetail slot of a second component mount adjacent to the first component mount. The tool may also include a lever arm including a first portion, an intermediate pivot for pivotally engaging the tool mount, and a second portion for engaging the turbine component. Actuating the lever arm against the tool mount causes the second portion of the lever arm to install the turbomachine component into the first dovetail slot of the first component.
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公开(公告)号：US20180283214A1
公开(公告)日：2018-10-04
申请号：US15476224
申请日：2017-03-31
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Daryl Paul Capriotti , Ansley Michelle Heard , Rachel Kate King , Travis Edwin Lipstein , Maithri Muddasani , Tewodros Fiseha Wondimu
CPC classification number: F01D25/28 , B25B5/065 , B25B5/14 , F01D5/147 , F05D2220/32 , F05D2240/90 , F05D2260/30
Abstract: Mounting apparatuses for turbine airfoils of turbine systems are disclosed. The mounting apparatuses may include a body portion configured to be at least partially positioned between a first airfoil and a second airfoil of the turbine system, and an adjustable, first retention component formed on a first side of the body portion. The adjustable, first retention component may be configured to contact a portion of a suction side of the first airfoil of the turbine system. The mounting apparatuses may also include a second retention component formed on a second side of the body portion, opposite the first side. The second retention component may be configured to contact a portion of a pressure side of the second airfoil of the turbine system.
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Patent Agency Ranking
公开(公告)号：US20170274510A1
公开(公告)日：2017-09-28
申请号：US15082151
申请日：2016-03-28
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Stuart Craig Hanson , Wayne David Sullivan
CPC classification number: B25B27/0028 , B25B27/02 , F01D5/005 , F01D5/3007 , F01D5/3015 , F01D11/001 , F01D11/005 , F01D25/285 , F05D2230/70
Abstract: A tool for removing a component from a turbomachine is provided. The tool includes a body having a connection portion for engaging the component. The tool additionally includes a force section connected to the body and configured to transfer a force to the connection portion in a direction at an acute angle relative to longitudinal axis of a dovetail slot of a rotor wheel adjacent to the component.
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公开(公告)号：US20160201556A1
公开(公告)日：2016-07-14
申请号：US14594379
申请日：2015-01-12
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Kevin Leon Bruce , Matthew Ryan Ferslew , Stuart Craig Hanson , Thomas Michael Merlau , Joshua Michael Oden , Christopher Michael Penny
IPC: F02C1/00
CPC classification number: F01D25/285 , F01D5/3007 , F02C1/00 , F05D2230/64 , F05D2230/68 , F05D2230/70
Abstract: 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.
Abstract translation: 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。
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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
Applicant: GENERAL ELECTRIC COMPANY
IPC: F01D25/28
CPC classification number: F01D25/285 , F05D2230/64 , F05D2230/68 , F05D2230/70 , F05D2250/75 , F05D2260/31
Abstract: 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
Applicant: General Electric Company
Abstract: 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：US10265838B2
公开(公告)日：2019-04-23
申请号：US15082151
申请日：2016-03-28
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Stuart Craig Hanson , Wayne David Sullivan
Abstract: A tool for removing a component from a turbomachine is provided. The tool includes a body having a connection portion for engaging the component. The tool additionally includes a force section connected to the body and configured to transfer a force to the connection portion in a direction at an acute angle relative to longitudinal axis of a dovetail slot of a rotor wheel adjacent to the component.
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