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公开(公告)号：US20170191380A1
公开(公告)日：2017-07-06
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
CPC classification number: F01D5/3007 , F01D11/008 , F01D25/285 , F05D2230/68 , Y02T50/671
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：US09636789B2
公开(公告)日：2017-05-02
申请号：US15171554
申请日：2016-06-02
Applicant: General Electric Company
Inventor： James Bradford Holmes , James Robert Hollis , David Randolph Spracher , Wayne David Sullivan
CPC classification number: B23P15/04 , B23P15/02 , B23P19/027 , B23P19/04 , F01D5/005 , F01D5/14 , F01D5/3007 , F01D25/285 , F05D2230/60 , Y10T29/4932 , Y10T29/53983
Abstract: Various embodiments include methods adapted to displace turbomachine components from a location within a turbomachine. In some embodiments, a method of displacing a turbine bucket from a turbomachine wheel slot using a displacement apparatus, includes: detachably engaging an engagement arm of the displacement apparatus to the turbine bucket, the engagement arm attached to a linear actuator coupled to a body of the displacement apparatus, and the engagement arm adapted to be actuated in a first axial direction by the linear actuator; contacting the turbomachine wheel with at least two contacting portions of the body of the displacement apparatus; and displacing the turbine bucket from a position within a slot of the turbomachine wheel in the first axial direction by linearly actuating the engagement arm with the linear actuator.
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公开(公告)号：US09429041B2
公开(公告)日：2016-08-30
申请号：US14277232
申请日：2014-05-14
Applicant: General Electric Company
Inventor： James Bradford Holmes , James Robert Hollis , David Randolph Spracher , Wayne David Sullivan
IPC: F01D5/28 , F01D25/28 , B23P19/027 , B25B27/14 , F01D5/30
CPC classification number: B23P15/04 , B23P19/025 , B23P19/027 , B25B27/14 , F01D5/3007 , F01D25/285 , F05D2220/30 , Y10T29/4932 , Y10T29/5383
Abstract: Various embodiments include apparatuses adapted to displace components from a location within a turbomachine. In some embodiments an apparatus for displacing a component of a gas turbine from a first slot in a spacer disk includes a body including a mounting member configured to affixedly attach to a second slot of the spacer disk, a linear actuator coupled to the body and a displacement arm coupled to the linear actuator, the displacement arm actuatable in a first axial direction by the linear actuator to contact the component and displace the component relative to the first slot.
Abstract translation: 各种实施例包括适于从涡轮机内的位置移位部件的装置。 在一些实施例中，用于将燃气涡轮机的部件从间隔盘中的第一槽移位的装置包括主体，其包括构造成固定地附接到间隔盘的第二槽的安装构件，联接到主体的线性致动器和 位移臂联接到线性致动器，位移臂通过线性致动器在第一轴向方向上致动以接触部件并相对于第一槽移位部件。
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公开(公告)号：US09144866B2
公开(公告)日：2015-09-29
申请号：US13714856
申请日：2012-12-14
Applicant: General Electric Company
Inventor： James Bradford Holmes , James Robert Hollis , Wayne David Sullivan
CPC classification number: B23P19/042 , B23P11/00 , F01D9/023 , F01D25/285 , F05D2230/64 , F23R3/60 , F23R2900/00017 , F23R2900/00019 , Y10T29/49236 , Y10T29/53974
Abstract: Various embodiments include an apparatus for installing or removing a transition piece (TP) in a gas turbine. The apparatus can include: a control arm assembly sized to rest within an opening in the gas turbine; a guide system coupled to the control arm assembly, the guide system for transporting the TP within the opening in the gas turbine; and a counter balance coupled to the guide system, the counter balance for countering weight of the TP during the installing or the removing of the TP in the gas turbine.
Abstract translation: 各种实施例包括用于在燃气轮机中安装或移除过渡件（TP）的装置。 该装置可以包括：尺寸适于搁置在燃气涡轮机的开口内的控制臂组件; 连接到控制臂组件的引导系统，用于在燃气涡轮机的开口内输送TP的引导系统; 以及连接到引导系统的平衡平衡，用于在燃气轮机中的TP的安装或移除期间对抗TP的重量的对抗平衡。
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公开(公告)号：US20150260043A1
公开(公告)日：2015-09-17
申请号：US14206461
申请日：2014-03-12
Applicant: General Electric Company
Inventor： James Bradford Holmes , David Randolph Spracher , James Robert Hollis , Wayne David Sullivan
CPC classification number: F01D25/285 , B25B5/108 , B25B27/026 , F05D2230/70 , Y10T29/49318 , Y10T29/53796
Abstract: A tool for removing a component from a turbomachine is provided. The tool includes a body having an alignment portion and a connection portion. The alignment portion defines a longitudinal axis and a cross sectional shape complementary to a slot defined in a rotor wheel of the turbomachine. When the tool is positioned in the slot, the connection portion is configured to contact 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 substantially parallel to the longitudinal axis of the alignment portion.
Abstract translation: 提供了用于从涡轮机中去除组件的工具。 该工具包括具有对准部分和连接部分的主体。 对准部分限定纵向轴线和与限定在涡轮机的转子轮中的狭槽互补的横截面形状。 当工具位于槽中时，连接部分被配置成与部件接触。 该工具还包括连接到主体并且构造成在基本上平行于对准部分的纵向轴线的方向上将力传递到连接部分的力部分。
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Patent Agency Ranking
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：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：US20180066543A1
公开(公告)日：2018-03-08
申请号：US15258543
申请日：2016-09-07
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Thomas Michael Merlau , Stuart Craig Hanson , Brett Darrick Klingler , Wayne David Sullivan
CPC classification number: F01D25/285 , B66F3/08 , F01D5/005 , F01D25/24 , F01D25/243 , F01D25/265 , F01D25/28 , F05D2230/60 , F05D2230/644 , F05D2230/68 , F05D2230/70
Abstract: An apparatus for lifting an inner casing of a turbine includes a base, an arm, a guide roller, and an adjustment system. The arm has a first end and a second end, and is pivotally connected to the base intermediate the first end and the second end. The guide roller is operatively coupled to the first end of the arm to rotatably engage an exterior surface of the inner casing, and an adjustment system extending from the base and engaging the arm to change an angular position of the arm relative to the base and adjust a position of the guide roller relative to the exterior surface of the inner casing.
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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：US20160332267A1
公开(公告)日：2016-11-17
申请号：US15222009
申请日：2016-07-28
Applicant: General Electric Company
Inventor： James Bradford Holmes , James Robert Hollis , David Randolph Spracher , Wayne David Sullivan
CPC classification number: B23P15/04 , B23P19/025 , B23P19/027 , B25B27/14 , F01D5/3007 , F01D25/285 , F05D2220/30 , Y10T29/4932 , Y10T29/5383
Abstract: Various embodiments include a method of displacing a turbomachine component from position in a first slot of a turbomachine spacer disk. The method can include detachably affixing a mounting member of a displacement apparatus to a second slot in the gas turbomachine spacer disk using an attachment device, rotating a displacement arm of the displacement apparatus until the displacement arm contacts the turbomachine component, and displacing the turbomachine component from the position within the first slot by linearly actuating the displacement arm with a linear actuator.
Abstract translation: 各种实施例包括从涡轮机间隔盘的第一槽中的位置移动涡轮机组件的方法。 该方法可以包括使用附接装置将位移设备的安装构件可拆卸地固定到气体涡轮机间隔盘中的第二狭槽，旋转位移设备的位移臂，直到位移臂接触涡轮机组件，以及使涡轮机组件 通过用线性致动器线性致动位移臂，从第一槽内的位置。
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