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公开(公告)号：US09677428B2
公开(公告)日：2017-06-13
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.
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公开(公告)号：US20150328729A1
公开(公告)日：2015-11-19
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: B23P19/027 , B23P19/02
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：US20140096354A1
公开(公告)日：2014-04-10
申请号：US13645068
申请日：2012-10-04
Applicant: GENERAL ELECTRIC COMPANY
CPC classification number: F01D25/285 , B66C17/06
Abstract: Various embodiments include a service apparatus for a turbomachine. The service apparatus can include: a frame for coupling to an opening in the turbomachine; a bridge member operably coupled to the frame and spanning a width of the frame, the bridge member being substantially movable along a length of the frame; and a crane member operably coupled to the bridge member, the crane member being substantially movable along the width of the frame, wherein the crane member includes at least one attachment device for attaching to an object within the turbomachine.
Abstract translation: 各种实施例包括用于涡轮机的服务装置。 服务设备可以包括：用于联接到涡轮机中的开口的框架; 桥接构件，其可操作地联接到所述框架并横跨所述框架的宽度，所述桥接构件基本上可沿所述框架的长度移动; 以及起重机构件，其可操作地联接到所述桥构件，所述起重机构件可沿所述框架的宽度基本上移动，其中所述起重机构件包括用于附接到所述涡轮机内的物体的至少一个附接装置。
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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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公开(公告)号：US09381602B2
公开(公告)日：2016-07-05
申请号：US14277222
申请日：2014-05-14
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 apparatuses adapted to displace turbomachine components from a location within a turbomachine. In some embodiments apparatuses for displacing a turbine bucket from a turbomachine wheel slot include a body having at least two contacting portions for contacting the turbomachine wheel, a linear actuator coupled to the body, and an engagement arm for engaging the turbine bucket, the engagement arm coupled to the linear actuator and adapted to be actuated in a first axial direction by the linear actuator.
Abstract translation: 各种实施例包括适于从涡轮机内的位置置换涡轮机组件的装置。 在一些实施例中，用于将涡轮机叶轮从涡轮机轮槽移位的装置包括具有至少两个用于接触涡轮机轮的接触部分的主体，联接到主体的线性致动器和用于接合涡轮机叶片的接合臂，接合臂 耦合到线性致动器并且适于通过线性致动器在第一轴向方向上致动。
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Patent Agency Ranking
公开(公告)号：US20150328728A1
公开(公告)日：2015-11-19
申请号：US14277222
申请日：2014-05-14
Applicant: General Electric Company
Inventor： James Bradford Holmes , James Robert Hollis , David Randolph Spracher , Wayne David Sullivan
IPC: B23P19/027 , B23P15/02 , B23P19/04
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 apparatuses adapted to displace turbomachine components from a location within a turbomachine. In some embodiments apparatuses for displacing a turbine bucket from a turbomachine wheel slot include a body having at least two contacting portions for contacting the turbomachine wheel, a linear actuator coupled to the body, and an engagement arm for engaging the turbine bucket, the engagement arm coupled to the linear actuator and adapted to be actuated in a first axial direction by the linear actuator.
Abstract translation: 各种实施例包括适于从涡轮机内的位置置换涡轮机组件的装置。 在一些实施例中，用于将涡轮机叶轮从涡轮机轮槽移位的装置包括具有至少两个用于接触涡轮机轮的接触部分的主体，联接到主体的线性致动器和用于接合涡轮机叶片的接合臂，接合臂 耦合到线性致动器并且适于通过线性致动器在第一轴向方向上致动。
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公开(公告)号：US20140165359A1
公开(公告)日：2014-06-19
申请号：US13714873
申请日：2012-12-14
Applicant: GENERAL ELECTRIC COMPANY
Inventor： James Bradford Holmes , James Robert Hollis , Wayne David Sullivan
CPC classification number: B23P19/10 , B23P11/00 , F01D9/023 , F01D25/285 , F05D2230/64 , F23R3/60 , F23R2900/00017 , Y10T29/4978 , Y10T29/53913
Abstract: Various embodiments include alignment systems for turbines. In various particular embodiments, an apparatus for aligning an end of a transition piece (TP) with an outlet of a combustor component is disclosed. The apparatus can include: a mount configured to attach to the combustor component proximate the outlet; a hinge component pivotably connected to the mount, the hinge component having an axis of motion substantially perpendicular with a primary axis of the combustor component; a dummy transition piece (dummy TP) component fixedly attached to the hinge component for pivoting with the hinge component; and an adjustment apparatus having a first end fixedly attached to the dummy TP, and a second end with an actuatable adjustment member for modifying a position of the dummy TP.
Abstract translation: 各种实施例包括用于涡轮机的对准系统。 在各种具体实施例中，公开了一种用于将过渡件（TP）的端部与燃烧器部件的出口对准的装置。 该装置可以包括：安装件，其构造成在靠近出口处附接到燃烧器部件; 铰链部件，其可枢转地连接到所述安装件，所述铰链部件具有基本上垂直于所述燃烧器部件的主轴线的运动轴线; 固定地附接到所述铰链部件以与所述铰链部件枢转的虚拟过渡件（虚拟TP）部件; 以及调节装置，其具有固定地连接到所述虚拟TP的第一端，以及具有用于修改所述虚拟TP的位置的可启动调节构件的第二端。
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公开(公告)号：US09713862B2
公开(公告)日：2017-07-25
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.
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公开(公告)号：US20160271743A1
公开(公告)日：2016-09-22
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.
Abstract translation: 各种实施例包括适于从涡轮机内的位置置换涡轮机组件的方法。 在一些实施例中，使用位移设备从涡轮机轮槽移动涡轮机叶片的方法包括：将所述位移设备的接合臂可拆卸地接合到所述涡轮机叶片，所述接合臂附接到线性致动器，所述线性致动器联接到 所述位移装置和所述接合臂适于通过所述线性致动器在第一轴向方向上致动; 使所述涡轮机轮与所述位移设备的主体的至少两个接触部分接触; 并且通过用线性致动器线性地致动接合臂，使涡轮机叶轮在第一轴向方向上从位于涡轮机轮的槽内的位置移位。
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公开(公告)号：US08910374B2
公开(公告)日：2014-12-16
申请号：US13645068
申请日：2012-10-04
Applicant: General Electric Company
IPC: B66C17/06
CPC classification number: F01D25/285 , B66C17/06
Abstract: Various embodiments include a service apparatus for a turbomachine. The service apparatus can include: a frame for coupling to an opening in the turbomachine; a bridge member operably coupled to the frame and spanning a width of the frame, the bridge member being substantially movable along a length of the frame; and a crane member operably coupled to the bridge member, the crane member being substantially movable along the width of the frame, wherein the crane member includes at least one attachment device for attaching to an object within the turbomachine.
Abstract translation: 各种实施例包括用于涡轮机的服务装置。 服务设备可以包括：用于联接到涡轮机中的开口的框架; 桥接构件，其可操作地联接到所述框架并横跨所述框架的宽度，所述桥接构件基本上可沿所述框架的长度移动; 以及起重机构件，其可操作地联接到所述桥构件，所述起重机构件可沿着所述框架的宽度基本上移动，其中所述起重机构件包括用于附接到所述涡轮机内的物体的至少一个附接装置。
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