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公开(公告)号：EP3179168A1
公开(公告)日：2017-06-14
申请号：EP16202218.0
申请日：2016-12-05
CPC分类号： F01D25/285 , B66F3/36 , B66F7/28 , F01D9/023 , F05D2230/68 , F05D2230/70 , F05D2230/72 , F05D2260/02 , F23R3/46 , F23R2900/00017 , F23R2900/00019
摘要： A combustor assembly lift system (200) comprises a track (210) that extends in at least a longitudinal direction, a lift arm (220) moveably engaged with the track (210) such that it can traverse along the track (210) in at least the longitudinal direction, and a combustor assembly engagement frame (240) connected to the lift arm (220), wherein the combustor assembly engagement frame (240) is configured to temporarily secure to at least a portion of a combustor assembly (20).
摘要翻译： 燃烧器组件升降系统（200）包括沿至少一个纵向方向延伸的轨道（210），与轨道（210）可移动地接合的升降臂（220），使得它可以沿着轨道（210）以 至少纵向方向，以及连接到提升臂（220）的燃烧器组件接合框架（240），其中燃烧器组件接合框架（240）构造成临时固定到燃烧器组件（20）的至少一部分。
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公开(公告)号：EP3312403B1
公开(公告)日：2019-06-12
申请号：EP17193833.5
申请日：2017-09-28
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公开(公告)号：EP3421408A1
公开(公告)日：2019-01-02
申请号：EP18178155.0
申请日：2018-06-18
摘要： The present disclosure is directed to a component handling assembly (100). The component handling assembly (100) includes a base member, an arm (106) pivotably coupled to the base member, and a beam (108) rotatably coupled to the base member. The component handling assembly (100) also includes a counterweight (150) rotatably coupled to a first end of the beam (108). The component handling assembly (100) further includes a coupling assembly (100) coupled to a second end of the beam (108). The coupling assembly (100) is configured for coupling to a component (34). Rotating the counterweight (150) in a first direction rotates the beam (108), the coupling assembly (100), and the component (34) in a second direction.
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公开(公告)号：EP3225779A1
公开(公告)日：2017-10-04
申请号：EP17162084.2
申请日：2017-03-21
CPC分类号： B25B27/0028 , B25B27/02 , F01D5/005 , F01D5/3007 , F01D5/3015 , F01D11/001 , F01D11/005 , F01D25/285 , F05D2230/70
摘要： A tool (100) for removing a component from a turbomachine is provided. The tool (100) includes a body (102) having a connection portion (104) for engaging the component. The tool (100) additionally includes a force section (132) connected to the body (102) and configured to transfer a force to the connection portion (104) in a direction at an acute angle relative to longitudinal axis of a dovetail slot (35) of a rotor wheel (34) adjacent to the component.
摘要翻译： 提供了一种用于从涡轮机中去除部件的工具（100）。 工具（100）包括具有用于接合部件的连接部分（104）的主体（102）。 所述工具（100）还包括力部分（132），所述力部分连接到所述主体（102）并且被配置为沿相对于燕尾槽（35）的纵向轴线成锐角的方向将力传递到所述连接部分（104） ）靠近所述部件的转子轮（34）。
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公开(公告)号：EP4013997A1
公开(公告)日：2022-06-22
申请号：EP20754099.8
申请日：2020-07-23
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公开(公告)号：EP3129712B1
公开(公告)日：2019-08-28
申请号：EP14721992.7
申请日：2014-04-09
发明人： KLEJC, Adrian Adam , HANSON, Stuart Craig , HERBOLD, John William , HOLMES, James Bradford , KOLVICK, Sandra Beverly , MOGLE, Thomas Alan, II , HUTH, Robert Edward , SAJDAK, Lukasz
IPC分类号： B23P6/00
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公开(公告)号：EP3391998A1
公开(公告)日：2018-10-24
申请号：EP18167687.5
申请日：2018-04-17
摘要： The present disclosure is directed to a coupling assembly (100) for a turbomachine (10). The coupling assembly (100) includes a liner (38) and a sleeve (52) at least partially positioned circumferentially around the liner (38). A frame (104) is positioned between the liner (38) and the sleeve (52). The frame (104) includes a first side wall (110), a second side wall (112), and a base wall (114) extending from the first side wall (110) to the second side wall (112). A block (106) is positioned between the liner (38) and the sleeve (52) and is movable relative to the frame (104) to permit the block (106) to move toward and away from the base wall (114). Moving the block (106) away from the base wall (114) causes the block (106) to exert an inward force on the liner (38) and the base wall (114) to exert an outward force on the sleeve (52).
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公开(公告)号：EP3351343A1
公开(公告)日：2018-07-25
申请号：EP18152111.3
申请日：2018-01-17
发明人： MERLAU, Thomas Michael , MEANS, Gregory Scott , LEINONEN, Brian Michael , HANSON, Stuart Craig , BECKER, Joseph Daniel
CPC分类号： F23R3/50 , B21D1/08 , B21D3/14 , B21D39/20 , B23P6/002 , B23P2700/13 , F01D25/285 , F05D2230/80 , F23R2900/00019 , Y02T50/671
摘要： A tool (130) for repairing an out-of-round component (116) such as a combustor body (116) is disclosed. The tool (130) includes a base (140) including a first arcuate member (142); a second arcuate member (144); and a linear actuator (146) coupling the second arcuate member (144) to the base (140). The linear actuator (146) moves the second arcuate member (144) between a retracted position out of engagement with the out-of-round component (116) and an extended position in which the first arcuate member (142) and the second arcuate member (144) engage an interior surface (154) of the out-of-round component (116) in an opposing relationship to force the out-of-round component (116) into a more round state compared to an initial state of the out-of-round component (116). A related method is also disclosed.
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公开(公告)号：EP3332097A1
公开(公告)日：2018-06-13
申请号：EP15759959.8
申请日：2015-08-06
发明人： KLEJC, Adrian Adam , MERLAU, Thomas Michael , BLACK, Kenneth Damon , HANSON, Stuart Craig , O'MEARA, Sean Cornelius
IPC分类号： F01D25/28
CPC分类号： F01D25/28 , F01D25/285 , F05D2230/68
摘要： An alignment assembly includes a base (14) and a support leg extending from the base, the leg configured to support a portion of a turbine system structure. Also included is a first support leg portion (20) disposed on a surface of the base (14) and coupleable thereto. Further included is a second support leg portion (22) angularly oriented relative to the first support leg portion (20) and coupleable to the turbine system structure (10). Yet further included is a jack assembly (24) moveable on the surface of the base (14) and configured to vertically and laterally adjust the turbine.
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公开(公告)号：EP3312403A3
公开(公告)日：2018-06-06
申请号：EP17193833.5
申请日：2017-09-28
CPC分类号： B23P19/042 , F01D9/023 , F01D25/285 , F05D2230/64 , F05D2230/70 , F05D2230/72 , F23R3/48 , F23R2900/00017 , F23R2900/00019
摘要： A tool kit (100) for decoupling a telescoping tube (60) from a liner (42) of a gas turbine engine (10) is disclosed. The tool kit (100) includes a base plate (108) coupled to a combustor casing (32). A post (134) extends outward from the base plate (108) into a combustion chamber (44) defined by the liner (42). A plunger (148) slidably mounts to the post (134) and is slidable between an extended position and a retracted position. A lever arm (160) pivotably couples to the post (134) and the plunger (148). Pivoting the lever arm (160) in a first direction slides the plunger (148) to the extended position to decouple the telescoping tube (60) from the liner (42). A retaining clip (104) couples to the combustor casing (32) and extends into an annular plenum (50) at least partially defined between the liner (42) and the combustor casing (32). The retaining clip (104) defines a notch (212) that receives the telescoping tube (60) after the plunger (148) decouples the telescoping tube (60) from the liner (42).
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