-
公开(公告)号：US10662793B2
公开(公告)日：2020-05-26
申请号：US14556305
申请日：2014-12-01
Applicant: General Electric Company
Abstract: A sealing system for a multi-stage turbine includes multiple first interstage seal subsystems disposed circumferentially about a rotor wheel shaft of the multi-stage turbine and extending axially between a first turbine stage and a second turbine stage of the multi-stage turbine. Each of the first interstage seal subsystems includes multiple near flow path seal segments. The first interstage seal subsystem also includes a forward coverplate disposed axially between a first turbine wheel of the first turbine stage and the near flow path seal segment and an aft coverplate disposed axially between the near flow path seal segment and a second turbine wheel of the second turbine stag. Further, each of the forward coverplate and the aft coverplate extends radially to a first stage bucket and a second stage bucket respectively.
-
公开(公告)号：US20140308088A1
公开(公告)日：2014-10-16
申请号：US13863441
申请日：2013-04-16
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Fernando Jorge Casanova , Rajesh Kumar , Madhumita Roy
IPC: F16B29/00
Abstract: A fastener is provided including a bolt having at least one threaded end, a first sleeve configured to fit over the bolt, and a second sleeve configured to fit over the first sleeve. At least one nut is configured to cooperate with threads in the threaded ends of the bolt. The first and second sleeves are configured to impart an outwardly radial load when the nuts are tightened on the bolt.
Abstract translation: 提供了紧固件，其包括具有至少一个螺纹端的螺栓，被配置成装配在螺栓上的第一套筒以及配置成装配在第一套筒上的第二套筒。 至少一个螺母构造成与螺栓的螺纹端部中的螺纹配合。 当螺母紧固在螺栓上时，第一和第二套筒构造成赋予向外的径向载荷。
-
公开(公告)号：US10337345B2
公开(公告)日：2019-07-02
申请号：US14627431
申请日：2015-02-20
Applicant: General Electric Company
Abstract: A sealing system for a multi-stage turbine includes multiple interstage seal segments disposed circumferentially about a turbine rotor wheel assembly and extending axially between a forward turbine stage and an aft turbine stage. Each of the interstage seal segments includes a forward end portion including an outer seal surface and an inner support face, an aft end portion, including an outer seal surface and an inner support face and a main body portion extending axially from the forward end portion to the aft end. The main body portion includes at least two support webs coupling the outer seal surfaces and the inner support faces. The outer seal surfaces are configured to be retained in a radial direction by a land support on each of a forward and aft stage turbine buckets, such that substantially all the centrifugal load from the multiple interstage seal segments is transferred to the forward and aft stage turbine buckets. A method of assembling the sealing system is disclosed.
-
4.发明申请TURBOMACHINE SEAL ASSEMBLY AND METHOD OF SEALING A ROTOR REGION OF A TURBOMACHINE 审中-公开涡轮密封组件和密封涡轮机转子区域的方法公开(公告)号：US20140154060A1
公开(公告)日：2014-06-05
申请号：US13705825
申请日：2012-12-05
Applicant: GENERAL ELECTRIC COMPANY
IPC: F01D11/00
CPC classification number: F01D11/003 , Y10T29/4932
Abstract: A turbomachine seal assembly includes a rotor disposed about an axial centerline, the rotor having an outer surface. Also included is a stationary component extending circumferentially about the rotor. Further included is at least one primary annular seal ring operably coupled to the stationary component and extending radially inwardly to close proximity with the outer surface of the rotor. Yet further included is a secondary annular seal ring operably coupled to the stationary component and integrally formed with the at least one primary annular seal ring, the secondary annular seal ring extending radially inwardly to close proximity with the outer surface of the rotor.
Abstract translation: 涡轮机械密封组件包括绕轴向中心线设置的转子，转子具有外表面。 还包括围绕转子周向延伸的固定部件。 还包括至少一个初级环形密封环，其可操作地联接到固定部件并且径向向内延伸以紧邻转子的外表面。 另外包括可操作地联接到静止部件并与至少一个主环形密封环一体形成的第二环形密封环，第二环形密封环径向向内延伸以紧邻转子的外表面。
-
公开(公告)号：US20210324507A1
公开(公告)日：2021-10-21
申请号：US16849418
申请日：2020-04-15
Applicant: General Electric Company
Inventor： David Allen Singletary , John Thomas Zanetti , Kassy Moy Hart , William Clifford Ross , Jose Troitino Lopez , Anderson Viaro Mattos , Fernando Jorge Casanova
Abstract: A coating method for a component with at least one aperture includes providing a component having at least one aperture formed in a surface thereof; additively manufacturing a hollow member on a portion of the surface to define a space above each aperture, the portion of the surface being adjacent to the aperture, the hollow member having an inner peripheral geometry complementary to a peripheral geometry at least one of aperture; applying at least one coating over the surface of the component and around hollow member to form an applied coating having an applied coating thickness; and removing at least a portion of the hollow member to make a top portion of the hollow member coplanar with the applied coating to expose the space through the applied coating; wherein a lower portion of the hollow member remains to define the space through the applied coating.
-
Patent Agency Ranking
公开(公告)号：US20160153302A1
公开(公告)日：2016-06-02
申请号：US14556305
申请日：2014-12-01
Applicant: General Electric Company
Abstract: A sealing system for a multi-stage turbine includes multiple first interstage seal subsystems disposed circumferentially about a rotor wheel shaft of the multi-stage turbine and extending axially between a first turbine stage and a second turbine stage of the multi-stage turbine. Each of the first interstage seal subsystems includes multiple near flow path seal segments. The first interstage seal subsystem also includes a forward coverplate disposed axially between a first turbine wheel of the first turbine stage and the near flow path seal segment and an aft coverplate disposed axially between the near flow path seal segment and a second turbine wheel of the second turbine stag. Further, each of the forward coverplate and the aft coverplate extends radially to a first stage bucket and a second stage bucket respectively.
Abstract translation: 用于多级涡轮机的密封系统包括多个第一级间密封子系统，其围绕多级涡轮机的转子轮轴周向设置，并且在多级涡轮机的第一涡轮级和第二涡轮级之间轴向延伸。 第一级间密封子系统中的每一个包括多个近流路密封段。 第一级间密封子系统还包括轴向设置在第一涡轮机台的第一涡轮机叶轮和近流动路径密封段之间的前盖板，以及轴向设置在近流路密封段和第二涡轮机叶轮的第二涡轮机叶轮之间的后盖板 涡轮机 此外，前盖板和后盖板中的每一个分别径向延伸到第一级铲斗和第二级铲斗。
-
公开(公告)号：US20220213583A1
公开(公告)日：2022-07-07
申请号：US17655892
申请日：2022-03-22
Applicant: General Electric Company
Inventor： David Allen Singletary , John Thomas Zanetti , Kassy Moy Hart , William Clifford Ross , Jose Troitino Lopez , Anderson Viaro Mattos , Fernando Jorge Casanova
Abstract: A coating method for a component with at least one aperture includes providing a component having at least one aperture formed in a surface thereof; additively manufacturing a hollow member on a portion of the surface to define a space above each aperture, the portion of the surface being adjacent to the aperture, the hollow member having an inner peripheral geometry complementary to a peripheral geometry at least one of aperture; applying at least one coating over the surface of the component and around hollow member to form an applied coating having an applied coating thickness; and removing at least a portion of the hollow member to make a top portion of the hollow member coplanar with the applied coating to expose the space through the applied coating; wherein a lower portion of the hollow member remains to define the space through the applied coating.
-
公开(公告)号：US09133868B2
公开(公告)日：2015-09-15
申请号：US13863441
申请日：2013-04-16
Applicant: General Electric Company
Inventor： Fernando Jorge Casanova , Rajesh Kumar , Madhumita Roy
Abstract: A fastener is provided including a bolt having at least one threaded end, a first sleeve configured to fit over the bolt, and a second sleeve configured to fit over the first sleeve. At least one nut is configured to cooperate with threads in the threaded ends of the bolt. The first and second sleeves are configured to impart an outwardly radial load when the nuts are tightened on the bolt.
Abstract translation: 提供了紧固件，其包括具有至少一个螺纹端的螺栓，被配置成装配在螺栓上的第一套筒以及配置成装配在第一套筒上的第二套筒。 至少一个螺母构造成与螺栓的螺纹端部中的螺纹配合。 当螺母紧固在螺栓上时，第一和第二套筒构造成赋予向外的径向载荷。
-
公开(公告)号：US11377722B2
公开(公告)日：2022-07-05
申请号：US16849418
申请日：2020-04-15
Applicant: General Electric Company
Inventor： David Allen Singletary , John Thomas Zanetti , Kassy Moy Hart , William Clifford Ross , Jose Troitino Lopez , Anderson Viaro Mattos , Fernando Jorge Casanova
IPC: B32B3/24 , C23C4/11 , B33Y80/00 , C23C4/134 , B33Y40/20 , B32B3/26 , C23C14/08 , C23C14/30 , B05D1/32 , C23C8/04
Abstract: A coating method for a component with at least one aperture includes providing a component having at least one aperture formed in a surface thereof; additively manufacturing a hollow member on a portion of the surface to define a space above each aperture, the portion of the surface being adjacent to the aperture, the hollow member having an inner peripheral geometry complementary to a peripheral geometry at least one of aperture; applying at least one coating over the surface of the component and around hollow member to form an applied coating having an applied coating thickness; and removing at least a portion of the hollow member to make a top portion of the hollow member coplanar with the applied coating to expose the space through the applied coating; wherein a lower portion of the hollow member remains to define the space through the applied coating.
-
10.发明申请公开(公告)号：US20160245106A1
公开(公告)日：2016-08-25
申请号：US14627431
申请日：2015-02-20
Applicant: General Electric Company
CPC classification number: F01D11/006 , F01D5/06 , F01D5/12 , F01D5/3007 , F01D11/001 , F01D11/005 , F01D11/02 , F05D2220/30 , F05D2230/60 , F05D2240/24 , F05D2240/55 , F05D2260/97
Abstract: A sealing system for a multi-stage turbine includes multiple interstage seal segments disposed circumferentially about a turbine rotor wheel assembly and extending axially between a forward turbine stage and an aft turbine stage. Each of the interstage seal segments includes a forward end portion including an outer seal surface and an inner support face, an aft end portion, including an outer seal surface and an inner support face and a main body portion extending axially from the forward end portion to the aft end. The main body portion includes at least two support webs coupling the outer seal surfaces and the inner support faces. The outer seal surfaces are configured to be retained in a radial direction by a land support on each of a forward and aft stage turbine buckets, such that substantially all the centrifugal load from the multiple interstage seal segments is transferred to the forward and aft stage turbine buckets. A method of assembling the sealing system is disclosed.
Abstract translation: 用于多级涡轮机的密封系统包括围绕涡轮机转子轮组件周向设置并且在正向涡轮机台架和后涡轮机台架之间轴向延伸的多个级间密封段。 每个级间密封段包括前端部分，其包括外密封表面和内支撑面，后端部分包括外密封表面和内支撑面以及主体部分，其从前端部轴向延伸到 后端 主体部分包括联接外密封表面和内支撑面的至少两个支撑腹板。 外密封表面被构造成通过在前级和后级涡轮机叶片中的每一个上的陆部支撑件沿径向保持，使得来自多个级间密封段的基本上所有的离心载荷被传递到前级和后级涡轮机 水桶 公开了一种组装密封系统的方法。
-
-
-
-
-
-
-
-
-
Search Results
10
records
(took 0.02 seconds)
