-
公开(公告)号：US20140062032A1
公开(公告)日：2014-03-06
申请号：US13690541
申请日：2012-11-30
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Christopher Edward Wolfe , Victor John Morgan , Neelesh Nandkumar Sarawate , David Wayne Weber
IPC: F01D11/00
CPC classification number: F01D11/005 , F05D2240/57 , F16J15/128
Abstract: A seal assembly is provided. The seal assembly includes a first outer shim and a second outer shim The second outer shim is operably coupled to the first outer shim and comprises at least one substantially impermeable portion that spans across a gap between at least two turbomachine components. The second outer shim further engages the at least two turbomachine components to substantially seal the gap. The substantially impermeable portion is substantially planar at least along a width of the seal assembly. The seal assembly further includes a resilient member that is either coupled to at least a portion of an outer surface of the first outer shim or comprises an integral portion of the first outer shim The resilient member engages the seal assembly to contact bottom surfaces of a cavity defined between the at least two turbomachine components.
Abstract translation: 提供密封组件。 密封组件包括第一外垫片和第二外垫片第二外垫片可操作地联接到第一外垫片，并且包括穿过至少两个涡轮机构件之间的间隙的至少一个基本不可渗透部分。 第二外垫片进一步接合至少两个涡轮机组件以基本上密封间隙。 至少沿着密封组件的宽度，基本上不可渗透部分基本上是平面的。 密封组件还包括弹性构件，其被联接到第一外垫片的外表面的至少一部分，或包括第一外垫片的整体部分。弹性构件接合密封组件以接触空腔的底表面 限定在所述至少两个涡轮机组件之间。
-
公开(公告)号：US11041389B2
公开(公告)日：2021-06-22
申请号：US15609576
申请日：2017-05-31
Applicant: General Electric Company
Inventor： Benjamin Paul Lacy , Victor John Morgan
Abstract: A hot gas path component of an industrial machine includes an adaptive cover for a cooling pathway. The component and adaptive cover are made by additive manufacturing. The component includes an outer surface exposed to a working fluid having a high temperature; an internal cooling circuit; and a cooling pathway in communication with the internal cooling circuit and extending towards the outer surface. The adaptive cover is positioned in the cooling pathway at the outer surface. The adaptive cover may include a heat transfer enhancing surface at the outer surface causing the adaptive cover to absorb heat faster than the outer surface.
-
公开(公告)号：US10927680B2
公开(公告)日：2021-02-23
申请号：US15609562
申请日：2017-05-31
Applicant: General Electric Company
Inventor： Benjamin Paul Lacy , Victor John Morgan
Abstract: A hot gas path component of an industrial machine includes an adaptive cover for a cooling pathway. The component and adaptive cover are made by additive manufacturing. The component includes an outer surface exposed to a working fluid having a high temperature; a thermal barrier coating over the outer surface; an internal cooling circuit; and a cooling pathway in communication with the internal cooling circuit and extending towards the outer surface. The adaptive cover is positioned in the cooling pathway at the outer surface. The adaptive cover includes a heat transfer enhancing surface at the outer surface causing the adaptive cover to absorb heat faster than the outer surface, e.g., when a spall in a thermal barrier coating thereover occurs.
-
公开(公告)号：US10704399B2
公开(公告)日：2020-07-07
申请号：US15609529
申请日：2017-05-31
Applicant: General Electric Company
Inventor： Benjamin Paul Lacy , Brian Peter Arness , Victor John Morgan , Stephen William Tesh
Abstract: A hot gas path component of an industrial machine includes a cooling pathway. The component includes a body including an outer surface; a thermal barrier coating (TBC) over the outer surface, the TBC exposed to a working fluid having a high temperature; and an internal cooling circuit in the body carrying a cooling medium. A cooling pathway is in the body and in fluid communication with the internal cooling circuit. The cooling pathway includes a terminating end in the body and a length extending along and spaced internally from the outer surface by a first spacing. In response to a spall in the TBC occurring at a location over the cooling pathway and the high temperature reaching or exceeding a predetermined temperature of the body, the cooling pathway opens at the location through the first spacing to allow a flow of the cooling medium therethrough.
-
公开(公告)号：US10583489B2
公开(公告)日：2020-03-10
申请号：US15497825
申请日：2017-04-26
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Victor John Morgan , George Andrew Gergely
IPC: B22F5/04 , B33Y10/00 , B33Y80/00 , B22F3/105 , B22F3/24 , B23K15/00 , B23K26/342 , B23K26/70 , B22F5/00 , C23C26/00 , C22C19/07 , C22C19/05 , C22C30/02 , B22D21/00 , B22D25/02 , F01D25/12 , B23P15/04 , F01D5/18 , F01D9/02 , B23K101/00
Abstract: A method of providing cooling structure for a component including forming a first cavity in the component and forming a first passageway in the first cavity in fluid communication with a second cavity positioned inside the component, the second cavity in fluid communication with a cooling air source. The method includes forming a unitary insert including a first surface, a second surface, the insert having an inlet formed in the first surface and an outlet formed in the second surface. A second passageway is in fluid communication with the inlet and the outlet. The method includes positioning the insert in the first cavity into fluid communication with the first passageway, the first surface facing the first cavity; and rigidly attaching the insert in the first cavity.
-
Patent Agency Ranking
公开(公告)号：US20190383488A1
公开(公告)日：2019-12-19
申请号：US16012412
申请日：2018-06-19
Applicant: General Electric Company
Inventor： Jonathan Dwight Berry , Michael John Hughes , Russell Pierson DeForest , Kevin Weston McMahan , Victor John Morgan , Ibrahim Sezer , Neelesh Nandkumar Sarawate , Deepak Trivedi
Abstract: An integrated combustor nozzle includes an inner liner segment; an outer liner segment; and a panel extending radially between the inner and outer liner segments. The panel includes a forward end, an aft end, and a side walls extending axially from the forward end to the aft end. The aft end defines a turbine nozzle having a trailing edge circumferentially offset from the forward end. The inner liner segment has a pair of sealing surfaces, each of which defines a first continuous curve in the circumferential direction. The outer liner segment has a pair of sealing surfaces, each of which defines a second continuous curve in the circumferential direction. In some instances, the curves are monotonic in the circumferential direction. A segmented annular combustor including an array of such integrated combustor nozzles is also provided.
-
公开(公告)号：US10280774B2
公开(公告)日：2019-05-07
申请号：US15585326
申请日：2017-05-03
Applicant: General Electric Company
Inventor： John Franklin Ryman , Victor John Morgan , Mary Virginia Holloway
IPC: F01D9/04
Abstract: The present application provides a turbine nozzle including an airfoil shape. The airfoil shape may have a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances in inches by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in inches. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The airfoil profile sections at Z distances may be joined smoothly with one another to form a complete airfoil shape.
-
公开(公告)号：US20180347370A1
公开(公告)日：2018-12-06
申请号：US15609562
申请日：2017-05-31
Applicant: General Electric Company
Inventor： Benjamin Paul Lacy , Victor John Morgan
CPC classification number: F01D5/288 , F01D5/186 , F01D5/187 , F05D2260/202 , F05D2260/22141 , F05D2270/46
Abstract: A hot gas path component of an industrial machine includes an adaptive cover for a cooling pathway. The component and adaptive cover are made by additive manufacturing. The component includes an outer surface exposed to a working fluid having a high temperature; a thermal barrier coating over the outer surface; an internal cooling circuit; and a cooling pathway in communication with the internal cooling circuit and extending towards the outer surface. The adaptive cover is positioned in the cooling pathway at the outer surface. The adaptive cover includes a heat transfer enhancing surface at the outer surface causing the adaptive cover to absorb heat faster than the outer surface, e.g., when a spall in a thermal barrier coating thereover occurs.
-
公开(公告)号：US20180045058A1
公开(公告)日：2018-02-15
申请号：US15236083
申请日：2016-08-12
Applicant: General Electric Company
Inventor： Brian Gene Brzek , Victor John Morgan , James Fredric Wiedenhoefer
CPC classification number: F01D9/065 , F05D2240/122 , F05D2250/231 , F05D2260/2212 , F05D2260/2214 , Y02T50/676
Abstract: An airfoil for turbomachines includes a first plurality of projections coupled to a suction sidewall adjacent a trailing edge and extending from the suction sidewall towards a pressure sidewall. A second plurality of projections is coupled to the pressure sidewall adjacent the trailing edge and extending from the pressure sidewall towards the suction sidewall. The airfoil includes a divider coupled to the first and second pluralities of projections and extending within a space between the first and second pluralities of projections. A first cooling channel is defined adjacent the suction sidewall and a second cooling channel is defined adjacent the pressure sidewall. The first and second cooling channels are configured to receive a coolant stream. The first plurality of projections is configured to meter the coolant stream through the first cooling channel and the second plurality of projections is configured to meter the coolant stream through the second cooling channel.
-
公开(公告)号：US20170167283A1
公开(公告)日：2017-06-15
申请号：US14963735
申请日：2015-12-09
Applicant: General Electric Company
CPC classification number: F01D11/005 , F01D25/005 , F01D25/24 , F05D2220/32 , F05D2240/11 , F05D2240/128 , F05D2240/14 , F05D2240/55 , F05D2240/57 , F05D2300/502 , F16J15/0825 , F16J15/0887
Abstract: Various embodiments include gas turbine seals and methods of forming such seals. In some cases, a turbine includes: a first arc segment adjacent to a second arc segment, each arc segment including an end surface and radially facing surfaces extending from opposite ends of the end surface; a slot located between the end surfaces of the first arc segment and the second arc segment; and a first seal disposed in the slot, the first seal contacting the first arc segment at the end surface and extending over the radially facing surfaces of the first arc segment, the first seal including: a shim contacting the first arc segment; a laminate material over the shim and covering the shim; and a conforming material coupling the laminate material to the shim.
-
-
-
-
-
-
-
-
-
Search Results
67
records
(took 0.025 seconds)
