-
公开(公告)号：US10322575B2
公开(公告)日：2019-06-18
申请号：US15661126
申请日：2017-07-27
Applicant: General Electric Company
Inventor： Benjamin Paul Lacy , Srikanth Chandrudu Kottilingam , Christopher Donald Porter , David Edward Schick
Abstract: Various embodiments of the disclosure include a turbomachine component. and methods of forming such a component. Some embodiments include a turbomachine component including: a first portion including at least one of a stainless steel or an alloy steel; and a second portion joined with the first portion, the second portion including a nickel alloy including an arced cooling feature extending therethrough, the second portion having a thermal expansion coefficient substantially similar to a thermal expansion coefficient of the first portion, wherein the arced cooling feature is located within the second portion to direct a portion of a coolant to a leakage area of the turbomachine component.
-
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.
-
93.发明授权公开(公告)号：US10099290B2
公开(公告)日：2018-10-16
申请号：US14574557
申请日：2014-12-18
Applicant: General Electric Company
IPC: B22F5/00 , B23K26/34 , B33Y10/00 , C22C19/07 , B22F7/08 , B22F3/105 , B22F3/24 , B22F5/04 , B22F7/06 , B33Y80/00 , B23K26/342 , B23K26/00 , C22C19/05 , F01L9/02 , B23K10/02 , B23K103/18 , B23K103/08 , B23K103/10 , B23K103/14 , B23K103/04
Abstract: A hybrid additive manufacturing method comprises building an additive structure on a pre-sintered preform base, wherein building the additive structure comprises iteratively fusing together a plurality of layers of additive material with at least a first layer of additive material joined to the pre-sintered preform base, and wherein the pre-sintered preform base comprises an initial shape. The hybrid additive manufacturing method further comprises modifying the initial shape of the pre-sintered preform base comprising the additive structure into a modified shape comprising the additive structure, and, joining the pre-sintered preform base in its modified shape to a component.
-
公开(公告)号：US10053988B2
公开(公告)日：2018-08-21
申请号：US14965178
申请日：2015-12-10
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Gary Michael Itzel , Benjamin Paul Lacy
IPC: F01D5/18 , B22F3/105 , B22F5/04 , B23K15/00 , B23K26/342 , B33Y10/00 , B33Y80/00 , F01D25/12 , F01D9/04 , B22F7/06 , F01D9/06 , B23K101/00 , B22F5/00
CPC classification number: F01D5/187 , B22F3/1055 , B22F5/04 , B22F7/06 , B22F2005/005 , B23K15/0086 , B23K26/342 , B23K2101/001 , B33Y10/00 , B33Y80/00 , F01D9/041 , F01D9/065 , F01D25/12 , F05D2220/32 , F05D2230/31 , F05D2260/202 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141 , F05D2300/172 , F05D2300/5024 , Y02P10/295
Abstract: An article and method of forming an article are provided. The article includes a body portion having an inner surface and an outer surface, the inner surface defining an inner region, and at least one cooling feature positioned within the inner region. The body portion includes a first material and the at least one cooling feature includes a second material, the second material having a higher thermal conductivity than the first material. The method includes manufacturing a body portion by an additive manufacturing technique and manufacturing at least one cooling feature by the additive manufacturing technique. The body portion includes a first material and the at least one cooling feature includes a second material, the second material having a higher thermal conductivity than the first material.
-
95.发明申请公开(公告)号：US20180223673A1
公开(公告)日：2018-08-09
申请号：US15426484
申请日：2017-02-07
Applicant: General Electric Company
Inventor： Benjamin Paul Lacy , Christopher Donald Porter , Ibrahim Sezer , James William Vehr
CPC classification number: F01D5/186 , F02C7/18 , F05D2250/232 , F05D2250/323 , F05D2250/324 , F05D2260/202 , Y02T50/676 , Y02T50/6765
Abstract: A hot gas path component may include a body, and a passage for delivering a coolant extending through at least a part of the body to an exit area of the body. A metering structure may be in fluid communication with the passage and disposed upstream of the exit area. The metering structure may include a converging passage portion followed by a diverging passage portion.
-
Patent Agency Ranking
公开(公告)号：US20180171802A1
公开(公告)日：2018-06-21
申请号：US15383228
申请日：2016-12-19
Applicant: General Electric Company
Inventor： Benjamin Paul Lacy , Kassy Moy Hart , Xiuzhang James Zhang
CPC classification number: F01D5/005 , B22F3/105 , B22F5/04 , F01D5/025 , F01D5/147 , F01D5/18 , F01D5/30 , F05D2220/30 , F05D2230/30 , F05D2230/80 , F05D2240/301 , F05D2240/60 , F05D2240/80 , Y02T50/671 , Y02T50/676
Abstract: This disclosure provides components and methods for blade extensions with internal features. An airfoil extends from a root connector and includes an airfoil body defining at least one air channel enclosed within the airfoil body. The air channel extends to a build surface. An additive extension extends from the build surface of the airfoil body. The additive extension includes an additive structure extending the air channel from the build surface to an external surface of the additive extension.
-
公开(公告)号：US09995172B2
公开(公告)日：2018-06-12
申请号：US14880575
申请日：2015-10-12
Applicant: General Electric Company
Inventor： Sandip Dutta , Benjamin Paul Lacy , Gary Michael Itzel , Stephen Paul Wassynger
CPC classification number: F01D25/12 , F01D9/041 , F05D2220/32 , F05D2240/128 , F05D2240/81 , F05D2260/202 , F05D2260/204 , Y02T50/676
Abstract: A turbine nozzle includes an airfoil that extends in span from an inner band to an outer band where the inner band and the outer band define inner and outer flow boundaries of the turbine nozzle. At least one of the inner band and the outer band defines a plurality of cooling channels formed and a coolant discharge plenum beneath a gas side surface of the corresponding inner or outer band that is in fluid communication with the cooling channels. The coolant discharge plenum is formed within the inner band or the outer band downstream from the cooling channels and upstream from a plurality of coolant discharge ports.
-
公开(公告)号：US09938899B2
公开(公告)日：2018-04-10
申请号：US14739791
申请日：2015-06-15
Applicant: General Electric Company
CPC classification number: F02C7/18 , F01D5/186 , F01D5/187 , F05D2230/21 , F05D2260/202 , Y02T50/672 , Y02T50/676
Abstract: A hot gas path component includes a substrate having an outer surface and an inner surface. The inner surface of the substrate defines at least one interior space. At least a portion of the outer surface of the substrate includes a recess formed therein. The recess includes a bottom surface and a groove extending at least partially along the bottom surface of the recess. A cover is disposed within the recess and covers at least a portion of the groove. The groove is configured to channel a cooling fluid therethrough to cool the cover.
-
公开(公告)号：US09931814B2
公开(公告)日：2018-04-03
申请号：US14496828
申请日：2014-09-25
Applicant: GENERAL ELECTRIC COMPANY
IPC: B22F3/105 , B32B15/01 , B22F3/24 , B22F7/08 , B23K26/34 , B23K26/00 , B23K35/30 , B23K35/02 , B33Y10/00 , B33Y80/00
CPC classification number: B32B15/01 , B22F3/1055 , B22F3/24 , B22F5/009 , B22F7/08 , B22F2003/248 , B22F2998/10 , B23K26/02 , B23K26/144 , B23K26/342 , B23K26/354 , B23K35/0238 , B23K35/3046 , B23K35/3053 , B23K35/308 , B23K35/3086 , B23K2103/08 , B33Y10/00 , B33Y80/00 , Y02P10/295 , B22F3/15
Abstract: An article and a method for making shaped cooling holes in an article are provided. The method includes the steps of providing a metal alloy powder; forming an initial layer with the metal alloy powder, the initial layer having a preselected thickness and a preselected shape, the preselected shape including at least one aperture; sequentially forming an additional layer over the initial layer with the metal alloy powder, the additional layer having a second preselected thickness and a second preselected shape, the second preselected shape including at least one aperture corresponding to the at least one aperture in the initial layer; and joining the additional layer to the initial layer, forming a structure having a predetermined thickness, a predetermined shape, and at least one aperture having a predetermined profile. The structure is attached to a substrate to make the article.
-
公开(公告)号：US09757936B2
公开(公告)日：2017-09-12
申请号：US14584442
申请日：2014-12-29
Applicant: General Electric Company
Inventor： Benjamin Paul Lacy , Srikanth Chandrudu Kottilingam , Christopher Donald Porter , David Edward Schick
CPC classification number: B33Y80/00 , B22F3/1055 , B22F5/009 , B22F7/062 , B22F2999/00 , B33Y10/00 , F01D5/225 , F01D11/24 , F01D25/12 , F05D2230/31 , F05D2230/51 , F05D2240/11 , F05D2240/81 , F05D2260/202 , Y02P10/295 , B22F2203/05
Abstract: Various embodiments of the disclosure include a turbomachine component. and methods of forming such a component. Some embodiments include a turbomachine component including: a first portion including at least one of a stainless steel or an alloy steel; and a second portion joined with the first portion, the second portion including a nickel alloy including an arced cooling feature extending therethrough, the second portion having a thermal expansion coefficient substantially similar to a thermal expansion coefficient of the first portion, wherein the arced cooling feature is located within the second portion to direct a portion of a coolant to a leakage area of the turbomachine component.
-
-
-
-
-
-
-
-
-
Search Results
112
records
(took 0.039 seconds)
