-
公开(公告)号：US20190071977A1
公开(公告)日：2019-03-07
申请号：US15697916
申请日：2017-09-07
Applicant: General Electric Company
Abstract: An apparatus and method relating to a cooling hole of a component of a turbine engine. The cooling hole can extend from an inlet to an outlet to define a connecting passage. The cooling hole can contain a diffusing section. The diffusing section can be defined by an interior surface having variable geometries.
-
公开(公告)号：US20180355728A1
公开(公告)日：2018-12-13
申请号：US15615869
申请日：2017-06-07
Applicant: General Electric Company
Inventor： Matthew Thomas Beyer , Gregory Terrence Garay
CPC classification number: F01D5/18 , F01D9/065 , F05D2230/21 , F05D2260/20
Abstract: A method for making a cooled component for a turbine engine includes casting an airfoil assembly having an airfoil with an airfoil cooling passage and extending from a platform with at least one platform cooling passage, and forming a connecting passage between the airfoil cooling air passage and the platform cooling air passage.
-
公开(公告)号：US20180347374A1
公开(公告)日：2018-12-06
申请号：US15609430
申请日：2017-05-31
Applicant: General Electric Company
Inventor： Matthew Thomas Beyer , Gregory Terrence Garay , Aaron Ezekiel Smith
IPC: F01D5/18
Abstract: An apparatus and method for cooling an airfoil tip for a turbine engine can include an airfoil, such as a cooled turbine blade, having a tip rail extending beyond a tip wall enclosing an interior for the airfoil at the tip. A plurality of cooling holes can be provided in the tip rail. A flow of cooling fluid can be provided through the cooling holes from the interior of the airfoil to cool the tip of the airfoil.
-
公开(公告)号：US20180179899A1
公开(公告)日：2018-06-28
申请号：US15387808
申请日：2016-12-22
Applicant: General Electric Company
Inventor： Gregory Terrence Garay , Weston Nolan Dooley
IPC: F01D5/18
CPC classification number: F01D5/20 , F05D2230/10 , F05D2230/237 , F05D2240/307 , F05D2260/202 , Y02T50/676
Abstract: A method and apparatus for brazed engine components include machining an engine component, such as using a casting process, to form an aperture in the component. A brazing material is provided in the aperture to close the aperture and seal an interior of the engine component. A shaped cooling hole is machined in the brazing material to cool the brazing material during engine operation.
-
公开(公告)号：US12065946B2
公开(公告)日：2024-08-20
申请号：US18142577
申请日：2023-05-02
Applicant: General Electric Company
Inventor： Thomas Earl Dyson , Nicholas William Rathay , Brendon James Leary , Gregory Terrence Garay , Gustavo Adolfo Ledezma , David Wayne Weber , Aaron Ezekiel Smith
CPC classification number: F01D5/187 , F01D5/141 , F01D5/20 , F01D5/3007 , F05D2220/323 , F05D2240/307 , F05D2260/201 , F05D2260/202 , F05D2260/205
Abstract: An airfoil includes a body, a cooling passage, a first cooling cavity, a second cooling cavity, a cooling conduit, and a connecting conduit. The body defines an interior and includes a tip rail with an exterior surface extending between a first surface, a second surface, and a third surface. The cooling passage is formed within the interior. The first cooling cavity and the second cooling cavity are spaced from each other within the tip rail. The cooling conduit fluidly couples the cooling passage with the first cooling cavity. The connecting conduit fluidly couples the first cooling cavity to the second cooling cavity.
-
Patent Agency Ranking
公开(公告)号：US20240247590A1
公开(公告)日：2024-07-25
申请号：US18599486
申请日：2024-03-08
Applicant: General Electric Company
CPC classification number: F01D5/186 , F01D5/187 , F01D9/02 , F01D9/065 , F05D2230/10 , F05D2260/202
Abstract: A component for a turbine engine comprises a wall having a first wall surface and a second wall surface; and a cooling hole comprising a connecting passage extending between an inlet at the first wall surface and an outlet located at the second wall surface. The connecting passage includes: a metering section extending from the inlet toward the outlet and defining a centerline, and a diffusing section at the outlet defining first and second side walls, a first junction between the first side wall and the metering section and a second junction between the second side wall the metering section, the first side wall extending between the first junction and the outlet, and the second side wall extending between the second junction and the outlet. A metering section distance is measured between the centerline and a metering section wall of the metering section.
-
公开(公告)号：US20240209738A1
公开(公告)日：2024-06-27
申请号：US18418909
申请日：2024-01-22
Applicant: General Electric Company
Inventor： Daniel Endecott Osgood , Zachary Daniel Webster , Gregory Terrence Garay , Kevin Robert Feldmann
CPC classification number: F01D5/186 , F01D1/12 , F01D5/147 , F01D5/284 , F01D11/12 , F01D11/122 , F01D11/14 , F05D2220/32 , F05D2230/31 , F05D2230/311 , F05D2240/303 , F05D2240/304 , F05D2260/201 , F05D2260/202 , F05D2300/514
Abstract: A component for a turbine engine includes a body with an exterior surface abutting a combustion flowpath for a combustion gas flow through the turbine engine, a cooling passage defined within the body, and a trench on the exterior surface. The trench includes a plurality of outlets, and a plurality of cooling holes extending from the cooling passage to the corresponding plurality of outlets.
-
公开(公告)号：US11927110B2
公开(公告)日：2024-03-12
申请号：US17582305
申请日：2022-01-24
Applicant: General Electric Company
CPC classification number: F01D5/186 , F01D5/187 , F01D9/02 , F01D9/065 , F05D2230/10 , F05D2260/202
Abstract: An apparatus and method relating to a cooling hole of a component of a turbine engine. The cooling hole can extend from an inlet to an outlet to define a connecting passage. The cooling hole can contain a diffusing section. The diffusing section can be defined by an interior surface having variable geometries.
-
公开(公告)号：US20240011399A1
公开(公告)日：2024-01-11
申请号：US18142577
申请日：2023-05-02
Applicant: General Electric Company
Inventor： Thomas Earl Dyson , Nicholas William Rathay , Brendon James Leary , Gregory Terrence Garay , Gustavo Adolfo Ledezma , David Wayne Weber , Aaron Ezekiel Smith
CPC classification number: F01D5/187 , F01D5/20 , F01D5/141 , F05D2260/201 , F05D2260/205 , F01D5/3007
Abstract: An airfoil includes a body, a cooling passage, a first cooling cavity, a second cooling cavity, a cooling conduit, and a connecting conduit. The body defines an interior and includes a tip rail with an exterior surface extending between a first surface, a second surface, and a third surface. The cooling passage is formed within the interior. The first cooling cavity and the second cooling cavity are spaced from each other within the tip rail. The cooling conduit fluidly couples the cooling passage with the first cooling cavity. The connecting conduit fluidly couples the first cooling cavity to the second cooling cavity.
-
公开(公告)号：US11782416B2
公开(公告)日：2023-10-10
申请号：US16871186
申请日：2020-05-11
Applicant: General Electric Company
Inventor： Daniel Endecott Osgood , Tingfan Pang , Gregory Terrence Garay , Xi Yang , Daniel Lee Durstock , Steven Robert Brassfield , William Charles Herman
IPC: G05B19/4099 , B29C64/393 , G06F30/10
CPC classification number: G05B19/4099 , B29C64/393 , G06F30/10 , G05B2219/35036 , G05B2219/35134 , G05B2219/49007
Abstract: A method of using additive manufacturing to form or print a component based on an original model of a component, where the geometry of the original model is compensated to form a compensated model. The compensated model can be used to form or print the component. The printed component as a final model can then be compared to the original model.
-
-
-
-
-
-
-
-
-
Search Results
125
records
(took 0.024 seconds)
