-
公开(公告)号：US11033845B2
公开(公告)日：2021-06-15
申请号：US15314536
申请日：2015-05-29
Applicant: General Electric Company
Inventor： Timothy Deryck Stone , Gregory Michael Laskowski , Robert Proctor , Curtis Stover , Robert Francis Manning , Victor Hugo Silva Correia , Jared Peter Buhler , Robert Carl Murray , Corey Bourassa, Jr. , Byron Andrew Pritchard , Jonathan Russell Ratzlaff
IPC: B01D45/16 , F02C7/18 , B04C3/06 , F02C6/08 , F01D5/18 , F01D9/06 , F02C7/052 , B04C3/00 , F02K3/04
Abstract: A turbine engine having a bypass fluid conduit coupled to the turbine section includes at least one particle separator located within the bypass fluid conduit to separate particles from a bypass fluid stream prior to the bypass stream reaching the turbine section for cooling. A centrifugal separator for removing particles from a fluid stream includes an angular velocity increaser, a particle outlet, an angular velocity decreaser downstream of the angular velocity increaser, and a bend provided between the angular velocity increaser and the angular velocity decreaser.
-
公开(公告)号：US10975731B2
公开(公告)日：2021-04-13
申请号：US15314341
申请日：2015-05-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Robert Francis Manning , Timothy Deryck Stone , Jared Peter Buhler , Victor Hugo Silva Correia , Gregory Michael Laskowski , Robert Carl Murray , Jonathan Russell Ratzlaff , Robert Proctor , John Howard Starkweather , Curtis Walton Stover
IPC: B01D45/16 , F02C7/05 , F02C7/052 , F01D25/32 , B04C3/06 , B04C3/00 , B64D33/08 , F01D5/08 , F01D25/12 , F02C3/04 , F02C7/18 , F02C9/18 , B64D33/02
Abstract: A centrifugal separator for removing particles from a fluid stream includes an angular velocity increaser configured to increase the angular velocity of a fluid stream, a flow splitter configured to split the fluid stream to form a concentrated-particle stream and a reduced-particle stream, and an exit conduit configured to receive the reduced-particle stream. An inducer assembly for a turbine engine includes an inducer with a flow passage having an inducer inlet and an inducer outlet in fluid communication with a turbine section of the engine, and a particle separator, which includes a particle concentrator that receives a compressed stream from a compressor section of the engine and a flow splitter. A turbine engine includes a cooling air flow circuit which supplies a fluid stream to a turbine section of the engine for cooling, a particle separator located within the cooling air flow circuit, and an inducer forming a portion of the cooling air flow circuit in fluid communication with the particle separator. A method of cooling a rotating blade of a turbine engine having an inducer includes directing a cooling fluid stream from a portion of turbine engine toward the rotating blade, separating particles from the cooling fluid stream by passing the cooling fluid stream through a inertial separator, accelerating a reduced-particle stream emitted from the inertial separator to the speed of the rotating blade, and orienting the reduced-particle stream by emitting the reduced-particle stream from the inertial separator into a cooling passage in the inducer.
-
公开(公告)号：US09915176B2
公开(公告)日：2018-03-13
申请号：US14715700
申请日：2015-05-19
Applicant: General Electric Company
Inventor： Robert Carl Murray , Gregory Michael Laskowski , Corey Bourassa , Byron Andrew Pritchard, Jr. , Curtis Walton Stover
CPC classification number: F01D25/24 , F01D25/14 , F02C7/18 , F05D2240/11 , F05D2260/607 , Y02T50/675
Abstract: A shroud assembly for a turbine engine includes a shroud having a front side confronting the blades of a turbine and a back side opposite the front side, a hanger configured to couple the shroud to with casing of the turbine, a cooling conduit extending through the hanger to supply a cooling fluid stream to the back side of the shroud, and a particle separator having a through passage forming part of the cooling conduit and a scavenge conduit branching from the through passage.
-
公开(公告)号：US10167725B2
公开(公告)日：2019-01-01
申请号：US14861522
申请日：2015-09-22
Applicant: General Electric Company
Inventor： Robert Francis Manning , Victor Hugo Silva Correia , Jared Peter Buhler , Byron Andrew Pritchard, Jr. , William Collins Vining , Corey Bourassa , Gregory Michael Laskowski , David Vickery Parker
Abstract: An engine component for a turbine engine includes a particle collector having a substrate configured to retain at least some particles from a particle-laden stream passing through a portion of the engine. A fluid bypass around the substrate of the collector enables the particle-laden stream to bypass the substrate if the substrate is filled with particles.
-
公开(公告)号：US11918943B2
公开(公告)日：2024-03-05
申请号：US17993082
申请日：2022-11-23
Applicant: General Electric Company
Inventor： Timothy Deryck Stone , Gregory Michael Laskowski , Robert Proctor , Curtis Stover , Robert Francis Manning , Victor Hugo Silva Correia , Jared Peter Buhler , Robert Carl Murray , Corey Bourassa , Byron Andrew Pritchard, Jr. , Jonathan Russell Ratzlaff
IPC: B01D45/16 , B04C3/00 , B04C3/06 , F01D5/18 , F01D9/06 , F02C6/08 , F02C7/052 , F02C7/18 , F02K3/04
CPC classification number: B01D45/16 , B04C3/06 , F01D5/189 , F01D9/065 , F02C6/08 , F02C7/052 , F02C7/18 , B04C2003/003 , B04C2003/006 , F02K3/04 , F05D2260/607 , Y02T50/60
Abstract: A turbine engine having a compressor section, a combustor section, a turbine section, and a rotatable drive shaft that couples a portion of the turbine section and a portion of the compressor section. A bypass conduit couples the compressor section to the turbine section while bypassing at least the combustion section. At least one particle separator is located in the turbine engine having a separator inlet that receives a bypass stream, a separator outlet that receives a reduced-particle stream flows, and a particle outlet that receives a concentrated-particle stream comprising separated particles. A conduit, fluidly coupled to the particle outlet, extends through an interior of at least one stationary vane.
-
Patent Agency Ranking
公开(公告)号：US11541340B2
公开(公告)日：2023-01-03
申请号：US17325650
申请日：2021-05-20
Applicant: General Electric Company
Inventor： Timothy Deryck Stone , Gregory Michael Laskowski , Robert Proctor , Curtis Stover , Robert Francis Manning , Victor Hugo Silva Correia , Jared Peter Buhler , Robert Carl Murray , Corey Bourassa , Byron Andrew Pritchard, Jr. , Jonathan Russell Ratzlaff
IPC: B01D45/16 , F02C7/18 , B04C3/06 , B04C3/00 , F02C6/08 , F01D5/18 , F01D9/06 , F02C7/052 , F02K3/04
Abstract: A turbine engine having an inducer assembly. The inducer assembly includes a centrifugal separator fluidly coupled to an inducer with an inducer inlet and an inducer outlet. The centrifugal separator includes a body, an angular velocity increaser to form a concentrated-particle stream and a reduced-particle stream, a flow splitter, and an exit conduit fluidly coupled to the body to receive the reduced-particle stream and define a separator outlet.
-
公开(公告)号：US10428664B2
公开(公告)日：2019-10-01
申请号：US14884134
申请日：2015-10-15
Applicant: General Electric Company
Inventor： Hojjat Nasr , Ronald Scott Bunker , Gregory Michael Laskowski , Erich Alois Krammer
Abstract: A nozzle assembly for a gas turbine engine includes at least one pair of fixed vanes to define a nozzle between the pair of fixed vanes. The vanes can have an interior chamber defining a cooling circuit with a particle separator located within the interior chamber. The particle separator, which can comprise a virtual impactor, can have an accelerator for accelerating fluid moving through the virtual impactor such that the flow path is divided into a major flow moving into the interior chamber and a minor flow moving into a particle collector defined within the virtual impactor. The accelerator accelerates the fluid such that particles within the fluid are carried by their momentum into the particle collector with the minor flow, removing the particles from the major flow of fluid moving into the interior chamber.
-
公开(公告)号：US20170107852A1
公开(公告)日：2017-04-20
申请号：US14884152
申请日：2015-10-15
Applicant: General Electric Company
CPC classification number: F01D25/14 , F01D9/04 , F01D11/24 , F01D25/12 , F01D25/28 , F01D25/32 , F02C7/12 , F05D2240/11 , F05D2260/607 , Y02T50/675
Abstract: A shroud assembly for a gas turbine engine includes a shroud, hanger, and a hanger support mounted adjacent to a plurality of blades. The hanger can have an interior chamber defining a cooling circuit with a particle separator located within the interior chamber. The particle separator can have an inlet for accepting a flow of cooling fluid, such that a the flow of cooling fluid separates into a major flow and a minor flow carrying particles or particulate matter along the minor flow into a particle collector comprising at least a portion of the particle separator. Particles become constrained to the minor flow and pass into the particle collector, while the major flow is separated into the remaining area of the interior chamber to remove the particles from the flow of cooling fluid passing into the interior chamber.
-
公开(公告)号：US09988936B2
公开(公告)日：2018-06-05
申请号：US14884152
申请日：2015-10-15
Applicant: General Electric Company
CPC classification number: F01D25/14 , F01D9/04 , F01D11/24 , F01D25/12 , F01D25/28 , F01D25/32 , F02C7/12 , F05D2240/11 , F05D2260/607 , Y02T50/675
Abstract: A shroud assembly for a gas turbine engine includes a shroud, hanger, and a hanger support mounted adjacent to a plurality of blades. The hanger can have an interior chamber defining a cooling circuit with a particle separator located within the interior chamber. The particle separator can have an inlet for accepting a flow of cooling fluid, such that a the flow of cooling fluid separates into a major flow and a minor flow carrying particles or particulate matter along the minor flow into a particle collector comprising at least a portion of the particle separator. Particles become constrained to the minor flow and pass into the particle collector, while the major flow is separated into the remaining area of the interior chamber to remove the particles from the flow of cooling fluid passing into the interior chamber.
-
公开(公告)号：US20170107834A1
公开(公告)日：2017-04-20
申请号：US14884134
申请日：2015-10-15
Applicant: General Electric Company
Inventor： Hojjat Nasr , Ronald Scott Bunker , Gregory Michael Laskowski , Erich Alois Krammer
Abstract: A nozzle assembly for a gas turbine engine includes at least one pair of fixed vanes to define a nozzle between the pair of fixed vanes. The vanes can have an interior chamber defining a cooling circuit with a particle separator located within the interior chamber. The particle separator, which can comprise a virtual impactor, can have an accelerator for accelerating fluid moving through the virtual impactor such that the flow path is divided into a major flow moving into the interior chamber and a minor flow moving into a particle collector defined within the virtual impactor. The accelerator accelerates the fluid such that particles within the fluid are carried by their momentum into the particle collector with the minor flow, removing the particles from the major flow of fluid moving into the interior chamber.
-
-
-
-
-
-
-
-
-
Search Results
10
records
(took 0.027 seconds)
