-
公开(公告)号：US20230287836A1
公开(公告)日：2023-09-14
申请号：US17665800
申请日：2022-02-07
Applicant: General Electric Company
Inventor： Jessie Thorup , Christopher David King
Abstract: Control schemes for controlling a gas turbine engine in response to disturbances associated with a load mechanically coupled with the gas turbine engine are provided. In one aspect, a gas turbine engine mechanically coupled with a load has a controller that includes executable control logic. The control logic includes a feedforward module, an aggressive control module, and a power turbine governor module. By executing the modules, the controller seeks to maintain a constant power turbine speed stably and subtly in response to small disturbances associated with the load and aggressively in response to large disturbances associated with the load, as well as smooth transitions between the responses.
-
公开(公告)号：US11920521B2
公开(公告)日：2024-03-05
申请号：US17665800
申请日：2022-02-07
Applicant: General Electric Company
Inventor： Jessie Thorup , Christopher David King
Abstract: Control schemes for controlling a gas turbine engine in response to disturbances associated with a load mechanically coupled with the gas turbine engine are provided. In one aspect, a gas turbine engine mechanically coupled with a load has a controller that includes executable control logic. The control logic includes a feedforward module, an aggressive control module, and a power turbine governor module. By executing the modules, the controller seeks to maintain a constant power turbine speed stably and subtly in response to small disturbances associated with the load and aggressively in response to large disturbances associated with the load, as well as smooth transitions between the responses.
-
公开(公告)号：US20200248571A1
公开(公告)日：2020-08-06
申请号：US16804641
申请日：2020-02-28
Applicant: General Electric Company
Inventor： Christopher David King , David Vickery Parker , John Alan Manteiga , Matthew Brian Surprenant , Megan Lynn Williams , Awot Michael Berhe , Jesse Jacob Ollove
IPC: F01D9/02 , F01D9/04 , B22F3/105 , B22F5/00 , B33Y80/00 , B33Y10/00 , B22F5/10 , F04D29/02 , F04D29/44
Abstract: A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer shell to define a plurality of fluid passageways and a splitter extends along the circumferential direction between adjacent vanes to split the flow of compressed air passing through the each fluid passageway. All of these components are manufactured as a single monolithic piece and are configured for diffusing and deswirling compressor air before passing it to a combustor for an improved combustion process.
-
Patent Agency Ranking
4.发明申请公开(公告)号：US20200217253A1
公开(公告)日：2020-07-09
申请号：US16238777
申请日：2019-01-03
Applicant: General Electric Company
Inventor： Christopher David King
Abstract: Provided are systems and methods of controlling load share in a multi-engine propulsion system. A load share participation value indicative of a load share participation regime for a first engine may be received and a load sharing requirement control command for the first engine may be output. The load share participation value may depend or be based at least in part on one or more operating conditions of a second engine. The load sharing requirement control command for the first engine may depend on whether the load share participation value indicates a full-participation load share regime for the first engine, a partial-participation load share regime for the first engine, or a non-participation load share regime for the first engine.
-
公开(公告)号：US12241426B2
公开(公告)日：2025-03-04
申请号：US16238777
申请日：2019-01-03
Applicant: General Electric Company
Inventor： Christopher David King , Jessie Thorup
Abstract: Provided are systems and methods of controlling load share in a multi-engine propulsion system. A load share participation value indicative of a load share participation regime for a first engine may be received and a load sharing requirement control command for the first engine may be output. The load share participation value may depend or be based at least in part on one or more operating conditions of a second engine. The load sharing requirement control command for the first engine may depend on whether the load share participation value indicates a full-participation load share regime for the first engine, a partial-participation load share regime for the first engine, or a non-participation load share regime for the first engine.
-
公开(公告)号：US11098601B2
公开(公告)日：2021-08-24
申请号：US16804641
申请日：2020-02-28
Applicant: General Electric Company
Inventor： Christopher David King , David Vickery Parker , John Alan Manteiga , Matthew Brian Surprenant , Megan Lynn Williams , Awot Michael Berhe , Jesse Jacob Ollove
IPC: F01D9/02 , F01D9/04 , F04D29/44 , F04D29/02 , B22F5/10 , B33Y10/00 , B33Y80/00 , B22F5/00 , B22F10/20
Abstract: A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer shell to define a plurality of fluid passageways and a splitter extends along the circumferential direction between adjacent vanes to split the flow of compressed air passing through the each fluid passageway. All of these components are manufactured as a single monolithic piece and are configured for diffusing and deswirling compressor air before passing it to a combustor for an improved combustion process.
-
公开(公告)号：US10718222B2
公开(公告)日：2020-07-21
申请号：US15469708
申请日：2017-03-27
Applicant: General Electric Company
Inventor： Christopher David King , David Vickery Parker , John Alan Manteiga , Matthew Brian Surprenant , Megan Lynn Williams , Awot Michael Berhe , Jesse Jacob Ollove
IPC: F02D9/02 , F01D9/02 , B22F3/105 , F01D9/04 , F04D29/44 , F04D29/02 , B22F5/10 , B33Y10/00 , B33Y80/00 , B22F5/00
Abstract: A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer shell to define a plurality of fluid passageways and a splitter extends along the circumferential direction between adjacent vanes to split the flow of compressed air passing through the each fluid passageway. All of these components are manufactured as a single monolithic piece and are configured for diffusing and deswirling compressor air before passing it to a combustor for an improved combustion process.
-
公开(公告)号：US20180274376A1
公开(公告)日：2018-09-27
申请号：US15469708
申请日：2017-03-27
Applicant: General Electric Company
Inventor： Christopher David King , David Vickery Parker , John Alan Manteiga , Matthew Brian Surprenant , Megan Lynn Williams , Awot Michael Berhe , Jesse Jacob Ollove
Abstract: A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer shell to define a plurality of fluid passageways and a splitter extends along the circumferential direction between adjacent vanes to split the flow of compressed air passing through the each fluid passageway. All of these components are manufactured as a single monolithic piece and are configured for diffusing and deswirling compressor air before passing it to a combustor for an improved combustion process.
-
-
-
-
-
-
-
Search Results
8
records
(took 0.011 seconds)
