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公开(公告)号:US11873728B2
公开(公告)日:2024-01-16
申请号:US18101564
申请日:2023-01-25
Applicant: General Electric Company
Inventor: Jorge Mario Rochin Machado , Jordan Scott Warton , Ashish Agrawal , Michael Anthony Acosta , Gerardo Plata Contreras , Miroslaw Pawel Babiuch , Frank Ociel Meza Koslowski
CPC classification number: F01D25/30 , F01D9/02 , F05D2230/80 , F05D2240/12 , F05D2240/60 , F05D2250/292 , F05D2250/324 , F05D2250/90
Abstract: A system includes an exhaust collector tunnel (32) configured to mount inside an exhaust collector (30) of a gas turbine (12). The exhaust collector tunnel (32) has a tunnel wall (33) configured to extend around a turbine shaft (17, 19) of the gas turbine (12). The tunnel wall (33) has a variable diameter (98) along at least a portion of a length of the exhaust collector tunnel (32).
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公开(公告)号:US11598224B2
公开(公告)日:2023-03-07
申请号:US17329820
申请日:2021-05-25
Applicant: General Electric Company
Inventor: Jorge Mario Rochin Machado , Jordan Scott Warton , Ashish Agrawal , Michael Anthony Acosta , Gerardo Plata Contreras , Miroslaw Pawel Babiuch , Frank Ociel Meza Koslowski
Abstract: A system includes an exhaust collector tunnel (32) configured to mount inside an exhaust collector (30) of a gas turbine (12). The exhaust collector tunnel (32) has a tunnel wall (33) configured to extend around a turbine shaft (17, 19) of the gas turbine (12). The tunnel wall (33) has a variable diameter (98) along at least a portion of a length of the exhaust collector tunnel (32).
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公开(公告)号:US20210388740A1
公开(公告)日:2021-12-16
申请号:US17329820
申请日:2021-05-25
Applicant: General Electric Company
Inventor: Jorge Mario Rochin Machado , Jordan Scott Warton , Ashish Agrawal , Michael Anthony Acosta , Gerardo Plata Contreras , Miroslaw Pawel Babiuch , Frank Ociel Meza Koslowski
Abstract: A system includes an exhaust collector tunnel (32) configured to mount inside an exhaust collector (30) of a gas turbine (12). The exhaust collector tunnel (32) has a tunnel wall (33) configured to extend around a turbine shaft (17, 19) of the gas turbine (12). The tunnel wall (33) has a variable diameter (98) along at least a portion of a length of the exhaust collector tunnel (32).
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公开(公告)号:US20190116170A1
公开(公告)日:2019-04-18
申请号:US15787400
申请日:2017-10-18
Applicant: General Electric Company
Inventor: Veera Kishore Reddipalli , Diwakar Kasibhotla , Ashish Agrawal
Abstract: Tenant-specific data required for use by a software analytic at an edge node is obtained. The software analytic is associated with a single tenant. The tenant-specific data and the analytic are transmitted from the edge node to a cluster of one or more software containers. Each of the containers at the cluster enforces a set of access privileges for files being accessed. The user data and the analytic are routed to a selected container within the cluster and the selected container executes the analytic such that the data accessed by the analytic at the container is protected from access by other tenants utilizing the cluster.
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公开(公告)号:US20180238195A1
公开(公告)日:2018-08-23
申请号:US15435465
申请日:2017-02-17
Applicant: General Electric Company
Inventor: Quoc Hoai Nguyen , Ashish Agrawal , Horacio Solis , Yunyi Zou , Tho V. Nguyen
CPC classification number: F01D25/285 , B60P7/16 , F02C7/20 , F05D2260/02 , F16M7/00
Abstract: This application provides elastomeric shock absorbers for turbine transportation. Example engine mounts may include a first plate, a second plate, and an elastomeric bearing positioned between the first plate and the second plate. The engine mount may be configured to absorb or dampen vibration along an X-axis, a Y-axis, and a Z-axis of a turbine during transportation.
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公开(公告)号:US11473450B2
公开(公告)日:2022-10-18
申请号:US16727410
申请日:2019-12-26
Applicant: General Electric Company
Inventor: Jorge Mario Rochin Machado , Paul Roberts Scarboro , Jordan Scott Warton , Michael Anthony Acosta , Ashish Agrawal , Miroslaw Pawel Babiuch
IPC: F01D25/30
Abstract: A system (10) includes a modular exhaust collector (30) configured to be arranged in a first orientation (50) or a second orientation (114, 116). The modular exhaust collector (30) is configured to receive an exhaust flow along an inlet axis (54), to direct the exhaust flow along a first direction (36) through an outlet (58) when in the first orientation (50), and to direct the exhaust flow along a second direction (114, 116) through the outlet (58) when in the second orientation (114, 116). The modular exhaust collector (30) includes an exhaust passage (64) to receive the exhaust flow, a plurality of compressor discharge (CD) ports (72), a plurality of flow ports (76), a bottom face (84) opposite the outlet (58) with a first drain (88), and a first side wall (82) with a second drain (88) between the bottom face (84) and the outlet (58). Each CD port (72) is disposed a first radial distance (118) from the inlet axis (54), and each flow port (76) is disposed a second radial distance (130) from the inlet axis (54).
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公开(公告)号:US10436072B2
公开(公告)日:2019-10-08
申请号:US15435465
申请日:2017-02-17
Applicant: General Electric Company
Inventor: Quoc Hoai Nguyen , Ashish Agrawal , Horacio Solis , Yunyi Zou , Tho V. Nguyen
Abstract: This application provides elastomeric shock absorbers for turbine transportation. Example engine mounts may include a first plate, a second plate, and an elastomeric bearing positioned between the first plate and the second plate. The engine mount may be configured to absorb or dampen vibration along an X-axis, a Y-axis, and a Z-axis of a turbine during transportation.
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公开(公告)号:US20230184138A1
公开(公告)日:2023-06-15
申请号:US18101564
申请日:2023-01-25
Applicant: General Electric Company
Inventor: Jorge Mario Rochin Machado , Jordan Scott Warton , Ashish Agrawal , Michael Anthony Acosta , Gerardo Plata Contreras , Miroslaw Pawel Babiuch , Frank Ociel Meza Koslowski
CPC classification number: F01D25/30 , F01D9/02 , F05D2230/80 , F05D2240/12 , F05D2240/60 , F05D2250/90 , F05D2250/292 , F05D2250/324
Abstract: A system includes an exhaust collector tunnel (32) configured to mount inside an exhaust collector (30) of a gas turbine (12). The exhaust collector tunnel (32) has a tunnel wall (33) configured to extend around a turbine shaft (17, 19) of the gas turbine (12). The tunnel wall (33) has a variable diameter (98) along at least a portion of a length of the exhaust collector tunnel (32).
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公开(公告)号:US20230068693A1
公开(公告)日:2023-03-02
申请号:US18047136
申请日:2022-10-17
Applicant: General Electric Company
Inventor: Jorge Mario Rochin Machado , Paul Roberts Scarboro , Jordan Scott Warton , Michael Anthony Acosta , Ashish Agrawal , Miroslaw Pawel Babiuch
IPC: F01D25/30
Abstract: A system includes a modular exhaust collector configured to be arranged in a first orientation or a second orientation. The modular exhaust collector is configured to receive an exhaust flow along an inlet axis, to direct the exhaust flow along a first direction through an outlet when in the first orientation, and to direct the exhaust flow along a second direction through the outlet when in the second orientation. The modular exhaust collector includes an exhaust passage to receive the exhaust flow, a plurality of compressor discharge (CD) ports, a plurality of flow ports, a bottom face opposite the outlet with a first drain, and a first side wall with a second drain between the bottom face and the outlet. Each CD port is disposed a first radial distance from the inlet axis, and each flow port is disposed a second radial distance from the inlet axis.
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