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公开(公告)号：US11781437B2
公开(公告)日：2023-10-10
申请号：US17307394
申请日：2021-05-04
Applicant: General Electric Company
Inventor： Apostolos Pavlos Karafillis , Eric Dean Jorgensen , Craig Douglas Young , Jonathan Harry Kerner , Leonardo Ajdelsztajn
CPC classification number: F01D9/06 , B05D1/12 , F01D25/24 , F05D2230/31 , F05D2240/128 , F05D2260/606
Abstract: A component for a turbine engine may be formed by spraying particulate with a nozzle toward a substrate. The particulate may be deposited to form one or more annular layers and a reinforcing structure. The component may be a closed loop annular component having a reinforcing structure of specific dimensions enabled by the methods described.
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公开(公告)号：US20240301825A1
公开(公告)日：2024-09-12
申请号：US18666496
申请日：2024-05-16
Applicant: General Electric Company
CPC classification number: F02C7/00 , F01D25/24 , F01D25/26 , F05D2220/323
Abstract: Methods, apparatus, systems and articles of manufacture are disclosed for a structure of an engine component, including a first plurality of unit cells offset from a neutral plane in a first direction, a second plurality of unit cells offset from the neutral plane in a second direction, a plurality of nodes joining ones of the first plurality of unit cells and ones of the second plurality of unit cells, wherein the first plurality of unit cells and the second plurality of unit cells are arranged in pairs such that ones of the first plurality of unit cells are laterally adjacent to and interconnected with ones of the second plurality of unit cells, and wherein the structure is a stiffened structure.
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公开(公告)号：US20230250756A1
公开(公告)日：2023-08-10
申请号：US18186769
申请日：2023-03-20
Applicant: General Electric Company
CPC classification number: F02C7/00 , F01D25/24 , F01D25/26 , F05D2220/323
Abstract: Methods, apparatus, systems and articles of manufacture are disclosed for a structure of an engine component, including a first plurality of unit cells offset from a neutral plane in a first direction, a second plurality of unit cells offset from the neutral plane in a second direction, a plurality of nodes joining ones of the first plurality of unit cells and ones of the second plurality of unit cells, wherein the first plurality of unit cells and the second plurality of unit cells are arranged in pairs such that ones of the first plurality of unit cells are laterally adjacent to and interconnected with ones of the second plurality of unit cells, and wherein the structure is a stiffened structure.
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公开(公告)号：US20230417147A1
公开(公告)日：2023-12-28
申请号：US18465487
申请日：2023-09-12
Applicant: General Electric Company
Inventor： Apostolos Pavlos Karafillis , Eric Dean Jorgensen , Craig Douglas Young , Jonathan Harry Kerner , Leonardo Ajdelsztajn
CPC classification number: F01D9/06 , B05D1/12 , F01D25/24 , F05D2260/606 , F05D2230/31 , F05D2240/128
Abstract: A component for a turbine engine may be formed by spraying particulate with a nozzle toward a substrate. The particulate may be deposited to form one or more annular layers and a reinforcing structure. The component may be a closed loop annular component having a reinforcing structure of specific dimensions enabled by the methods described.
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Patent Agency Ranking
公开(公告)号：US11608780B2
公开(公告)日：2023-03-21
申请号：US17550885
申请日：2021-12-14
Applicant: General Electric Company
Abstract: Methods, apparatus, systems and articles of manufacture are disclosed for a structure of an engine component, including a first plurality of unit cells offset from a neutral plane in a first direction, a second plurality of unit cells offset from the neutral plane in a second direction, a plurality of nodes joining ones of the first plurality of unit cells and ones of the second plurality of unit cells, wherein the first plurality of unit cells and the second plurality of unit cells are arranged in pairs such that ones of the first plurality of unit cells are laterally adjacent to and interconnected with ones of the second plurality of unit cells, and wherein the structure is a stiffened structure.
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公开(公告)号：US20220356807A1
公开(公告)日：2022-11-10
申请号：US17307394
申请日：2021-05-04
Applicant: General Electric Company
Inventor： Apostolos Pavlos Karafillis , Eric Dean Jorgensen , Craig Douglas Young , Jonathan Harry Kerner , Leonardo Ajdelsztajn
Abstract: A component for a turbine engine may be formed by spraying particulate with a nozzle toward a substrate. The particulate may be deposited to form one or more annular layers and a reinforcing structure. The component may be a closed loop annular component having a reinforcing structure of specific dimensions enabled by the methods described.
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公开(公告)号：US11988139B2
公开(公告)日：2024-05-21
申请号：US18186769
申请日：2023-03-20
Applicant: General Electric Company
CPC classification number: F02C7/00 , F01D25/24 , F01D25/26 , F05D2220/323
Abstract: Methods, apparatus, systems and articles of manufacture are disclosed for a structure of an engine component, including a first plurality of unit cells offset from a neutral plane in a first direction, a second plurality of unit cells offset from the neutral plane in a second direction, a plurality of nodes joining ones of the first plurality of unit cells and ones of the second plurality of unit cells, wherein the first plurality of unit cells and the second plurality of unit cells are arranged in pairs such that ones of the first plurality of unit cells are laterally adjacent to and interconnected with ones of the second plurality of unit cells, and wherein the structure is a stiffened structure.
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公开(公告)号：US20220120219A1
公开(公告)日：2022-04-21
申请号：US17550885
申请日：2021-12-14
Applicant: General Electric Company
Abstract: Methods, apparatus, systems and articles of manufacture are disclosed for a structure of an engine component, including a first plurality of unit cells offset from a neutral plane in a first direction, a second plurality of unit cells offset from the neutral plane in a second direction, a plurality of nodes joining ones of the first plurality of unit cells and ones of the second plurality of unit cells, wherein the first plurality of unit cells and the second plurality of unit cells are arranged in pairs such that ones of the first plurality of unit cells are laterally adjacent to and interconnected with ones of the second plurality of unit cells, and wherein the structure is a stiffened structure.
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公开(公告)号：US11230971B1
公开(公告)日：2022-01-25
申请号：US17074209
申请日：2020-10-19
Applicant: General Electric Company
Abstract: Methods, apparatus, systems and articles of manufacture are disclosed for a structure of an engine component, including a first plurality of unit cells offset from a neutral plane in a first direction, a second plurality of unit cells offset from the neutral plane in a second direction, a plurality of nodes joining ones of the first plurality of unit cells and ones of the second plurality of unit cells, wherein the first plurality of unit cells and the second plurality of unit cells are arranged in pairs such that ones of the first plurality of unit cells are laterally adjacent to and interconnected with ones of the second plurality of unit cells, and wherein the structure is a stiffened structure.
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