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公开(公告)号：US20170260877A1
公开(公告)日：2017-09-14
申请号：US15068682
申请日：2016-03-14
Applicant: General Electric Company
Inventor： Daniel Elmer King , Jonathan Harry Kerner
CPC classification number: F01D25/243 , F01D9/042 , F01D25/162 , F01D25/246 , F02C7/20 , F05D2220/32 , Y02T50/672
Abstract: A doubler attachment system is provided for fixedly coupling a strut to an engine casing. The strut includes at least one flanged end configured to mate with the engine casing. The doubler attachment system includes a doubler plate having a first radial surface and a second opposing radial surface. The first radial surface is configured to mate with and conform to a contour of the at least one flanged end of the strut. The doubler attachment system further includes at least two bolts fixedly attached to the doubler plate at the first radial surface. The at least two bolts extend radially away from the first radial surface and toward the engine casing.
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公开(公告)号：US10443447B2
公开(公告)日：2019-10-15
申请号：US15068682
申请日：2016-03-14
Applicant: General Electric Company
Inventor： Daniel Elmer King , Jonathan Harry Kerner
Abstract: A doubler attachment system is provided for fixedly coupling a strut to an engine casing. The strut includes at least one flanged end configured to mate with the engine casing. The doubler attachment system includes a doubler plate having a first radial surface and a second opposing radial surface. The first radial surface is configured to mate with and conform to a contour of the at least one flanged end of the strut. The doubler attachment system further includes at least two bolts fixedly attached to the doubler plate at the first radial surface. The at least two bolts extend radially away from the first radial surface and toward the engine casing.
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Patent Agency Ranking
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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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：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：US10450954B2
公开(公告)日：2019-10-22
申请号：US15072662
申请日：2016-03-17
Applicant: General Electric Company
Inventor： Alan Scott Grissino , John Alan Manteiga , Jonathan Harry Kerner
Abstract: An apparatus for providing foreign object debris protection and anti-icing capabilities to an air intake of an aircraft engine. The apparatus includes a frame having at least a portion configured to conduct fluids. A tube is positioned such that different portions of the frame are fluidly connected. There is a discharge outlet defined within the frame that is configured to discharge fluids from the frame into the air intake. An inlet is defined within the frame and is fluidly connected to a compressor section of the aircraft engine. In this manner, air from the compressor section of the aircraft engine can flow through the inlet, through the tube, and through the discharge outlet, to return to the compressor section of the aircraft engine.
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公开(公告)号：US20170268424A1
公开(公告)日：2017-09-21
申请号：US15072662
申请日：2016-03-17
Applicant: General Electric Company
Inventor： Alan Scott Grissino , John Alan Manteiga , Jonathan Harry Kerner
CPC classification number: F02C7/047 , B64D15/04 , B64D33/02 , B64D2033/022 , B64D2033/0233 , B64D2033/0246 , B64D2033/0293 , F02C6/08 , F02C7/05 , F02C7/055 , F04D29/522 , F05D2220/32 , F05D2240/129 , F05D2270/11 , Y02T50/671
Abstract: An apparatus for providing foreign object debris protection and anti-icing capabilities to an air intake of an aircraft engine. The apparatus includes a frame having at least a portion configured to conduct fluids. A tube is positioned such that different portions of the frame are fluidly connected. There is a discharge outlet defined within the frame that is configured to discharge fluids from the frame into the air intake. An inlet is defined within the frame and is fluidly connected to a compressor section of the aircraft engine. In this manner, air from the compressor section of the aircraft engine can flow through the inlet, through the tube, and through the discharge outlet, to return to the compressor section of the aircraft engine.
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