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公开(公告)号：US10094221B2
公开(公告)日：2018-10-09
申请号：US15014103
申请日：2016-02-03
Applicant: General Electric Company
Inventor： Herbert Chidsey Roberts , David Scott Diwinsky , Wayne R. Grady
Abstract: Methods for remotely joining material a surface area of a component of a gas turbine engine are provided. The method can include inserting an integrated repair interface attached to a cable delivery system within a gas turbine engine; positioning a tip of the integrated repair interface adjacent to a defect defined within a surface of the component; temporarily attaching the tip adjacent to the defect within the surface of the component; and supplying a new material to the area to fill the defect.
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公开(公告)号：US10247002B2
公开(公告)日：2019-04-02
申请号：US15014075
申请日：2016-02-03
Applicant: General Electric Company
Inventor： Herbert Chidsey Roberts , David Scott Diwinsky , Wayne R. Grady
IPC: B23P6/04 , B23K26/03 , B23K26/08 , F01D5/00 , B23K26/342 , B23K26/70 , B23K26/144 , B23K101/00 , B23K103/18
Abstract: A method for remotely stopping a crack in a component of a gas turbine engine is provided. The method can include inserting an integrated repair interface attached to a cable delivery system within a gas turbine engine; positioning the tip adjacent to a defect within a surface of the component; temporarily attaching the tip adjacent to the defect within the surface on the component; supplying a new material to the area to fill the defect; and heating the new material to fuse the new material to the component within the defect.
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公开(公告)号：US20170218761A1
公开(公告)日：2017-08-03
申请号：US15014075
申请日：2016-02-03
Applicant: General Electric Company
Inventor： Herbert Chidsey Roberts , David Scott Diwinsky , Wayne R. Grady
CPC classification number: F01D5/005 , B23P6/045 , F05D2230/80 , F05D2230/90 , F05D2260/83
Abstract: A method for remotely stopping a crack in a component of a gas turbine engine is provided. The method can include inserting an integrated repair interface attached to a cable delivery system within a gas turbine engine; positioning the tip adjacent to a defect within a surface of the component; temporarily attaching the tip adjacent to the defect within the surface on the component; supplying a new material to the area to fill the defect; and heating the new material to fuse the new material to the component within the defect.
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公开(公告)号：US20170218764A1
公开(公告)日：2017-08-03
申请号：US15014103
申请日：2016-02-03
Applicant: General Electric Company
Inventor： Herbert Chidsey Roberts , David Scott Diwinsky , Wayne R. Grady
CPC classification number: F01D5/005 , B23P6/045 , F01D5/12 , F05D2220/32 , F05D2230/30 , F05D2230/80
Abstract: Methods for remotely joining material a surface area of a component of a gas turbine engine are provided. The method can include inserting an integrated repair interface attached to a cable delivery system within a gas turbine engine; positioning a tip of the integrated repair interface adjacent to a defect defined within a surface of the component; temporarily attaching the tip adjacent to the defect within the surface of the component; and supplying a new material to the area to fill the defect.
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