SYSTEMS AND METHODS OF BLADE LEADING EDGE REPAIR USING FIELD ASSISTED SINTERING TECHNOLOGY
A method can comprise forming a component (610) comprising a first mating surface (602); coupling the component (610) to an airfoil (202) having a second mating surface (612) and a Field Assisted Sintering Technology ("FAST") system; heating, via the FAST system, the airfoil (202) and the...
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creator | MINOR, Michael J IVORY, Steven LORICCO, Nicholas M RETTBERG, Luke Henry CRAIG, Brian Richard HAZEL, Brian T BISCHOF, Christopher J FOWLER, Stewart S LIU, Xuan |
description | A method can comprise forming a component (610) comprising a first mating surface (602); coupling the component (610) to an airfoil (202) having a second mating surface (612) and a Field Assisted Sintering Technology ("FAST") system; heating, via the FAST system, the airfoil (202) and the component (610) ; and applying, via the FAST system, a mechanical pressure between the first mating surface (602) and the second mating surface (612) to join the airfoil (202) to the component (610) and form a blade (650), the component (610) at least partially defining a leading edge (204) of the blade (650) in response to joining the airfoil (202) to the component (610). |
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IVORY, Steven ; LORICCO, Nicholas M ; RETTBERG, Luke Henry ; CRAIG, Brian Richard ; HAZEL, Brian T ; BISCHOF, Christopher J ; FOWLER, Stewart S ; LIU, Xuan</creatorcontrib><description>A method can comprise forming a component (610) comprising a first mating surface (602); coupling the component (610) to an airfoil (202) having a second mating surface (612) and a Field Assisted Sintering Technology ("FAST") system; heating, via the FAST system, the airfoil (202) and the component (610) ; and applying, via the FAST system, a mechanical pressure between the first mating surface (602) and the second mating surface (612) to join the airfoil (202) to the component (610) and form a blade (650), the component (610) at least partially defining a leading edge (204) of the blade (650) in response to joining the airfoil (202) to the component (610).</description><language>eng ; fre ; ger</language><subject>BLASTING ; COMBINED OPERATIONS ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINE TOOLS ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; OTHER WORKING OF METAL ; PERFORMING OPERATIONS ; STEAM ENGINES ; TRANSPORTING ; UNIVERSAL MACHINE TOOLS ; WEAPONS</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240529&DB=EPODOC&CC=EP&NR=4375482A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240529&DB=EPODOC&CC=EP&NR=4375482A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MINOR, Michael J</creatorcontrib><creatorcontrib>IVORY, Steven</creatorcontrib><creatorcontrib>LORICCO, Nicholas M</creatorcontrib><creatorcontrib>RETTBERG, Luke Henry</creatorcontrib><creatorcontrib>CRAIG, Brian Richard</creatorcontrib><creatorcontrib>HAZEL, Brian T</creatorcontrib><creatorcontrib>BISCHOF, Christopher J</creatorcontrib><creatorcontrib>FOWLER, Stewart S</creatorcontrib><creatorcontrib>LIU, Xuan</creatorcontrib><title>SYSTEMS AND METHODS OF BLADE LEADING EDGE REPAIR USING FIELD ASSISTED SINTERING TECHNOLOGY</title><description>A method can comprise forming a component (610) comprising a first mating surface (602); 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coupling the component (610) to an airfoil (202) having a second mating surface (612) and a Field Assisted Sintering Technology ("FAST") system; heating, via the FAST system, the airfoil (202) and the component (610) ; and applying, via the FAST system, a mechanical pressure between the first mating surface (602) and the second mating surface (612) to join the airfoil (202) to the component (610) and form a blade (650), the component (610) at least partially defining a leading edge (204) of the blade (650) in response to joining the airfoil (202) to the component (610).</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | BLASTING COMBINED OPERATIONS ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OTHER WORKING OF METAL PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS |
title | SYSTEMS AND METHODS OF BLADE LEADING EDGE REPAIR USING FIELD ASSISTED SINTERING TECHNOLOGY |
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