FABRICATION OF GAS TURBINE ENGINE COMPONENTS USING MULTIPLE PROCESSING STEPS
Methods for fabricating a component of a gas turbine engine are provided. In one embodiment, the method includes molding a CMC material to form a first portion of the gas turbine engine component, processing the first portion to form a first assembly, preparing the first assembly and a second portio...
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| creator | Tyler Robert Marusko Mark Willard Hasse Christopher Verrilli Michael J Noe Mark Eugene Izon Paul |
| description | Methods for fabricating a component of a gas turbine engine are provided. In one embodiment, the method includes molding a CMC material to form a first portion of the gas turbine engine component, processing the first portion to form a first assembly, preparing the first assembly and a second portion of the gas turbine engine component for processing, and processing the first assembly and second portion to form a second assembly. In another embodiment, the method includes processing a first plurality of CMC plies to form a first assembly; positioning the first assembly and a second plurality of CMC plies on a tool for processing, the first assembly defining a first plane, the second plurality of plies defining a second plane, wherein the second plane is perpendicular to the first plane; and processing the first assembly and the second plurality of plies to form a second assembly. |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2017114649A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2017114649A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2017114649A13</originalsourceid><addsrcrecordid>eNrjZPBxc3QK8nR2DPH091Pwd1NwdwxWCAkNcvL0c1Vw9XMHUc7-vgH-fq5-IcEKocGefu4KvqE-IZ4BPq4KAUH-zq7BYLHgENeAYB4G1rTEnOJUXijNzaDs5hri7KGbWpAfn1pckJicmpdaEh8abGRgaG5oaGJmYuloaEycKgCMxi8y</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>FABRICATION OF GAS TURBINE ENGINE COMPONENTS USING MULTIPLE PROCESSING STEPS</title><source>esp@cenet</source><creator>Tyler Robert ; Marusko Mark Willard ; Hasse Christopher ; Verrilli Michael J ; Noe Mark Eugene ; Izon Paul</creator><creatorcontrib>Tyler Robert ; Marusko Mark Willard ; Hasse Christopher ; Verrilli Michael J ; Noe Mark Eugene ; Izon Paul</creatorcontrib><description>Methods for fabricating a component of a gas turbine engine are provided. In one embodiment, the method includes molding a CMC material to form a first portion of the gas turbine engine component, processing the first portion to form a first assembly, preparing the first assembly and a second portion of the gas turbine engine component for processing, and processing the first assembly and second portion to form a second assembly. In another embodiment, the method includes processing a first plurality of CMC plies to form a first assembly; positioning the first assembly and a second plurality of CMC plies on a tool for processing, the first assembly defining a first plane, the second plurality of plies defining a second plane, wherein the second plane is perpendicular to the first plane; and processing the first assembly and the second plurality of plies to form a second assembly.</description><language>eng</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2017</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=20170427&DB=EPODOC&CC=US&NR=2017114649A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170427&DB=EPODOC&CC=US&NR=2017114649A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Tyler Robert</creatorcontrib><creatorcontrib>Marusko Mark Willard</creatorcontrib><creatorcontrib>Hasse Christopher</creatorcontrib><creatorcontrib>Verrilli Michael J</creatorcontrib><creatorcontrib>Noe Mark Eugene</creatorcontrib><creatorcontrib>Izon Paul</creatorcontrib><title>FABRICATION OF GAS TURBINE ENGINE COMPONENTS USING MULTIPLE PROCESSING STEPS</title><description>Methods for fabricating a component of a gas turbine engine are provided. In one embodiment, the method includes molding a CMC material to form a first portion of the gas turbine engine component, processing the first portion to form a first assembly, preparing the first assembly and a second portion of the gas turbine engine component for processing, and processing the first assembly and second portion to form a second assembly. In another embodiment, the method includes processing a first plurality of CMC plies to form a first assembly; positioning the first assembly and a second plurality of CMC plies on a tool for processing, the first assembly defining a first plane, the second plurality of plies defining a second plane, wherein the second plane is perpendicular to the first plane; and processing the first assembly and the second plurality of plies to form a second assembly.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPBxc3QK8nR2DPH091Pwd1NwdwxWCAkNcvL0c1Vw9XMHUc7-vgH-fq5-IcEKocGefu4KvqE-IZ4BPq4KAUH-zq7BYLHgENeAYB4G1rTEnOJUXijNzaDs5hri7KGbWpAfn1pckJicmpdaEh8abGRgaG5oaGJmYuloaEycKgCMxi8y</recordid><startdate>20170427</startdate><enddate>20170427</enddate><creator>Tyler Robert</creator><creator>Marusko Mark Willard</creator><creator>Hasse Christopher</creator><creator>Verrilli Michael J</creator><creator>Noe Mark Eugene</creator><creator>Izon Paul</creator><scope>EVB</scope></search><sort><creationdate>20170427</creationdate><title>FABRICATION OF GAS TURBINE ENGINE COMPONENTS USING MULTIPLE PROCESSING STEPS</title><author>Tyler Robert ; Marusko Mark Willard ; Hasse Christopher ; Verrilli Michael J ; Noe Mark Eugene ; Izon Paul</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2017114649A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2017</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Tyler Robert</creatorcontrib><creatorcontrib>Marusko Mark Willard</creatorcontrib><creatorcontrib>Hasse Christopher</creatorcontrib><creatorcontrib>Verrilli Michael J</creatorcontrib><creatorcontrib>Noe Mark Eugene</creatorcontrib><creatorcontrib>Izon Paul</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Tyler Robert</au><au>Marusko Mark Willard</au><au>Hasse Christopher</au><au>Verrilli Michael J</au><au>Noe Mark Eugene</au><au>Izon Paul</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>FABRICATION OF GAS TURBINE ENGINE COMPONENTS USING MULTIPLE PROCESSING STEPS</title><date>2017-04-27</date><risdate>2017</risdate><abstract>Methods for fabricating a component of a gas turbine engine are provided. In one embodiment, the method includes molding a CMC material to form a first portion of the gas turbine engine component, processing the first portion to form a first assembly, preparing the first assembly and a second portion of the gas turbine engine component for processing, and processing the first assembly and second portion to form a second assembly. In another embodiment, the method includes processing a first plurality of CMC plies to form a first assembly; positioning the first assembly and a second plurality of CMC plies on a tool for processing, the first assembly defining a first plane, the second plurality of plies defining a second plane, wherein the second plane is perpendicular to the first plane; and processing the first assembly and the second plurality of plies to form a second assembly.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | FABRICATION OF GAS TURBINE ENGINE COMPONENTS USING MULTIPLE PROCESSING STEPS |
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