METHOD FOR THE FABRICATION OF NEEDLE-PUNCHED CARBON COMPOSITE
PURPOSE: A method for fabricating a needle-punched carbon composite is provided to prevent delamination or crack of layers and to save production cost. CONSTITUTION: A method for fabricating a needle-punched carbon composite comprises: a step of preparing a fiber layer of a predetermined thickness u...
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| creator | LEE, JAE YEOL PARK, JONG KYOO YUN, NAM GYUN |
| description | PURPOSE: A method for fabricating a needle-punched carbon composite is provided to prevent delamination or crack of layers and to save production cost. CONSTITUTION: A method for fabricating a needle-punched carbon composite comprises: a step of preparing a fiber layer of a predetermined thickness using a heat resistant fiber(S101); a step of laminating the prepared fiber layers and needle-punching while compressing the fiber layers to tight the fiber layers(S102); a step of performing thermal treatment of the fiber reinforcing material(S103); and a step of filling the fiber reinforcing material with a carbon ingredient(S104). The heat resistant fiber is an oxidized-polyacrylonitrile fiber. The fiber layer has a form of a woven fabric, a non-woven fabric, a knitted fabric, a multiaxial warp knitted fabric, a unidirectional fabric, or a web. [Reference numerals] (AA) Start; (BB) End; (S101) Preparing a fiber layer of a predetermined thickness using a heat resistant fiber; (S102) Laminating the prepared fiber layers and needle-punching the fiber layers while compressing; (S103) Thermally treating the fiber reinforcing material; (S104) Filling the fiber reinforcing material with a carbon ingredient |
| format | Patent |
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CONSTITUTION: A method for fabricating a needle-punched carbon composite comprises: a step of preparing a fiber layer of a predetermined thickness using a heat resistant fiber(S101); a step of laminating the prepared fiber layers and needle-punching while compressing the fiber layers to tight the fiber layers(S102); a step of performing thermal treatment of the fiber reinforcing material(S103); and a step of filling the fiber reinforcing material with a carbon ingredient(S104). The heat resistant fiber is an oxidized-polyacrylonitrile fiber. The fiber layer has a form of a woven fabric, a non-woven fabric, a knitted fabric, a multiaxial warp knitted fabric, a unidirectional fabric, or a web. [Reference numerals] (AA) Start; (BB) End; (S101) Preparing a fiber layer of a predetermined thickness using a heat resistant fiber; (S102) Laminating the prepared fiber layers and needle-punching the fiber layers while compressing; (S103) Thermally treating the fiber reinforcing material; (S104) Filling the fiber reinforcing material with a carbon ingredient</description><language>eng ; kor</language><subject>BRAIDING ; COTTON-WOOL ; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS,NON-WOVEN FABRICS ; KNITTING ; LACE-MAKING ; LAYERED PRODUCTS ; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM ; MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARYMATERIAL ; NON-WOVEN FABRICS ; PERFORMING OPERATIONS ; TEXTILES ; TRANSPORTING ; TRIMMINGS ; WADDING</subject><creationdate>2013</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=20130115&DB=EPODOC&CC=KR&NR=101222467B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20130115&DB=EPODOC&CC=KR&NR=101222467B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LEE, JAE YEOL</creatorcontrib><creatorcontrib>PARK, JONG KYOO</creatorcontrib><creatorcontrib>YUN, NAM GYUN</creatorcontrib><title>METHOD FOR THE FABRICATION OF NEEDLE-PUNCHED CARBON COMPOSITE</title><description>PURPOSE: A method for fabricating a needle-punched carbon composite is provided to prevent delamination or crack of layers and to save production cost. CONSTITUTION: A method for fabricating a needle-punched carbon composite comprises: a step of preparing a fiber layer of a predetermined thickness using a heat resistant fiber(S101); a step of laminating the prepared fiber layers and needle-punching while compressing the fiber layers to tight the fiber layers(S102); a step of performing thermal treatment of the fiber reinforcing material(S103); and a step of filling the fiber reinforcing material with a carbon ingredient(S104). The heat resistant fiber is an oxidized-polyacrylonitrile fiber. The fiber layer has a form of a woven fabric, a non-woven fabric, a knitted fabric, a multiaxial warp knitted fabric, a unidirectional fabric, or a web. [Reference numerals] (AA) Start; (BB) End; (S101) Preparing a fiber layer of a predetermined thickness using a heat resistant fiber; (S102) Laminating the prepared fiber layers and needle-punching the fiber layers while compressing; (S103) Thermally treating the fiber reinforcing material; (S104) Filling the fiber reinforcing material with a carbon ingredient</description><subject>BRAIDING</subject><subject>COTTON-WOOL</subject><subject>FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS,NON-WOVEN FABRICS</subject><subject>KNITTING</subject><subject>LACE-MAKING</subject><subject>LAYERED PRODUCTS</subject><subject>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</subject><subject>MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARYMATERIAL</subject><subject>NON-WOVEN FABRICS</subject><subject>PERFORMING OPERATIONS</subject><subject>TEXTILES</subject><subject>TRANSPORTING</subject><subject>TRIMMINGS</subject><subject>WADDING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLD1dQ3x8HdRcPMPUgjxcFVwc3QK8nR2DPH091Pwd1Pwc3V18XHVDQj1c_ZwdVFwdgxyAko4-_sG-Ad7hrjyMLCmJeYUp_JCaW4GZTfXEGcP3dSC_PjU4oLE5NS81JJ47yBDA0MjIyMTM3MnJ0Nj4lQBAK81KoM</recordid><startdate>20130115</startdate><enddate>20130115</enddate><creator>LEE, JAE YEOL</creator><creator>PARK, JONG KYOO</creator><creator>YUN, NAM GYUN</creator><scope>EVB</scope></search><sort><creationdate>20130115</creationdate><title>METHOD FOR THE FABRICATION OF NEEDLE-PUNCHED CARBON COMPOSITE</title><author>LEE, JAE YEOL ; PARK, JONG KYOO ; YUN, NAM GYUN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR101222467BB13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; kor</language><creationdate>2013</creationdate><topic>BRAIDING</topic><topic>COTTON-WOOL</topic><topic>FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS,NON-WOVEN FABRICS</topic><topic>KNITTING</topic><topic>LACE-MAKING</topic><topic>LAYERED PRODUCTS</topic><topic>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</topic><topic>MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARYMATERIAL</topic><topic>NON-WOVEN FABRICS</topic><topic>PERFORMING OPERATIONS</topic><topic>TEXTILES</topic><topic>TRANSPORTING</topic><topic>TRIMMINGS</topic><topic>WADDING</topic><toplevel>online_resources</toplevel><creatorcontrib>LEE, JAE YEOL</creatorcontrib><creatorcontrib>PARK, JONG KYOO</creatorcontrib><creatorcontrib>YUN, NAM GYUN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LEE, JAE YEOL</au><au>PARK, JONG KYOO</au><au>YUN, NAM GYUN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD FOR THE FABRICATION OF NEEDLE-PUNCHED CARBON COMPOSITE</title><date>2013-01-15</date><risdate>2013</risdate><abstract>PURPOSE: A method for fabricating a needle-punched carbon composite is provided to prevent delamination or crack of layers and to save production cost. CONSTITUTION: A method for fabricating a needle-punched carbon composite comprises: a step of preparing a fiber layer of a predetermined thickness using a heat resistant fiber(S101); a step of laminating the prepared fiber layers and needle-punching while compressing the fiber layers to tight the fiber layers(S102); a step of performing thermal treatment of the fiber reinforcing material(S103); and a step of filling the fiber reinforcing material with a carbon ingredient(S104). The heat resistant fiber is an oxidized-polyacrylonitrile fiber. The fiber layer has a form of a woven fabric, a non-woven fabric, a knitted fabric, a multiaxial warp knitted fabric, a unidirectional fabric, or a web. [Reference numerals] (AA) Start; (BB) End; (S101) Preparing a fiber layer of a predetermined thickness using a heat resistant fiber; (S102) Laminating the prepared fiber layers and needle-punching the fiber layers while compressing; (S103) Thermally treating the fiber reinforcing material; (S104) Filling the fiber reinforcing material with a carbon ingredient</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; kor |
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| subjects | BRAIDING COTTON-WOOL FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS,NON-WOVEN FABRICS KNITTING LACE-MAKING LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARYMATERIAL NON-WOVEN FABRICS PERFORMING OPERATIONS TEXTILES TRANSPORTING TRIMMINGS WADDING |
| title | METHOD FOR THE FABRICATION OF NEEDLE-PUNCHED CARBON COMPOSITE |
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