Ni-BASED SINGLE CRYSTAL SUPERALLOY
A Ni-based single crystal superalloy which contains from 6% by mass to 12% by mass (inclusive) of Cr, from 0.4% by mass to 3.0% by mass (inclusive) of Mo, from 6% by mass to 10% by mass (inclusive) of W, from 4.0% by mass to 6.5% by mass (inclusive) of Al, from 0% by mass to 1% by mass (inclusive) o...
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| creator | TORII SHUNSUKE UEMURA YOSHITAKA MASADA JUNICHIRO SAKAMOTO MASAO SHIMOHATA SACHIO KOBAYASHI TOSHIHARU HARADA HIROSHI YOKOKAWA TADAHARU OGUMA HIDETAKA KAWAGISHI KYOKO TANEIKE MASAKI KOIZUMI YUTAKA OKIMOTO RYOTA OKADA IKUO TSUKAGOSHI KEIZO YUYAMA MICHINARI |
| description | A Ni-based single crystal superalloy which contains from 6% by mass to 12% by mass (inclusive) of Cr, from 0.4% by mass to 3.0% by mass (inclusive) of Mo, from 6% by mass to 10% by mass (inclusive) of W, from 4.0% by mass to 6.5% by mass (inclusive) of Al, from 0% by mass to 1% by mass (inclusive) of Nb, from 8% by mass to 12% by mass (inclusive) of Ta, from 0% by mass to 0.15% by mass (inclusive) of Hf, from 0.01% by mass to 0.2% by mass (inclusive) of Si and from 0% by mass to 0.04% by mass (inclusive) of Zr, while optionally containing at least one element that is selected from among B, C, Y, La, Ce and V, with the balance made up of Ni and unavoidable impurities.
La présente invention se rapporte à un superalliage monocristallin à base de nickel (Ni) qui contient une quantité de chrome (Cr) comprise entre 6 % en masse et 12 % en masse (inclus), une quantité de molybdène (Mo) comprise entre 0,4 % en masse et 3,0 % en masse (inclus), une quantité de tungstène (W) comprise entre 6 % en masse et 10 % en masse (inclus), une quantité d'aluminium (Al) comprise entre 4,0 % en masse et 6,4 % en masse (inclus), une quantité de niobium (Nb) comprise entre 0 % en masse et 1 % en masse (inclus), une quantité de tantale (Ta) comprise entre 8 % en masse et 12 % en masse (inclus), une quantité de hafnium (Hf) comprise entre 0 % en masse et 0,15 % en masse (inclus), une quantité de silicium (Si) comprise entre 0,01 % en masse et 0,2 % en masse (inclus) et une quantité de zirconium (Zr) comprise entre 0 % en masse et 0,04 % en masse (inclus) tout en contenant facultativement au moins un élément qui est sélectionné dans le groupe constitué par le bore (B), le carbone (C), l'yttrium (Y), le lanthane (La), le cérium (Ce) et le vanadium (V), le reste étant composé de nickel (Ni) et d'impuretés inévitables. |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_WO2014024734A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>WO2014024734A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_WO2014024734A13</originalsourceid><addsrcrecordid>eNrjZFDyy9R1cgx2dVEI9vRz93FVcA6KDA5x9FEIDg1wDXL08fGP5GFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8eH-RgaGJgZGJubGJo6GxsSpAgDTjSOG</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Ni-BASED SINGLE CRYSTAL SUPERALLOY</title><source>esp@cenet</source><creator>TORII SHUNSUKE ; UEMURA YOSHITAKA ; MASADA JUNICHIRO ; SAKAMOTO MASAO ; SHIMOHATA SACHIO ; KOBAYASHI TOSHIHARU ; HARADA HIROSHI ; YOKOKAWA TADAHARU ; OGUMA HIDETAKA ; KAWAGISHI KYOKO ; TANEIKE MASAKI ; KOIZUMI YUTAKA ; OKIMOTO RYOTA ; OKADA IKUO ; TSUKAGOSHI KEIZO ; YUYAMA MICHINARI</creator><creatorcontrib>TORII SHUNSUKE ; UEMURA YOSHITAKA ; MASADA JUNICHIRO ; SAKAMOTO MASAO ; SHIMOHATA SACHIO ; KOBAYASHI TOSHIHARU ; HARADA HIROSHI ; YOKOKAWA TADAHARU ; OGUMA HIDETAKA ; KAWAGISHI KYOKO ; TANEIKE MASAKI ; KOIZUMI YUTAKA ; OKIMOTO RYOTA ; OKADA IKUO ; TSUKAGOSHI KEIZO ; YUYAMA MICHINARI</creatorcontrib><description>A Ni-based single crystal superalloy which contains from 6% by mass to 12% by mass (inclusive) of Cr, from 0.4% by mass to 3.0% by mass (inclusive) of Mo, from 6% by mass to 10% by mass (inclusive) of W, from 4.0% by mass to 6.5% by mass (inclusive) of Al, from 0% by mass to 1% by mass (inclusive) of Nb, from 8% by mass to 12% by mass (inclusive) of Ta, from 0% by mass to 0.15% by mass (inclusive) of Hf, from 0.01% by mass to 0.2% by mass (inclusive) of Si and from 0% by mass to 0.04% by mass (inclusive) of Zr, while optionally containing at least one element that is selected from among B, C, Y, La, Ce and V, with the balance made up of Ni and unavoidable impurities.
La présente invention se rapporte à un superalliage monocristallin à base de nickel (Ni) qui contient une quantité de chrome (Cr) comprise entre 6 % en masse et 12 % en masse (inclus), une quantité de molybdène (Mo) comprise entre 0,4 % en masse et 3,0 % en masse (inclus), une quantité de tungstène (W) comprise entre 6 % en masse et 10 % en masse (inclus), une quantité d'aluminium (Al) comprise entre 4,0 % en masse et 6,4 % en masse (inclus), une quantité de niobium (Nb) comprise entre 0 % en masse et 1 % en masse (inclus), une quantité de tantale (Ta) comprise entre 8 % en masse et 12 % en masse (inclus), une quantité de hafnium (Hf) comprise entre 0 % en masse et 0,15 % en masse (inclus), une quantité de silicium (Si) comprise entre 0,01 % en masse et 0,2 % en masse (inclus) et une quantité de zirconium (Zr) comprise entre 0 % en masse et 0,04 % en masse (inclus) tout en contenant facultativement au moins un élément qui est sélectionné dans le groupe constitué par le bore (B), le carbone (C), l'yttrium (Y), le lanthane (La), le cérium (Ce) et le vanadium (V), le reste étant composé de nickel (Ni) et d'impuretés inévitables.</description><language>eng ; fre ; jpn</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; ALLOYS ; BLASTING ; CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS ; CHEMISTRY ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; FERROUS OR NON-FERROUS ALLOYS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; METALLURGY ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; TREATMENT OF ALLOYS OR NON-FERROUS METALS ; WEAPONS</subject><creationdate>2014</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=20140213&DB=EPODOC&CC=WO&NR=2014024734A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140213&DB=EPODOC&CC=WO&NR=2014024734A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TORII SHUNSUKE</creatorcontrib><creatorcontrib>UEMURA YOSHITAKA</creatorcontrib><creatorcontrib>MASADA JUNICHIRO</creatorcontrib><creatorcontrib>SAKAMOTO MASAO</creatorcontrib><creatorcontrib>SHIMOHATA SACHIO</creatorcontrib><creatorcontrib>KOBAYASHI TOSHIHARU</creatorcontrib><creatorcontrib>HARADA HIROSHI</creatorcontrib><creatorcontrib>YOKOKAWA TADAHARU</creatorcontrib><creatorcontrib>OGUMA HIDETAKA</creatorcontrib><creatorcontrib>KAWAGISHI KYOKO</creatorcontrib><creatorcontrib>TANEIKE MASAKI</creatorcontrib><creatorcontrib>KOIZUMI YUTAKA</creatorcontrib><creatorcontrib>OKIMOTO RYOTA</creatorcontrib><creatorcontrib>OKADA IKUO</creatorcontrib><creatorcontrib>TSUKAGOSHI KEIZO</creatorcontrib><creatorcontrib>YUYAMA MICHINARI</creatorcontrib><title>Ni-BASED SINGLE CRYSTAL SUPERALLOY</title><description>A Ni-based single crystal superalloy which contains from 6% by mass to 12% by mass (inclusive) of Cr, from 0.4% by mass to 3.0% by mass (inclusive) of Mo, from 6% by mass to 10% by mass (inclusive) of W, from 4.0% by mass to 6.5% by mass (inclusive) of Al, from 0% by mass to 1% by mass (inclusive) of Nb, from 8% by mass to 12% by mass (inclusive) of Ta, from 0% by mass to 0.15% by mass (inclusive) of Hf, from 0.01% by mass to 0.2% by mass (inclusive) of Si and from 0% by mass to 0.04% by mass (inclusive) of Zr, while optionally containing at least one element that is selected from among B, C, Y, La, Ce and V, with the balance made up of Ni and unavoidable impurities.
La présente invention se rapporte à un superalliage monocristallin à base de nickel (Ni) qui contient une quantité de chrome (Cr) comprise entre 6 % en masse et 12 % en masse (inclus), une quantité de molybdène (Mo) comprise entre 0,4 % en masse et 3,0 % en masse (inclus), une quantité de tungstène (W) comprise entre 6 % en masse et 10 % en masse (inclus), une quantité d'aluminium (Al) comprise entre 4,0 % en masse et 6,4 % en masse (inclus), une quantité de niobium (Nb) comprise entre 0 % en masse et 1 % en masse (inclus), une quantité de tantale (Ta) comprise entre 8 % en masse et 12 % en masse (inclus), une quantité de hafnium (Hf) comprise entre 0 % en masse et 0,15 % en masse (inclus), une quantité de silicium (Si) comprise entre 0,01 % en masse et 0,2 % en masse (inclus) et une quantité de zirconium (Zr) comprise entre 0 % en masse et 0,04 % en masse (inclus) tout en contenant facultativement au moins un élément qui est sélectionné dans le groupe constitué par le bore (B), le carbone (C), l'yttrium (Y), le lanthane (La), le cérium (Ce) et le vanadium (V), le reste étant composé de nickel (Ni) et d'impuretés inévitables.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>ALLOYS</subject><subject>BLASTING</subject><subject>CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS</subject><subject>CHEMISTRY</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>FERROUS OR NON-FERROUS ALLOYS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>METALLURGY</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFDyy9R1cgx2dVEI9vRz93FVcA6KDA5x9FEIDg1wDXL08fGP5GFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8eH-RgaGJgZGJubGJo6GxsSpAgDTjSOG</recordid><startdate>20140213</startdate><enddate>20140213</enddate><creator>TORII SHUNSUKE</creator><creator>UEMURA YOSHITAKA</creator><creator>MASADA JUNICHIRO</creator><creator>SAKAMOTO MASAO</creator><creator>SHIMOHATA SACHIO</creator><creator>KOBAYASHI TOSHIHARU</creator><creator>HARADA HIROSHI</creator><creator>YOKOKAWA TADAHARU</creator><creator>OGUMA HIDETAKA</creator><creator>KAWAGISHI KYOKO</creator><creator>TANEIKE MASAKI</creator><creator>KOIZUMI YUTAKA</creator><creator>OKIMOTO RYOTA</creator><creator>OKADA IKUO</creator><creator>TSUKAGOSHI KEIZO</creator><creator>YUYAMA MICHINARI</creator><scope>EVB</scope></search><sort><creationdate>20140213</creationdate><title>Ni-BASED SINGLE CRYSTAL SUPERALLOY</title><author>TORII SHUNSUKE ; UEMURA YOSHITAKA ; MASADA JUNICHIRO ; SAKAMOTO MASAO ; SHIMOHATA SACHIO ; KOBAYASHI TOSHIHARU ; HARADA HIROSHI ; YOKOKAWA TADAHARU ; OGUMA HIDETAKA ; KAWAGISHI KYOKO ; TANEIKE MASAKI ; KOIZUMI YUTAKA ; OKIMOTO RYOTA ; OKADA IKUO ; TSUKAGOSHI KEIZO ; YUYAMA MICHINARI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2014024734A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; jpn</language><creationdate>2014</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>ALLOYS</topic><topic>BLASTING</topic><topic>CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS</topic><topic>CHEMISTRY</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>FERROUS OR NON-FERROUS ALLOYS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>METALLURGY</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>TREATMENT OF ALLOYS OR NON-FERROUS METALS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>TORII SHUNSUKE</creatorcontrib><creatorcontrib>UEMURA YOSHITAKA</creatorcontrib><creatorcontrib>MASADA JUNICHIRO</creatorcontrib><creatorcontrib>SAKAMOTO MASAO</creatorcontrib><creatorcontrib>SHIMOHATA SACHIO</creatorcontrib><creatorcontrib>KOBAYASHI TOSHIHARU</creatorcontrib><creatorcontrib>HARADA HIROSHI</creatorcontrib><creatorcontrib>YOKOKAWA TADAHARU</creatorcontrib><creatorcontrib>OGUMA HIDETAKA</creatorcontrib><creatorcontrib>KAWAGISHI KYOKO</creatorcontrib><creatorcontrib>TANEIKE MASAKI</creatorcontrib><creatorcontrib>KOIZUMI YUTAKA</creatorcontrib><creatorcontrib>OKIMOTO RYOTA</creatorcontrib><creatorcontrib>OKADA IKUO</creatorcontrib><creatorcontrib>TSUKAGOSHI KEIZO</creatorcontrib><creatorcontrib>YUYAMA MICHINARI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TORII SHUNSUKE</au><au>UEMURA YOSHITAKA</au><au>MASADA JUNICHIRO</au><au>SAKAMOTO MASAO</au><au>SHIMOHATA SACHIO</au><au>KOBAYASHI TOSHIHARU</au><au>HARADA HIROSHI</au><au>YOKOKAWA TADAHARU</au><au>OGUMA HIDETAKA</au><au>KAWAGISHI KYOKO</au><au>TANEIKE MASAKI</au><au>KOIZUMI YUTAKA</au><au>OKIMOTO RYOTA</au><au>OKADA IKUO</au><au>TSUKAGOSHI KEIZO</au><au>YUYAMA MICHINARI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Ni-BASED SINGLE CRYSTAL SUPERALLOY</title><date>2014-02-13</date><risdate>2014</risdate><abstract>A Ni-based single crystal superalloy which contains from 6% by mass to 12% by mass (inclusive) of Cr, from 0.4% by mass to 3.0% by mass (inclusive) of Mo, from 6% by mass to 10% by mass (inclusive) of W, from 4.0% by mass to 6.5% by mass (inclusive) of Al, from 0% by mass to 1% by mass (inclusive) of Nb, from 8% by mass to 12% by mass (inclusive) of Ta, from 0% by mass to 0.15% by mass (inclusive) of Hf, from 0.01% by mass to 0.2% by mass (inclusive) of Si and from 0% by mass to 0.04% by mass (inclusive) of Zr, while optionally containing at least one element that is selected from among B, C, Y, La, Ce and V, with the balance made up of Ni and unavoidable impurities.
La présente invention se rapporte à un superalliage monocristallin à base de nickel (Ni) qui contient une quantité de chrome (Cr) comprise entre 6 % en masse et 12 % en masse (inclus), une quantité de molybdène (Mo) comprise entre 0,4 % en masse et 3,0 % en masse (inclus), une quantité de tungstène (W) comprise entre 6 % en masse et 10 % en masse (inclus), une quantité d'aluminium (Al) comprise entre 4,0 % en masse et 6,4 % en masse (inclus), une quantité de niobium (Nb) comprise entre 0 % en masse et 1 % en masse (inclus), une quantité de tantale (Ta) comprise entre 8 % en masse et 12 % en masse (inclus), une quantité de hafnium (Hf) comprise entre 0 % en masse et 0,15 % en masse (inclus), une quantité de silicium (Si) comprise entre 0,01 % en masse et 0,2 % en masse (inclus) et une quantité de zirconium (Zr) comprise entre 0 % en masse et 0,04 % en masse (inclus) tout en contenant facultativement au moins un élément qui est sélectionné dans le groupe constitué par le bore (B), le carbone (C), l'yttrium (Y), le lanthane (La), le cérium (Ce) et le vanadium (V), le reste étant composé de nickel (Ni) et d'impuretés inévitables.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS ALLOYS BLASTING CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS CHEMISTRY COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL FERROUS OR NON-FERROUS ALLOYS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METALLURGY NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES TREATMENT OF ALLOYS OR NON-FERROUS METALS WEAPONS |
| title | Ni-BASED SINGLE CRYSTAL SUPERALLOY |
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