NICKEL-BASED SUPERALLOY, MECHANICAL COMPONENT MADE OF THE ABOVE MENTIONED SUPERALLOY, PIECE OF TURBOMACHINERY WHICH INCLUDES THE ABOVE MENTIONED COMPONENT AND RELATED METHODS

A nickel-based superalloy particularly suitable for the fabrication of mechanical components for a piece of turbomachinery is provided. The nickel-based superalloy consists of in percentage by weight: chromium between 4% and 6%; tungsten between 3% and 15%; tantalum between 4.5% and 5.5%; aluminium...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: TASSA, ORIANA, CAROSI, ANDREA, MARESCA, PASQUALE, TESTANI, CLAUDIO, INNOCENTI, MARCO, GIAMBI, BARBARA
Format: Patent
Sprache:eng ; fre
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator TASSA, ORIANA
CAROSI, ANDREA
MARESCA, PASQUALE
TESTANI, CLAUDIO
INNOCENTI, MARCO
GIAMBI, BARBARA
description A nickel-based superalloy particularly suitable for the fabrication of mechanical components for a piece of turbomachinery is provided. The nickel-based superalloy consists of in percentage by weight: chromium between 4% and 6%; tungsten between 3% and 15%; tantalum between 4.5% and 5.5%; aluminium between 5% and 7%; carbon less than 0.1%; yttrium oxide in a percentage by volume of up to 7%; optionally cobalt in less than 5%; optionally one or more of hafnium or zirconium up to a total of 2%; optionally rhenium between 0% and 10%; and the remaining percentage of nickel plus impurities. Un superalliage à base de nickel particulièrement adapté à la fabrication de composants mécaniques pour une pièce de turbomachine est fourni. Le superalliage à base de nickel est constitué en pourcentage en poids : entre 4 % et 6 % de chrome; entre 3 % et 15 % de tungstène; entre 4,5 % et 5,5 % de tantale; entre 5 % et 7 % daluminium; moins de 0,1 % de carbone; pourcentage volumique doxyde dyttrium allant jusquà 7 %; possiblement de cobalt à moins de 5%; possiblement dun ou de plusieurs éléments parmi lhafnium ou le zirconium, jusquà concurrence de 2 % au total; possiblement du rhénium entre 0 % et 10 %; et le pourcentage restant de nickel plus impuretés.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CA2711325C</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CA2711325C</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CA2711325C3</originalsourceid><addsrcrecordid>eNqFjb0KwkAQhNNYiPoM7gOYIglivdnbcIf3E5KLkioEOSvRQHwun9GAggiC1cDMNzPz6GEV7VnHOdYsoG5KrlBr127AMEmcUtRAzpTOsvVgUDC4ArxkwNwdeMKsV1P4XS4V0wtsqtwZJKksVy0cpSIJypJuBNc_Zz5naAVUrNFPrmEvnaiX0ezcX8aweusiWhfsScZhuHVhHPpTuIZ7R5jukiRLt5T9J54ExUeR</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>NICKEL-BASED SUPERALLOY, MECHANICAL COMPONENT MADE OF THE ABOVE MENTIONED SUPERALLOY, PIECE OF TURBOMACHINERY WHICH INCLUDES THE ABOVE MENTIONED COMPONENT AND RELATED METHODS</title><source>esp@cenet</source><creator>TASSA, ORIANA ; CAROSI, ANDREA ; MARESCA, PASQUALE ; TESTANI, CLAUDIO ; INNOCENTI, MARCO ; GIAMBI, BARBARA</creator><creatorcontrib>TASSA, ORIANA ; CAROSI, ANDREA ; MARESCA, PASQUALE ; TESTANI, CLAUDIO ; INNOCENTI, MARCO ; GIAMBI, BARBARA</creatorcontrib><description>A nickel-based superalloy particularly suitable for the fabrication of mechanical components for a piece of turbomachinery is provided. The nickel-based superalloy consists of in percentage by weight: chromium between 4% and 6%; tungsten between 3% and 15%; tantalum between 4.5% and 5.5%; aluminium between 5% and 7%; carbon less than 0.1%; yttrium oxide in a percentage by volume of up to 7%; optionally cobalt in less than 5%; optionally one or more of hafnium or zirconium up to a total of 2%; optionally rhenium between 0% and 10%; and the remaining percentage of nickel plus impurities. Un superalliage à base de nickel particulièrement adapté à la fabrication de composants mécaniques pour une pièce de turbomachine est fourni. Le superalliage à base de nickel est constitué en pourcentage en poids : entre 4 % et 6 % de chrome; entre 3 % et 15 % de tungstène; entre 4,5 % et 5,5 % de tantale; entre 5 % et 7 % daluminium; moins de 0,1 % de carbone; pourcentage volumique doxyde dyttrium allant jusquà 7 %; possiblement de cobalt à moins de 5%; possiblement dun ou de plusieurs éléments parmi lhafnium ou le zirconium, jusquà concurrence de 2 % au total; possiblement du rhénium entre 0 % et 10 %; et le pourcentage restant de nickel plus impuretés.</description><language>eng ; fre</language><subject>ALLOYS ; BLASTING ; CHEMISTRY ; ENGINE PLANTS IN GENERAL ; FERROUS OR NON-FERROUS ALLOYS ; HEATING ; 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>2019</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&amp;date=20190514&amp;DB=EPODOC&amp;CC=CA&amp;NR=2711325C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20190514&amp;DB=EPODOC&amp;CC=CA&amp;NR=2711325C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TASSA, ORIANA</creatorcontrib><creatorcontrib>CAROSI, ANDREA</creatorcontrib><creatorcontrib>MARESCA, PASQUALE</creatorcontrib><creatorcontrib>TESTANI, CLAUDIO</creatorcontrib><creatorcontrib>INNOCENTI, MARCO</creatorcontrib><creatorcontrib>GIAMBI, BARBARA</creatorcontrib><title>NICKEL-BASED SUPERALLOY, MECHANICAL COMPONENT MADE OF THE ABOVE MENTIONED SUPERALLOY, PIECE OF TURBOMACHINERY WHICH INCLUDES THE ABOVE MENTIONED COMPONENT AND RELATED METHODS</title><description>A nickel-based superalloy particularly suitable for the fabrication of mechanical components for a piece of turbomachinery is provided. The nickel-based superalloy consists of in percentage by weight: chromium between 4% and 6%; tungsten between 3% and 15%; tantalum between 4.5% and 5.5%; aluminium between 5% and 7%; carbon less than 0.1%; yttrium oxide in a percentage by volume of up to 7%; optionally cobalt in less than 5%; optionally one or more of hafnium or zirconium up to a total of 2%; optionally rhenium between 0% and 10%; and the remaining percentage of nickel plus impurities. Un superalliage à base de nickel particulièrement adapté à la fabrication de composants mécaniques pour une pièce de turbomachine est fourni. Le superalliage à base de nickel est constitué en pourcentage en poids : entre 4 % et 6 % de chrome; entre 3 % et 15 % de tungstène; entre 4,5 % et 5,5 % de tantale; entre 5 % et 7 % daluminium; moins de 0,1 % de carbone; pourcentage volumique doxyde dyttrium allant jusquà 7 %; possiblement de cobalt à moins de 5%; possiblement dun ou de plusieurs éléments parmi lhafnium ou le zirconium, jusquà concurrence de 2 % au total; possiblement du rhénium entre 0 % et 10 %; et le pourcentage restant de nickel plus impuretés.</description><subject>ALLOYS</subject><subject>BLASTING</subject><subject>CHEMISTRY</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>FERROUS OR NON-FERROUS ALLOYS</subject><subject>HEATING</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqFjb0KwkAQhNNYiPoM7gOYIglivdnbcIf3E5KLkioEOSvRQHwun9GAggiC1cDMNzPz6GEV7VnHOdYsoG5KrlBr127AMEmcUtRAzpTOsvVgUDC4ArxkwNwdeMKsV1P4XS4V0wtsqtwZJKksVy0cpSIJypJuBNc_Zz5naAVUrNFPrmEvnaiX0ezcX8aweusiWhfsScZhuHVhHPpTuIZ7R5jukiRLt5T9J54ExUeR</recordid><startdate>20190514</startdate><enddate>20190514</enddate><creator>TASSA, ORIANA</creator><creator>CAROSI, ANDREA</creator><creator>MARESCA, PASQUALE</creator><creator>TESTANI, CLAUDIO</creator><creator>INNOCENTI, MARCO</creator><creator>GIAMBI, BARBARA</creator><scope>EVB</scope></search><sort><creationdate>20190514</creationdate><title>NICKEL-BASED SUPERALLOY, MECHANICAL COMPONENT MADE OF THE ABOVE MENTIONED SUPERALLOY, PIECE OF TURBOMACHINERY WHICH INCLUDES THE ABOVE MENTIONED COMPONENT AND RELATED METHODS</title><author>TASSA, ORIANA ; CAROSI, ANDREA ; MARESCA, PASQUALE ; TESTANI, CLAUDIO ; INNOCENTI, MARCO ; GIAMBI, BARBARA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2711325C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2019</creationdate><topic>ALLOYS</topic><topic>BLASTING</topic><topic>CHEMISTRY</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>FERROUS OR NON-FERROUS ALLOYS</topic><topic>HEATING</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>TASSA, ORIANA</creatorcontrib><creatorcontrib>CAROSI, ANDREA</creatorcontrib><creatorcontrib>MARESCA, PASQUALE</creatorcontrib><creatorcontrib>TESTANI, CLAUDIO</creatorcontrib><creatorcontrib>INNOCENTI, MARCO</creatorcontrib><creatorcontrib>GIAMBI, BARBARA</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TASSA, ORIANA</au><au>CAROSI, ANDREA</au><au>MARESCA, PASQUALE</au><au>TESTANI, CLAUDIO</au><au>INNOCENTI, MARCO</au><au>GIAMBI, BARBARA</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>NICKEL-BASED SUPERALLOY, MECHANICAL COMPONENT MADE OF THE ABOVE MENTIONED SUPERALLOY, PIECE OF TURBOMACHINERY WHICH INCLUDES THE ABOVE MENTIONED COMPONENT AND RELATED METHODS</title><date>2019-05-14</date><risdate>2019</risdate><abstract>A nickel-based superalloy particularly suitable for the fabrication of mechanical components for a piece of turbomachinery is provided. The nickel-based superalloy consists of in percentage by weight: chromium between 4% and 6%; tungsten between 3% and 15%; tantalum between 4.5% and 5.5%; aluminium between 5% and 7%; carbon less than 0.1%; yttrium oxide in a percentage by volume of up to 7%; optionally cobalt in less than 5%; optionally one or more of hafnium or zirconium up to a total of 2%; optionally rhenium between 0% and 10%; and the remaining percentage of nickel plus impurities. Un superalliage à base de nickel particulièrement adapté à la fabrication de composants mécaniques pour une pièce de turbomachine est fourni. Le superalliage à base de nickel est constitué en pourcentage en poids : entre 4 % et 6 % de chrome; entre 3 % et 15 % de tungstène; entre 4,5 % et 5,5 % de tantale; entre 5 % et 7 % daluminium; moins de 0,1 % de carbone; pourcentage volumique doxyde dyttrium allant jusquà 7 %; possiblement de cobalt à moins de 5%; possiblement dun ou de plusieurs éléments parmi lhafnium ou le zirconium, jusquà concurrence de 2 % au total; possiblement du rhénium entre 0 % et 10 %; et le pourcentage restant de nickel plus impuretés.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre
recordid cdi_epo_espacenet_CA2711325C
source esp@cenet
subjects ALLOYS
BLASTING
CHEMISTRY
ENGINE PLANTS IN GENERAL
FERROUS OR NON-FERROUS ALLOYS
HEATING
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 NICKEL-BASED SUPERALLOY, MECHANICAL COMPONENT MADE OF THE ABOVE MENTIONED SUPERALLOY, PIECE OF TURBOMACHINERY WHICH INCLUDES THE ABOVE MENTIONED COMPONENT AND RELATED METHODS
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-24T12%3A06%3A38IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=TASSA,%20ORIANA&rft.date=2019-05-14&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECA2711325C%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true