NICKEL-BASE HEAT-RESISTANT DEFORMABLE ALLOY AND ARTICLE MADE OF THIS ALLOY

FIELD: metallurgy. ^ SUBSTANCE: invention relates to nickel-base heat-resistant deformable alloys and articles made of these alloys used in aviation technique, machine engineering and other branches of industry. Invention proposes nickel-base heat-resistant deformable alloy and article made of its....

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: LIMONOVA ELENA NIKOLAEVNA, LOMBERG BORIS SAMUILOVICH, OVSEPJAN SERGEJ VJACHESLAVOVICH, CHABINA ELENA BORISOVNA, KABLOV EVGENIJ NIKOLAEVICH, BAKRADZE MIKHAIL MIKHAJLOVICH, MARKINA LJUDMILA SERGEEVNA
Format: Patent
Sprache:eng ; rus
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 LIMONOVA ELENA NIKOLAEVNA
LOMBERG BORIS SAMUILOVICH
OVSEPJAN SERGEJ VJACHESLAVOVICH
CHABINA ELENA BORISOVNA
KABLOV EVGENIJ NIKOLAEVICH
BAKRADZE MIKHAIL MIKHAJLOVICH
MARKINA LJUDMILA SERGEEVNA
description FIELD: metallurgy. ^ SUBSTANCE: invention relates to nickel-base heat-resistant deformable alloys and articles made of these alloys used in aviation technique, machine engineering and other branches of industry. Invention proposes nickel-base heat-resistant deformable alloy and article made of its. Alloy comprises cobalt, chrome, tungsten, molybdenum, vanadium, aluminum, titanium, niobium, carbon, boron, lanthanum, cerium, magnesium, rhenium and scandium taken in the following ratio of components, wt.-%: cobalt, 14.0-15.9; chrome, 9.7-12.0; tungsten, 1.5-3.5; molybdenum, 3.5-4.5; rhenium, 0.5-2.5; vanadium, 0.4-0.7; aluminum, 3.5-4.2; titanium, 2.5-3.5; niobium, 2.5-4.0; carbon, 0.04-0.10; boron, 0.007-0.014; lanthanum, 0.005-0.015; cerium, 0.003-0.010; magnesium, 0.004-0.015; scandium, 0.003-0.015, and nickel, the balance. Invention provides the development of alloy for turbine disks of gas-turbine engines showing high heat-resistance in the range of temperature 650-850°C, strength and impact viscosity at room temperature, good plasticity in treatment by pressure that provides the high yield of articles and reduces the article price. Invention can be used in making turbine disks of gas-turbine engines and other units and members working at temperatures below 850°C. ^ EFFECT: improved and valuable technical properties of alloy and articles. ^ 3 cl, 2 tbl
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_RU2280091C1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>RU2280091C1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_RU2280091C13</originalsourceid><addsrcrecordid>eNrjZPDy83T2dvXRdXIMdlXwcHUM0Q1yDfYMDnH0C1FwcXXzD_J1dPJxVXD08fGPVHD0c1FwDArxdAaK-Dq6uCr4uymEeHgGQ6R5GFjTEnOKU3mhNDeDgptriLOHbmpBfnxqcUFicmpeakl8UKiRkYWBgaWhs6ExEUoA1Y0spQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>NICKEL-BASE HEAT-RESISTANT DEFORMABLE ALLOY AND ARTICLE MADE OF THIS ALLOY</title><source>esp@cenet</source><creator>LIMONOVA ELENA NIKOLAEVNA ; LOMBERG BORIS SAMUILOVICH ; OVSEPJAN SERGEJ VJACHESLAVOVICH ; CHABINA ELENA BORISOVNA ; KABLOV EVGENIJ NIKOLAEVICH ; BAKRADZE MIKHAIL MIKHAJLOVICH ; MARKINA LJUDMILA SERGEEVNA</creator><creatorcontrib>LIMONOVA ELENA NIKOLAEVNA ; LOMBERG BORIS SAMUILOVICH ; OVSEPJAN SERGEJ VJACHESLAVOVICH ; CHABINA ELENA BORISOVNA ; KABLOV EVGENIJ NIKOLAEVICH ; BAKRADZE MIKHAIL MIKHAJLOVICH ; MARKINA LJUDMILA SERGEEVNA</creatorcontrib><description>FIELD: metallurgy. ^ SUBSTANCE: invention relates to nickel-base heat-resistant deformable alloys and articles made of these alloys used in aviation technique, machine engineering and other branches of industry. Invention proposes nickel-base heat-resistant deformable alloy and article made of its. Alloy comprises cobalt, chrome, tungsten, molybdenum, vanadium, aluminum, titanium, niobium, carbon, boron, lanthanum, cerium, magnesium, rhenium and scandium taken in the following ratio of components, wt.-%: cobalt, 14.0-15.9; chrome, 9.7-12.0; tungsten, 1.5-3.5; molybdenum, 3.5-4.5; rhenium, 0.5-2.5; vanadium, 0.4-0.7; aluminum, 3.5-4.2; titanium, 2.5-3.5; niobium, 2.5-4.0; carbon, 0.04-0.10; boron, 0.007-0.014; lanthanum, 0.005-0.015; cerium, 0.003-0.010; magnesium, 0.004-0.015; scandium, 0.003-0.015, and nickel, the balance. Invention provides the development of alloy for turbine disks of gas-turbine engines showing high heat-resistance in the range of temperature 650-850°C, strength and impact viscosity at room temperature, good plasticity in treatment by pressure that provides the high yield of articles and reduces the article price. Invention can be used in making turbine disks of gas-turbine engines and other units and members working at temperatures below 850°C. ^ EFFECT: improved and valuable technical properties of alloy and articles. ^ 3 cl, 2 tbl</description><language>eng ; rus</language><subject>ALLOYS ; CHEMISTRY ; FERROUS OR NON-FERROUS ALLOYS ; METALLURGY ; TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><creationdate>2006</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=20060720&amp;DB=EPODOC&amp;CC=RU&amp;NR=2280091C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20060720&amp;DB=EPODOC&amp;CC=RU&amp;NR=2280091C1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LIMONOVA ELENA NIKOLAEVNA</creatorcontrib><creatorcontrib>LOMBERG BORIS SAMUILOVICH</creatorcontrib><creatorcontrib>OVSEPJAN SERGEJ VJACHESLAVOVICH</creatorcontrib><creatorcontrib>CHABINA ELENA BORISOVNA</creatorcontrib><creatorcontrib>KABLOV EVGENIJ NIKOLAEVICH</creatorcontrib><creatorcontrib>BAKRADZE MIKHAIL MIKHAJLOVICH</creatorcontrib><creatorcontrib>MARKINA LJUDMILA SERGEEVNA</creatorcontrib><title>NICKEL-BASE HEAT-RESISTANT DEFORMABLE ALLOY AND ARTICLE MADE OF THIS ALLOY</title><description>FIELD: metallurgy. ^ SUBSTANCE: invention relates to nickel-base heat-resistant deformable alloys and articles made of these alloys used in aviation technique, machine engineering and other branches of industry. Invention proposes nickel-base heat-resistant deformable alloy and article made of its. Alloy comprises cobalt, chrome, tungsten, molybdenum, vanadium, aluminum, titanium, niobium, carbon, boron, lanthanum, cerium, magnesium, rhenium and scandium taken in the following ratio of components, wt.-%: cobalt, 14.0-15.9; chrome, 9.7-12.0; tungsten, 1.5-3.5; molybdenum, 3.5-4.5; rhenium, 0.5-2.5; vanadium, 0.4-0.7; aluminum, 3.5-4.2; titanium, 2.5-3.5; niobium, 2.5-4.0; carbon, 0.04-0.10; boron, 0.007-0.014; lanthanum, 0.005-0.015; cerium, 0.003-0.010; magnesium, 0.004-0.015; scandium, 0.003-0.015, and nickel, the balance. Invention provides the development of alloy for turbine disks of gas-turbine engines showing high heat-resistance in the range of temperature 650-850°C, strength and impact viscosity at room temperature, good plasticity in treatment by pressure that provides the high yield of articles and reduces the article price. Invention can be used in making turbine disks of gas-turbine engines and other units and members working at temperatures below 850°C. ^ EFFECT: improved and valuable technical properties of alloy and articles. ^ 3 cl, 2 tbl</description><subject>ALLOYS</subject><subject>CHEMISTRY</subject><subject>FERROUS OR NON-FERROUS ALLOYS</subject><subject>METALLURGY</subject><subject>TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2006</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPDy83T2dvXRdXIMdlXwcHUM0Q1yDfYMDnH0C1FwcXXzD_J1dPJxVXD08fGPVHD0c1FwDArxdAaK-Dq6uCr4uymEeHgGQ6R5GFjTEnOKU3mhNDeDgptriLOHbmpBfnxqcUFicmpeakl8UKiRkYWBgaWhs6ExEUoA1Y0spQ</recordid><startdate>20060720</startdate><enddate>20060720</enddate><creator>LIMONOVA ELENA NIKOLAEVNA</creator><creator>LOMBERG BORIS SAMUILOVICH</creator><creator>OVSEPJAN SERGEJ VJACHESLAVOVICH</creator><creator>CHABINA ELENA BORISOVNA</creator><creator>KABLOV EVGENIJ NIKOLAEVICH</creator><creator>BAKRADZE MIKHAIL MIKHAJLOVICH</creator><creator>MARKINA LJUDMILA SERGEEVNA</creator><scope>EVB</scope></search><sort><creationdate>20060720</creationdate><title>NICKEL-BASE HEAT-RESISTANT DEFORMABLE ALLOY AND ARTICLE MADE OF THIS ALLOY</title><author>LIMONOVA ELENA NIKOLAEVNA ; LOMBERG BORIS SAMUILOVICH ; OVSEPJAN SERGEJ VJACHESLAVOVICH ; CHABINA ELENA BORISOVNA ; KABLOV EVGENIJ NIKOLAEVICH ; BAKRADZE MIKHAIL MIKHAJLOVICH ; MARKINA LJUDMILA SERGEEVNA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2280091C13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2006</creationdate><topic>ALLOYS</topic><topic>CHEMISTRY</topic><topic>FERROUS OR NON-FERROUS ALLOYS</topic><topic>METALLURGY</topic><topic>TREATMENT OF ALLOYS OR NON-FERROUS METALS</topic><toplevel>online_resources</toplevel><creatorcontrib>LIMONOVA ELENA NIKOLAEVNA</creatorcontrib><creatorcontrib>LOMBERG BORIS SAMUILOVICH</creatorcontrib><creatorcontrib>OVSEPJAN SERGEJ VJACHESLAVOVICH</creatorcontrib><creatorcontrib>CHABINA ELENA BORISOVNA</creatorcontrib><creatorcontrib>KABLOV EVGENIJ NIKOLAEVICH</creatorcontrib><creatorcontrib>BAKRADZE MIKHAIL MIKHAJLOVICH</creatorcontrib><creatorcontrib>MARKINA LJUDMILA SERGEEVNA</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LIMONOVA ELENA NIKOLAEVNA</au><au>LOMBERG BORIS SAMUILOVICH</au><au>OVSEPJAN SERGEJ VJACHESLAVOVICH</au><au>CHABINA ELENA BORISOVNA</au><au>KABLOV EVGENIJ NIKOLAEVICH</au><au>BAKRADZE MIKHAIL MIKHAJLOVICH</au><au>MARKINA LJUDMILA SERGEEVNA</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>NICKEL-BASE HEAT-RESISTANT DEFORMABLE ALLOY AND ARTICLE MADE OF THIS ALLOY</title><date>2006-07-20</date><risdate>2006</risdate><abstract>FIELD: metallurgy. ^ SUBSTANCE: invention relates to nickel-base heat-resistant deformable alloys and articles made of these alloys used in aviation technique, machine engineering and other branches of industry. Invention proposes nickel-base heat-resistant deformable alloy and article made of its. Alloy comprises cobalt, chrome, tungsten, molybdenum, vanadium, aluminum, titanium, niobium, carbon, boron, lanthanum, cerium, magnesium, rhenium and scandium taken in the following ratio of components, wt.-%: cobalt, 14.0-15.9; chrome, 9.7-12.0; tungsten, 1.5-3.5; molybdenum, 3.5-4.5; rhenium, 0.5-2.5; vanadium, 0.4-0.7; aluminum, 3.5-4.2; titanium, 2.5-3.5; niobium, 2.5-4.0; carbon, 0.04-0.10; boron, 0.007-0.014; lanthanum, 0.005-0.015; cerium, 0.003-0.010; magnesium, 0.004-0.015; scandium, 0.003-0.015, and nickel, the balance. Invention provides the development of alloy for turbine disks of gas-turbine engines showing high heat-resistance in the range of temperature 650-850°C, strength and impact viscosity at room temperature, good plasticity in treatment by pressure that provides the high yield of articles and reduces the article price. Invention can be used in making turbine disks of gas-turbine engines and other units and members working at temperatures below 850°C. ^ EFFECT: improved and valuable technical properties of alloy and articles. ^ 3 cl, 2 tbl</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; rus
recordid cdi_epo_espacenet_RU2280091C1
source esp@cenet
subjects ALLOYS
CHEMISTRY
FERROUS OR NON-FERROUS ALLOYS
METALLURGY
TREATMENT OF ALLOYS OR NON-FERROUS METALS
title NICKEL-BASE HEAT-RESISTANT DEFORMABLE ALLOY AND ARTICLE MADE OF THIS ALLOY
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-02T10%3A59%3A59IST&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=LIMONOVA%20ELENA%20NIKOLAEVNA&rft.date=2006-07-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ERU2280091C1%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