Manufacturing method of high-strength alloy cold-drawn wire for aircraft fastener
The invention relates to a manufacturing method of a high-strength alloy cold-drawn wire for an aircraft fastener. The manufacturing method comprises the following steps: taking return steel, chromium metal, a nickel plate, pure iron, manganese metal, molybdenum metal, pure titanium, aluminum metal,...
Gespeichert in:
Hauptverfasser: | , , , , , |
---|---|
Format: | Patent |
Sprache: | chi ; eng |
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 | ZHANG LING PEI BINGHONG WANG RUI FENG XU CHEN PANQUAN HE YUNHUA |
description | The invention relates to a manufacturing method of a high-strength alloy cold-drawn wire for an aircraft fastener. The manufacturing method comprises the following steps: taking return steel, chromium metal, a nickel plate, pure iron, manganese metal, molybdenum metal, pure titanium, aluminum metal, ferroboron and nickel-magnesium alloy as raw materials, and performing a smelting process through a vacuum induction furnace and a consumable electrode vacuum furnace to obtain a steel ingot; carrying out forging hot working and rolling hot working on the steel ingot to obtain a wire rod blank; and after the wire rod blank is subjected to solid solution, surface treatment and cold drawing machining, the high-strength alloy cold-drawn wire for the aircraft fastener is obtained. When the vacuum induction furnace and the consumable electrode furnace are used for smelting, the return steel is used, so that the addition of metal chromium, pure iron and nickel plates is greatly reduced, and the production cost is reduce |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN116441344A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN116441344A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN116441344A3</originalsourceid><addsrcrecordid>eNqNyr0KwjAQAOAuDqK-w_kAGUKDuxTFRUFwL0dy-YE0KZcrxbfXwQdw-pZv2z3vWBaPVhZOJcBEEquD6iGmEFUTphIkAuZc32BrdsoxrgXWxAS-MmBiy-gFPDahQrzvNh5zo8PPXXe8Xl7DTdFcR2oz2u-ScXhofTJG98ac-3_OB_mTN-Q</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Manufacturing method of high-strength alloy cold-drawn wire for aircraft fastener</title><source>esp@cenet</source><creator>ZHANG LING ; PEI BINGHONG ; WANG RUI ; FENG XU ; CHEN PANQUAN ; HE YUNHUA</creator><creatorcontrib>ZHANG LING ; PEI BINGHONG ; WANG RUI ; FENG XU ; CHEN PANQUAN ; HE YUNHUA</creatorcontrib><description>The invention relates to a manufacturing method of a high-strength alloy cold-drawn wire for an aircraft fastener. The manufacturing method comprises the following steps: taking return steel, chromium metal, a nickel plate, pure iron, manganese metal, molybdenum metal, pure titanium, aluminum metal, ferroboron and nickel-magnesium alloy as raw materials, and performing a smelting process through a vacuum induction furnace and a consumable electrode vacuum furnace to obtain a steel ingot; carrying out forging hot working and rolling hot working on the steel ingot to obtain a wire rod blank; and after the wire rod blank is subjected to solid solution, surface treatment and cold drawing machining, the high-strength alloy cold-drawn wire for the aircraft fastener is obtained. When the vacuum induction furnace and the consumable electrode furnace are used for smelting, the return steel is used, so that the addition of metal chromium, pure iron and nickel plates is greatly reduced, and the production cost is reduce</description><language>chi ; eng</language><subject>ALLOYS ; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKINGWITHOUT ESSENTIALLY REMOVING MATERIAL ; CHEMISTRY ; FERROUS OR NON-FERROUS ALLOYS ; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS ; MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS ; MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES,OTHERWISE THAN BY ROLLING ; MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL ; METALLURGY ; METALLURGY OF IRON ; MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS ; PERFORMING OPERATIONS ; PUNCHING METAL ; TRANSPORTING ; TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><creationdate>2023</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=20230718&DB=EPODOC&CC=CN&NR=116441344A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230718&DB=EPODOC&CC=CN&NR=116441344A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ZHANG LING</creatorcontrib><creatorcontrib>PEI BINGHONG</creatorcontrib><creatorcontrib>WANG RUI</creatorcontrib><creatorcontrib>FENG XU</creatorcontrib><creatorcontrib>CHEN PANQUAN</creatorcontrib><creatorcontrib>HE YUNHUA</creatorcontrib><title>Manufacturing method of high-strength alloy cold-drawn wire for aircraft fastener</title><description>The invention relates to a manufacturing method of a high-strength alloy cold-drawn wire for an aircraft fastener. The manufacturing method comprises the following steps: taking return steel, chromium metal, a nickel plate, pure iron, manganese metal, molybdenum metal, pure titanium, aluminum metal, ferroboron and nickel-magnesium alloy as raw materials, and performing a smelting process through a vacuum induction furnace and a consumable electrode vacuum furnace to obtain a steel ingot; carrying out forging hot working and rolling hot working on the steel ingot to obtain a wire rod blank; and after the wire rod blank is subjected to solid solution, surface treatment and cold drawing machining, the high-strength alloy cold-drawn wire for the aircraft fastener is obtained. When the vacuum induction furnace and the consumable electrode furnace are used for smelting, the return steel is used, so that the addition of metal chromium, pure iron and nickel plates is greatly reduced, and the production cost is reduce</description><subject>ALLOYS</subject><subject>AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKINGWITHOUT ESSENTIALLY REMOVING MATERIAL</subject><subject>CHEMISTRY</subject><subject>FERROUS OR NON-FERROUS ALLOYS</subject><subject>GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS</subject><subject>MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS</subject><subject>MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES,OTHERWISE THAN BY ROLLING</subject><subject>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</subject><subject>METALLURGY</subject><subject>METALLURGY OF IRON</subject><subject>MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS</subject><subject>PERFORMING OPERATIONS</subject><subject>PUNCHING METAL</subject><subject>TRANSPORTING</subject><subject>TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyr0KwjAQAOAuDqK-w_kAGUKDuxTFRUFwL0dy-YE0KZcrxbfXwQdw-pZv2z3vWBaPVhZOJcBEEquD6iGmEFUTphIkAuZc32BrdsoxrgXWxAS-MmBiy-gFPDahQrzvNh5zo8PPXXe8Xl7DTdFcR2oz2u-ScXhofTJG98ac-3_OB_mTN-Q</recordid><startdate>20230718</startdate><enddate>20230718</enddate><creator>ZHANG LING</creator><creator>PEI BINGHONG</creator><creator>WANG RUI</creator><creator>FENG XU</creator><creator>CHEN PANQUAN</creator><creator>HE YUNHUA</creator><scope>EVB</scope></search><sort><creationdate>20230718</creationdate><title>Manufacturing method of high-strength alloy cold-drawn wire for aircraft fastener</title><author>ZHANG LING ; PEI BINGHONG ; WANG RUI ; FENG XU ; CHEN PANQUAN ; HE YUNHUA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116441344A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>ALLOYS</topic><topic>AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKINGWITHOUT ESSENTIALLY REMOVING MATERIAL</topic><topic>CHEMISTRY</topic><topic>FERROUS OR NON-FERROUS ALLOYS</topic><topic>GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS</topic><topic>MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS</topic><topic>MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES,OTHERWISE THAN BY ROLLING</topic><topic>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</topic><topic>METALLURGY</topic><topic>METALLURGY OF IRON</topic><topic>MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS</topic><topic>PERFORMING OPERATIONS</topic><topic>PUNCHING METAL</topic><topic>TRANSPORTING</topic><topic>TREATMENT OF ALLOYS OR NON-FERROUS METALS</topic><toplevel>online_resources</toplevel><creatorcontrib>ZHANG LING</creatorcontrib><creatorcontrib>PEI BINGHONG</creatorcontrib><creatorcontrib>WANG RUI</creatorcontrib><creatorcontrib>FENG XU</creatorcontrib><creatorcontrib>CHEN PANQUAN</creatorcontrib><creatorcontrib>HE YUNHUA</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHANG LING</au><au>PEI BINGHONG</au><au>WANG RUI</au><au>FENG XU</au><au>CHEN PANQUAN</au><au>HE YUNHUA</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Manufacturing method of high-strength alloy cold-drawn wire for aircraft fastener</title><date>2023-07-18</date><risdate>2023</risdate><abstract>The invention relates to a manufacturing method of a high-strength alloy cold-drawn wire for an aircraft fastener. The manufacturing method comprises the following steps: taking return steel, chromium metal, a nickel plate, pure iron, manganese metal, molybdenum metal, pure titanium, aluminum metal, ferroboron and nickel-magnesium alloy as raw materials, and performing a smelting process through a vacuum induction furnace and a consumable electrode vacuum furnace to obtain a steel ingot; carrying out forging hot working and rolling hot working on the steel ingot to obtain a wire rod blank; and after the wire rod blank is subjected to solid solution, surface treatment and cold drawing machining, the high-strength alloy cold-drawn wire for the aircraft fastener is obtained. When the vacuum induction furnace and the consumable electrode furnace are used for smelting, the return steel is used, so that the addition of metal chromium, pure iron and nickel plates is greatly reduced, and the production cost is reduce</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | chi ; eng |
recordid | cdi_epo_espacenet_CN116441344A |
source | esp@cenet |
subjects | ALLOYS AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKINGWITHOUT ESSENTIALLY REMOVING MATERIAL CHEMISTRY FERROUS OR NON-FERROUS ALLOYS GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES,OTHERWISE THAN BY ROLLING MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL METALLURGY METALLURGY OF IRON MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS PERFORMING OPERATIONS PUNCHING METAL TRANSPORTING TREATMENT OF ALLOYS OR NON-FERROUS METALS |
title | Manufacturing method of high-strength alloy cold-drawn wire for aircraft fastener |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-20T02%3A41%3A39IST&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=ZHANG%20LING&rft.date=2023-07-18&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN116441344A%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 |