Integral die forging forming method for spherical shell of manned cabin of titanium alloy bathyscaph

The invention provides an integral die forging forming method for a spherical shell of a manned cabin of a titanium alloy bathyscaph. The integral die forging forming method comprises the steps that a forge piece drawing is designed; a bar is blanked, and the bar is subjected to multiple times of up...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: MO ANJUN, LI WENQIANG, XIONG YUNSEN, GONG BIN, ZENG JING, MIN WU, WEI MINGGANG, LEI JIAFENG, YU SHENGFENG
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 MO ANJUN
LI WENQIANG
XIONG YUNSEN
GONG BIN
ZENG JING
MIN WU
WEI MINGGANG
LEI JIAFENG
YU SHENGFENG
description The invention provides an integral die forging forming method for a spherical shell of a manned cabin of a titanium alloy bathyscaph. The integral die forging forming method comprises the steps that a forge piece drawing is designed; a bar is blanked, and the bar is subjected to multiple times of upsetting; the forging temperature is T beta-(30-50 DEG C), and the deformation amount is 30%-55%; the forging temperature is T beta + (5-30 DEG C), and the deformation amount is 20%-50%; the forging temperature is T beta-(30-50 DEG C), and the deformation is 10%-20%; and heat treatment. The bathyscaph manned cabin spherical shell with the three outlook holes is integrally formed in a die forging mode, welding seams are eliminated, the welding risk and the overall production cost are reduced, the connection strength between the outlook holes and the spherical shell is guaranteed, and weak links are prevented. 本发明提供了一种钛合金深潜器载人舱球壳整体模锻成形方法,包括设计锻件图;棒材下料,对棒材进行多次镦粗;第一火模锻,锻造温度Tβ-(30~50℃),变形量30%~55%;第二火模锻,锻造温度Tβ+(5~30℃),变形量2
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN114260401A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN114260401A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN114260401A3</originalsourceid><addsrcrecordid>eNqNyjEKAjEQQNE0FqLeYTyAsNHFXhZFGyv7ZTaZbALJJCSx2NtrwANYPT78tdAPrjRn9KAdgYl5djw3QzNQtVG3hJIsZae-Y7HkPUQDAZlJg8LJcevqKrJ7B0Dv4wITVrsUhcluxcqgL7T7uRH72_U13A-U4kgloSKmOg5PKfvjues7eTn983wAyT0-nw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Integral die forging forming method for spherical shell of manned cabin of titanium alloy bathyscaph</title><source>esp@cenet</source><creator>MO ANJUN ; LI WENQIANG ; XIONG YUNSEN ; GONG BIN ; ZENG JING ; MIN WU ; WEI MINGGANG ; LEI JIAFENG ; YU SHENGFENG</creator><creatorcontrib>MO ANJUN ; LI WENQIANG ; XIONG YUNSEN ; GONG BIN ; ZENG JING ; MIN WU ; WEI MINGGANG ; LEI JIAFENG ; YU SHENGFENG</creatorcontrib><description>The invention provides an integral die forging forming method for a spherical shell of a manned cabin of a titanium alloy bathyscaph. The integral die forging forming method comprises the steps that a forge piece drawing is designed; a bar is blanked, and the bar is subjected to multiple times of upsetting; the forging temperature is T beta-(30-50 DEG C), and the deformation amount is 30%-55%; the forging temperature is T beta + (5-30 DEG C), and the deformation amount is 20%-50%; the forging temperature is T beta-(30-50 DEG C), and the deformation is 10%-20%; and heat treatment. The bathyscaph manned cabin spherical shell with the three outlook holes is integrally formed in a die forging mode, welding seams are eliminated, the welding risk and the overall production cost are reduced, the connection strength between the outlook holes and the spherical shell is guaranteed, and weak links are prevented. 本发明提供了一种钛合金深潜器载人舱球壳整体模锻成形方法,包括设计锻件图;棒材下料,对棒材进行多次镦粗;第一火模锻,锻造温度Tβ-(30~50℃),变形量30%~55%;第二火模锻,锻造温度Tβ+(5~30℃),变形量2</description><language>chi ; eng</language><subject>FORGE FURNACES ; FORGING ; HAMMERING ; MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL ; PERFORMING OPERATIONS ; PRESSING METAL ; PUNCHING METAL ; RIVETING ; TRANSPORTING</subject><creationdate>2022</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=20220401&amp;DB=EPODOC&amp;CC=CN&amp;NR=114260401A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220401&amp;DB=EPODOC&amp;CC=CN&amp;NR=114260401A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MO ANJUN</creatorcontrib><creatorcontrib>LI WENQIANG</creatorcontrib><creatorcontrib>XIONG YUNSEN</creatorcontrib><creatorcontrib>GONG BIN</creatorcontrib><creatorcontrib>ZENG JING</creatorcontrib><creatorcontrib>MIN WU</creatorcontrib><creatorcontrib>WEI MINGGANG</creatorcontrib><creatorcontrib>LEI JIAFENG</creatorcontrib><creatorcontrib>YU SHENGFENG</creatorcontrib><title>Integral die forging forming method for spherical shell of manned cabin of titanium alloy bathyscaph</title><description>The invention provides an integral die forging forming method for a spherical shell of a manned cabin of a titanium alloy bathyscaph. The integral die forging forming method comprises the steps that a forge piece drawing is designed; a bar is blanked, and the bar is subjected to multiple times of upsetting; the forging temperature is T beta-(30-50 DEG C), and the deformation amount is 30%-55%; the forging temperature is T beta + (5-30 DEG C), and the deformation amount is 20%-50%; the forging temperature is T beta-(30-50 DEG C), and the deformation is 10%-20%; and heat treatment. The bathyscaph manned cabin spherical shell with the three outlook holes is integrally formed in a die forging mode, welding seams are eliminated, the welding risk and the overall production cost are reduced, the connection strength between the outlook holes and the spherical shell is guaranteed, and weak links are prevented. 本发明提供了一种钛合金深潜器载人舱球壳整体模锻成形方法,包括设计锻件图;棒材下料,对棒材进行多次镦粗;第一火模锻,锻造温度Tβ-(30~50℃),变形量30%~55%;第二火模锻,锻造温度Tβ+(5~30℃),变形量2</description><subject>FORGE FURNACES</subject><subject>FORGING</subject><subject>HAMMERING</subject><subject>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</subject><subject>PERFORMING OPERATIONS</subject><subject>PRESSING METAL</subject><subject>PUNCHING METAL</subject><subject>RIVETING</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyjEKAjEQQNE0FqLeYTyAsNHFXhZFGyv7ZTaZbALJJCSx2NtrwANYPT78tdAPrjRn9KAdgYl5djw3QzNQtVG3hJIsZae-Y7HkPUQDAZlJg8LJcevqKrJ7B0Dv4wITVrsUhcluxcqgL7T7uRH72_U13A-U4kgloSKmOg5PKfvjues7eTn983wAyT0-nw</recordid><startdate>20220401</startdate><enddate>20220401</enddate><creator>MO ANJUN</creator><creator>LI WENQIANG</creator><creator>XIONG YUNSEN</creator><creator>GONG BIN</creator><creator>ZENG JING</creator><creator>MIN WU</creator><creator>WEI MINGGANG</creator><creator>LEI JIAFENG</creator><creator>YU SHENGFENG</creator><scope>EVB</scope></search><sort><creationdate>20220401</creationdate><title>Integral die forging forming method for spherical shell of manned cabin of titanium alloy bathyscaph</title><author>MO ANJUN ; LI WENQIANG ; XIONG YUNSEN ; GONG BIN ; ZENG JING ; MIN WU ; WEI MINGGANG ; LEI JIAFENG ; YU SHENGFENG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN114260401A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>FORGE FURNACES</topic><topic>FORGING</topic><topic>HAMMERING</topic><topic>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</topic><topic>PERFORMING OPERATIONS</topic><topic>PRESSING METAL</topic><topic>PUNCHING METAL</topic><topic>RIVETING</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>MO ANJUN</creatorcontrib><creatorcontrib>LI WENQIANG</creatorcontrib><creatorcontrib>XIONG YUNSEN</creatorcontrib><creatorcontrib>GONG BIN</creatorcontrib><creatorcontrib>ZENG JING</creatorcontrib><creatorcontrib>MIN WU</creatorcontrib><creatorcontrib>WEI MINGGANG</creatorcontrib><creatorcontrib>LEI JIAFENG</creatorcontrib><creatorcontrib>YU SHENGFENG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MO ANJUN</au><au>LI WENQIANG</au><au>XIONG YUNSEN</au><au>GONG BIN</au><au>ZENG JING</au><au>MIN WU</au><au>WEI MINGGANG</au><au>LEI JIAFENG</au><au>YU SHENGFENG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Integral die forging forming method for spherical shell of manned cabin of titanium alloy bathyscaph</title><date>2022-04-01</date><risdate>2022</risdate><abstract>The invention provides an integral die forging forming method for a spherical shell of a manned cabin of a titanium alloy bathyscaph. The integral die forging forming method comprises the steps that a forge piece drawing is designed; a bar is blanked, and the bar is subjected to multiple times of upsetting; the forging temperature is T beta-(30-50 DEG C), and the deformation amount is 30%-55%; the forging temperature is T beta + (5-30 DEG C), and the deformation amount is 20%-50%; the forging temperature is T beta-(30-50 DEG C), and the deformation is 10%-20%; and heat treatment. The bathyscaph manned cabin spherical shell with the three outlook holes is integrally formed in a die forging mode, welding seams are eliminated, the welding risk and the overall production cost are reduced, the connection strength between the outlook holes and the spherical shell is guaranteed, and weak links are prevented. 本发明提供了一种钛合金深潜器载人舱球壳整体模锻成形方法,包括设计锻件图;棒材下料,对棒材进行多次镦粗;第一火模锻,锻造温度Tβ-(30~50℃),变形量30%~55%;第二火模锻,锻造温度Tβ+(5~30℃),变形量2</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN114260401A
source esp@cenet
subjects FORGE FURNACES
FORGING
HAMMERING
MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL
PERFORMING OPERATIONS
PRESSING METAL
PUNCHING METAL
RIVETING
TRANSPORTING
title Integral die forging forming method for spherical shell of manned cabin of titanium alloy bathyscaph
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-04T19%3A09%3A29IST&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=MO%20ANJUN&rft.date=2022-04-01&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN114260401A%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