Structure property regulation and control process for Ti2AlNb aero-engine case part
The invention discloses a structure property regulation and control process for Ti2AlNb aero-engine case parts, and belongs to the field of material heat treatment. The diameter size of the Ti2AlNb aero-engine case type part is generally not less than 500mm, the overall heat treatment of the Ti2AlNb...
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 | ZHU XUHUI WU JIE XU LEI LU ZHENGGUAN YANG RUI |
| description | The invention discloses a structure property regulation and control process for Ti2AlNb aero-engine case parts, and belongs to the field of material heat treatment. The diameter size of the Ti2AlNb aero-engine case type part is generally not less than 500mm, the overall heat treatment of the Ti2AlNb aero-engine case type part can be realized by adopting the process, the case type part is put into a heat treatment furnace, the temperature of the part is increased to T1 along with the furnace, heat preservation is performed for a period of time, heating is stopped, and the part is cooled to room temperature and discharged out of the furnace; and then heat treatment at T2 temperature is carried out, so that the structure is more uniform, and the performance is more stable. According to the method, the mechanical property of the Ti2AlNb aero-engine case part can be improved, and the structure is more uniform.
本发明公开了一种Ti2AlNb航空发动机机匣类零件的组织性能调控工艺，属于材料热处理领域。Ti2AlNb航空发动机机匣类零件的直径尺寸一般不低于500mm，采用该工艺能够实现Ti2AlNb航空发动机机匣类零件的 |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN116065110A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN116065110A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN116065110A3</originalsourceid><addsrcrecordid>eNqNjDEKwkAQANNYiPqH9QGBnGL6EBSrNEkf1nMTDo7dY2-v8Pcq-ACrKWaYbTWOpsVbUYKkkkjtBUpriWhBGJCf4IVNJX69p5xhEYUpnLo4PABJpSZeAxN4zJ8Jqu2rzYIx0-HHXXW8Xaf-XlOSmXJCT0w294NzbdNenGu68z_NG3q0OFc</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Structure property regulation and control process for Ti2AlNb aero-engine case part</title><source>esp@cenet</source><creator>ZHU XUHUI ; WU JIE ; XU LEI ; LU ZHENGGUAN ; YANG RUI</creator><creatorcontrib>ZHU XUHUI ; WU JIE ; XU LEI ; LU ZHENGGUAN ; YANG RUI</creatorcontrib><description>The invention discloses a structure property regulation and control process for Ti2AlNb aero-engine case parts, and belongs to the field of material heat treatment. The diameter size of the Ti2AlNb aero-engine case type part is generally not less than 500mm, the overall heat treatment of the Ti2AlNb aero-engine case type part can be realized by adopting the process, the case type part is put into a heat treatment furnace, the temperature of the part is increased to T1 along with the furnace, heat preservation is performed for a period of time, heating is stopped, and the part is cooled to room temperature and discharged out of the furnace; and then heat treatment at T2 temperature is carried out, so that the structure is more uniform, and the performance is more stable. According to the method, the mechanical property of the Ti2AlNb aero-engine case part can be improved, and the structure is more uniform.
本发明公开了一种Ti2AlNb航空发动机机匣类零件的组织性能调控工艺，属于材料热处理领域。Ti2AlNb航空发动机机匣类零件的直径尺寸一般不低于500mm，采用该工艺能够实现Ti2AlNb航空发动机机匣类零件的</description><language>chi ; eng</language><subject>CASTING ; CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS ; 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 ; MAKING METALLIC POWDER ; MANUFACTURE OF ARTICLES FROM METALLIC POWDER ; MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL ; METALLURGY ; METALLURGY OF IRON ; MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS ; PERFORMING OPERATIONS ; POWDER METALLURGY ; PUNCHING METAL ; ROLLING OF METAL ; TRANSPORTING ; TREATMENT OF ALLOYS OR NON-FERROUS METALS ; WORKING METALLIC POWDER</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=20230505&DB=EPODOC&CC=CN&NR=116065110A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230505&DB=EPODOC&CC=CN&NR=116065110A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ZHU XUHUI</creatorcontrib><creatorcontrib>WU JIE</creatorcontrib><creatorcontrib>XU LEI</creatorcontrib><creatorcontrib>LU ZHENGGUAN</creatorcontrib><creatorcontrib>YANG RUI</creatorcontrib><title>Structure property regulation and control process for Ti2AlNb aero-engine case part</title><description>The invention discloses a structure property regulation and control process for Ti2AlNb aero-engine case parts, and belongs to the field of material heat treatment. The diameter size of the Ti2AlNb aero-engine case type part is generally not less than 500mm, the overall heat treatment of the Ti2AlNb aero-engine case type part can be realized by adopting the process, the case type part is put into a heat treatment furnace, the temperature of the part is increased to T1 along with the furnace, heat preservation is performed for a period of time, heating is stopped, and the part is cooled to room temperature and discharged out of the furnace; and then heat treatment at T2 temperature is carried out, so that the structure is more uniform, and the performance is more stable. According to the method, the mechanical property of the Ti2AlNb aero-engine case part can be improved, and the structure is more uniform.
本发明公开了一种Ti2AlNb航空发动机机匣类零件的组织性能调控工艺，属于材料热处理领域。Ti2AlNb航空发动机机匣类零件的直径尺寸一般不低于500mm，采用该工艺能够实现Ti2AlNb航空发动机机匣类零件的</description><subject>CASTING</subject><subject>CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS</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>MAKING METALLIC POWDER</subject><subject>MANUFACTURE OF ARTICLES FROM METALLIC POWDER</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>POWDER METALLURGY</subject><subject>PUNCHING METAL</subject><subject>ROLLING OF METAL</subject><subject>TRANSPORTING</subject><subject>TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><subject>WORKING METALLIC POWDER</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjDEKwkAQANNYiPqH9QGBnGL6EBSrNEkf1nMTDo7dY2-v8Pcq-ACrKWaYbTWOpsVbUYKkkkjtBUpriWhBGJCf4IVNJX69p5xhEYUpnLo4PABJpSZeAxN4zJ8Jqu2rzYIx0-HHXXW8Xaf-XlOSmXJCT0w294NzbdNenGu68z_NG3q0OFc</recordid><startdate>20230505</startdate><enddate>20230505</enddate><creator>ZHU XUHUI</creator><creator>WU JIE</creator><creator>XU LEI</creator><creator>LU ZHENGGUAN</creator><creator>YANG RUI</creator><scope>EVB</scope></search><sort><creationdate>20230505</creationdate><title>Structure property regulation and control process for Ti2AlNb aero-engine case part</title><author>ZHU XUHUI ; WU JIE ; XU LEI ; LU ZHENGGUAN ; YANG RUI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116065110A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>CASTING</topic><topic>CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS</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>MAKING METALLIC POWDER</topic><topic>MANUFACTURE OF ARTICLES FROM METALLIC POWDER</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>POWDER METALLURGY</topic><topic>PUNCHING METAL</topic><topic>ROLLING OF METAL</topic><topic>TRANSPORTING</topic><topic>TREATMENT OF ALLOYS OR NON-FERROUS METALS</topic><topic>WORKING METALLIC POWDER</topic><toplevel>online_resources</toplevel><creatorcontrib>ZHU XUHUI</creatorcontrib><creatorcontrib>WU JIE</creatorcontrib><creatorcontrib>XU LEI</creatorcontrib><creatorcontrib>LU ZHENGGUAN</creatorcontrib><creatorcontrib>YANG RUI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHU XUHUI</au><au>WU JIE</au><au>XU LEI</au><au>LU ZHENGGUAN</au><au>YANG RUI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Structure property regulation and control process for Ti2AlNb aero-engine case part</title><date>2023-05-05</date><risdate>2023</risdate><abstract>The invention discloses a structure property regulation and control process for Ti2AlNb aero-engine case parts, and belongs to the field of material heat treatment. The diameter size of the Ti2AlNb aero-engine case type part is generally not less than 500mm, the overall heat treatment of the Ti2AlNb aero-engine case type part can be realized by adopting the process, the case type part is put into a heat treatment furnace, the temperature of the part is increased to T1 along with the furnace, heat preservation is performed for a period of time, heating is stopped, and the part is cooled to room temperature and discharged out of the furnace; and then heat treatment at T2 temperature is carried out, so that the structure is more uniform, and the performance is more stable. According to the method, the mechanical property of the Ti2AlNb aero-engine case part can be improved, and the structure is more uniform.
本发明公开了一种Ti2AlNb航空发动机机匣类零件的组织性能调控工艺，属于材料热处理领域。Ti2AlNb航空发动机机匣类零件的直径尺寸一般不低于500mm，采用该工艺能够实现Ti2AlNb航空发动机机匣类零件的</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN116065110A |
| source | esp@cenet |
| subjects | CASTING CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS 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 MAKING METALLIC POWDER MANUFACTURE OF ARTICLES FROM METALLIC POWDER MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL METALLURGY METALLURGY OF IRON MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS PERFORMING OPERATIONS POWDER METALLURGY PUNCHING METAL ROLLING OF METAL TRANSPORTING TREATMENT OF ALLOYS OR NON-FERROUS METALS WORKING METALLIC POWDER |
| title | Structure property regulation and control process for Ti2AlNb aero-engine case part |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-25T01%3A38%3A41IST&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=ZHU%20XUHUI&rft.date=2023-05-05&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN116065110A%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 |