Assembly for turbomachine including nozzle supported by annular member
The invention relates to an assembly for a turbomachine having a longitudinal axis (X), comprising a nozzle (40) carried by an annular part (30) fixed to an outer housing (20), the nozzle (40) comprising an outer annular platform (42), a radial annular wall (44) extends radially outward from the out...
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 | BAUMAS OLIVIER JEAN-DANIEL BEGUIN, ANSON, PIERRE DELABORTE, NICOLAS, DANIEL |
| description | The invention relates to an assembly for a turbomachine having a longitudinal axis (X), comprising a nozzle (40) carried by an annular part (30) fixed to an outer housing (20), the nozzle (40) comprising an outer annular platform (42), a radial annular wall (44) extends radially outward from the outer annular platform and carries an annular attachment lug (45) extending longitudinally upstream from the radial annular wall (44), the assembly comprising a cooling circuit comprising: an inner annular chamber (61) defined radially by the outer annular platform (42) and the annular member (30) and defined downstream by the radial annular wall (44); an intermediate annular chamber (62) formed radially outside the annular attachment lug (45) and in fluid communication with the outer housing (20); and a fluid communication member between the inner annular chamber (61) and the intermediate annular chamber (62), said member being formed in an annular attachment lug (45) of said nozzle (40).
本发明涉及用于具有纵向轴线(X)的涡轮机的组合件，所述组 |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN118510979A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN118510979A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN118510979A3</originalsourceid><addsrcrecordid>eNrjZHBzLC5OzU3KqVRIyy9SKCktSsrPTUzOyMxLVcjMS84pTcnMS1fIy6-qyklVKC4tKMgvKklNUUiqVEjMyyvNSSxSyAXqTi3iYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhhamhgaW5paOxsSoAQCGczRQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Assembly for turbomachine including nozzle supported by annular member</title><source>esp@cenet</source><creator>BAUMAS OLIVIER JEAN-DANIEL ; BEGUIN, ANSON, PIERRE ; DELABORTE, NICOLAS, DANIEL</creator><creatorcontrib>BAUMAS OLIVIER JEAN-DANIEL ; BEGUIN, ANSON, PIERRE ; DELABORTE, NICOLAS, DANIEL</creatorcontrib><description>The invention relates to an assembly for a turbomachine having a longitudinal axis (X), comprising a nozzle (40) carried by an annular part (30) fixed to an outer housing (20), the nozzle (40) comprising an outer annular platform (42), a radial annular wall (44) extends radially outward from the outer annular platform and carries an annular attachment lug (45) extending longitudinally upstream from the radial annular wall (44), the assembly comprising a cooling circuit comprising: an inner annular chamber (61) defined radially by the outer annular platform (42) and the annular member (30) and defined downstream by the radial annular wall (44); an intermediate annular chamber (62) formed radially outside the annular attachment lug (45) and in fluid communication with the outer housing (20); and a fluid communication member between the inner annular chamber (61) and the intermediate annular chamber (62), said member being formed in an annular attachment lug (45) of said nozzle (40).
本发明涉及用于具有纵向轴线(X)的涡轮机的组合件，所述组</description><language>chi ; eng</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2024</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=20240816&DB=EPODOC&CC=CN&NR=118510979A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25555,76308</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240816&DB=EPODOC&CC=CN&NR=118510979A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BAUMAS OLIVIER JEAN-DANIEL</creatorcontrib><creatorcontrib>BEGUIN, ANSON, PIERRE</creatorcontrib><creatorcontrib>DELABORTE, NICOLAS, DANIEL</creatorcontrib><title>Assembly for turbomachine including nozzle supported by annular member</title><description>The invention relates to an assembly for a turbomachine having a longitudinal axis (X), comprising a nozzle (40) carried by an annular part (30) fixed to an outer housing (20), the nozzle (40) comprising an outer annular platform (42), a radial annular wall (44) extends radially outward from the outer annular platform and carries an annular attachment lug (45) extending longitudinally upstream from the radial annular wall (44), the assembly comprising a cooling circuit comprising: an inner annular chamber (61) defined radially by the outer annular platform (42) and the annular member (30) and defined downstream by the radial annular wall (44); an intermediate annular chamber (62) formed radially outside the annular attachment lug (45) and in fluid communication with the outer housing (20); and a fluid communication member between the inner annular chamber (61) and the intermediate annular chamber (62), said member being formed in an annular attachment lug (45) of said nozzle (40).
本发明涉及用于具有纵向轴线(X)的涡轮机的组合件，所述组</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHBzLC5OzU3KqVRIyy9SKCktSsrPTUzOyMxLVcjMS84pTcnMS1fIy6-qyklVKC4tKMgvKklNUUiqVEjMyyvNSSxSyAXqTi3iYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhhamhgaW5paOxsSoAQCGczRQ</recordid><startdate>20240816</startdate><enddate>20240816</enddate><creator>BAUMAS OLIVIER JEAN-DANIEL</creator><creator>BEGUIN, ANSON, PIERRE</creator><creator>DELABORTE, NICOLAS, DANIEL</creator><scope>EVB</scope></search><sort><creationdate>20240816</creationdate><title>Assembly for turbomachine including nozzle supported by annular member</title><author>BAUMAS OLIVIER JEAN-DANIEL ; BEGUIN, ANSON, PIERRE ; DELABORTE, NICOLAS, DANIEL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN118510979A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>BAUMAS OLIVIER JEAN-DANIEL</creatorcontrib><creatorcontrib>BEGUIN, ANSON, PIERRE</creatorcontrib><creatorcontrib>DELABORTE, NICOLAS, DANIEL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BAUMAS OLIVIER JEAN-DANIEL</au><au>BEGUIN, ANSON, PIERRE</au><au>DELABORTE, NICOLAS, DANIEL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Assembly for turbomachine including nozzle supported by annular member</title><date>2024-08-16</date><risdate>2024</risdate><abstract>The invention relates to an assembly for a turbomachine having a longitudinal axis (X), comprising a nozzle (40) carried by an annular part (30) fixed to an outer housing (20), the nozzle (40) comprising an outer annular platform (42), a radial annular wall (44) extends radially outward from the outer annular platform and carries an annular attachment lug (45) extending longitudinally upstream from the radial annular wall (44), the assembly comprising a cooling circuit comprising: an inner annular chamber (61) defined radially by the outer annular platform (42) and the annular member (30) and defined downstream by the radial annular wall (44); an intermediate annular chamber (62) formed radially outside the annular attachment lug (45) and in fluid communication with the outer housing (20); and a fluid communication member between the inner annular chamber (61) and the intermediate annular chamber (62), said member being formed in an annular attachment lug (45) of said nozzle (40).
本发明涉及用于具有纵向轴线(X)的涡轮机的组合件，所述组</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN118510979A |
| source | esp@cenet |
| subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | Assembly for turbomachine including nozzle supported by annular member |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-14T18%3A24%3A42IST&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=BAUMAS%20OLIVIER%20JEAN-DANIEL&rft.date=2024-08-16&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN118510979A%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 |