TURBINE ROTOR COMPRISING VENTILATION SPACER
The invention relates to a rotor (3) of a member (7) of a turbomachine (1), for example a rotor of a turbine (7), said rotor (3) comprising: a first element (30), a second element (20) defining with the first element a ventilation cavity (9), the rotor (3) being characterized in that it further comp...
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| creator | OUDIN BENJAMIN CYRILLE JACQUES CASALIGGI PASCAL CAPOLUNGO THIERRY LAURENT PASQUIET DIDIER DESIRE RENE |
| description | The invention relates to a rotor (3) of a member (7) of a turbomachine (1), for example a rotor of a turbine (7), said rotor (3) comprising: a first element (30), a second element (20) defining with the first element a ventilation cavity (9), the rotor (3) being characterized in that it further comprises a spacer (40) that is introduced and secured between the first element (30) and the second element (20) and that comprises a row of through-passages (42) that are configured to permit injection of cooling fluid (F) into the ventilation cavity (9).
本发明涉及涡轮机(1)的构件(7)的转子(3)，例如涡轮(7)的转子，所述转子(3)包括：-第元件(30)，-第二元件(20)，所述第二元件与所述第元件起限定出通风腔(9)，所述转子(3)的特征在于，所述转子进步包括间隔件(40)，所述间隔件被引到并固定在第元件(30)和第二元件(20)之间，并且包括排贯通通道(42)，所述贯通通道被构造成允许冷却流体(F)注入到所述通风腔(9)中。 |
| format | Patent |
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本发明涉及涡轮机(1)的构件(7)的转子(3)，例如涡轮(7)的转子，所述转子(3)包括：-第元件(30)，-第二元件(20)，所述第二元件与所述第元件起限定出通风腔(9)，所述转子(3)的特征在于，所述转子进步包括间隔件(40)，所述间隔件被引到并固定在第元件(30)和第二元件(20)之间，并且包括排贯通通道(42)，所述贯通通道被构造成允许冷却流体(F)注入到所述通风腔(9)中。</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>2018</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=20181123&DB=EPODOC&CC=CN&NR=108884714A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20181123&DB=EPODOC&CC=CN&NR=108884714A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>OUDIN BENJAMIN CYRILLE JACQUES</creatorcontrib><creatorcontrib>CASALIGGI PASCAL</creatorcontrib><creatorcontrib>CAPOLUNGO THIERRY LAURENT</creatorcontrib><creatorcontrib>PASQUIET DIDIER DESIRE RENE</creatorcontrib><title>TURBINE ROTOR COMPRISING VENTILATION SPACER</title><description>The invention relates to a rotor (3) of a member (7) of a turbomachine (1), for example a rotor of a turbine (7), said rotor (3) comprising: a first element (30), a second element (20) defining with the first element a ventilation cavity (9), the rotor (3) being characterized in that it further comprises a spacer (40) that is introduced and secured between the first element (30) and the second element (20) and that comprises a row of through-passages (42) that are configured to permit injection of cooling fluid (F) into the ventilation cavity (9).
本发明涉及涡轮机(1)的构件(7)的转子(3)，例如涡轮(7)的转子，所述转子(3)包括：-第元件(30)，-第二元件(20)，所述第二元件与所述第元件起限定出通风腔(9)，所述转子(3)的特征在于，所述转子进步包括间隔件(40)，所述间隔件被引到并固定在第元件(30)和第二元件(20)之间，并且包括排贯通通道(42)，所述贯通通道被构造成允许冷却流体(F)注入到所述通风腔(9)中。</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAOCQ1y8vRzVQjyD_EPUnD29w0I8gz29HNXCHP1C_H0cQzx9PdTCA5wdHYN4mFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hgYWFhYm5oYmjsbEqAEAoPslWQ</recordid><startdate>20181123</startdate><enddate>20181123</enddate><creator>OUDIN BENJAMIN CYRILLE JACQUES</creator><creator>CASALIGGI PASCAL</creator><creator>CAPOLUNGO THIERRY LAURENT</creator><creator>PASQUIET DIDIER DESIRE RENE</creator><scope>EVB</scope></search><sort><creationdate>20181123</creationdate><title>TURBINE ROTOR COMPRISING VENTILATION SPACER</title><author>OUDIN BENJAMIN CYRILLE JACQUES ; CASALIGGI PASCAL ; CAPOLUNGO THIERRY LAURENT ; PASQUIET DIDIER DESIRE RENE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN108884714A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2018</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>OUDIN BENJAMIN CYRILLE JACQUES</creatorcontrib><creatorcontrib>CASALIGGI PASCAL</creatorcontrib><creatorcontrib>CAPOLUNGO THIERRY LAURENT</creatorcontrib><creatorcontrib>PASQUIET DIDIER DESIRE RENE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>OUDIN BENJAMIN CYRILLE JACQUES</au><au>CASALIGGI PASCAL</au><au>CAPOLUNGO THIERRY LAURENT</au><au>PASQUIET DIDIER DESIRE RENE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBINE ROTOR COMPRISING VENTILATION SPACER</title><date>2018-11-23</date><risdate>2018</risdate><abstract>The invention relates to a rotor (3) of a member (7) of a turbomachine (1), for example a rotor of a turbine (7), said rotor (3) comprising: a first element (30), a second element (20) defining with the first element a ventilation cavity (9), the rotor (3) being characterized in that it further comprises a spacer (40) that is introduced and secured between the first element (30) and the second element (20) and that comprises a row of through-passages (42) that are configured to permit injection of cooling fluid (F) into the ventilation cavity (9).
本发明涉及涡轮机(1)的构件(7)的转子(3)，例如涡轮(7)的转子，所述转子(3)包括：-第元件(30)，-第二元件(20)，所述第二元件与所述第元件起限定出通风腔(9)，所述转子(3)的特征在于，所述转子进步包括间隔件(40)，所述间隔件被引到并固定在第元件(30)和第二元件(20)之间，并且包括排贯通通道(42)，所述贯通通道被构造成允许冷却流体(F)注入到所述通风腔(9)中。</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| 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 | TURBINE ROTOR COMPRISING VENTILATION SPACER |
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