AIRCRAFT ENGINE FUEL CIRCUIT VALVE SLIDE
The present invention relates to a slide (22) for a fuel circuit valve (20) of an aircraft engine extending along a longitudinal axis (23), and comprising a narrowed intermediate portion (32) extending between two cylindrical end portions (29, 31), a first end portion (29) being separated from the n...
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 | PORA LOIC CEBILLE CHRISTOPHE BERNARD CLEMENT |
| description | The present invention relates to a slide (22) for a fuel circuit valve (20) of an aircraft engine extending along a longitudinal axis (23), and comprising a narrowed intermediate portion (32) extending between two cylindrical end portions (29, 31), a first end portion (29) being separated from the narrowed intermediate portion (32) by a shoulder (36) having a surface (37) arranged overall perpendicular to the longitudinal axis (23), the narrowed intermediate portion (32) including in turn, as an extension of the shoulder (36), at least one cylindrical portion (34), the shoulder (36) comprisingat least one groove (38) which extends radially from the cylindrical surface (30) of the first end portion (29), towards the longitudinal axis (23), and which forms a fuel recirculation area (40) which provides the generation of a jet of fuel on the cylindrical portion (34) of the narrowed intermediate portion (32), when fuel flows along the first end portion (29) towards the narrowed intermediate portion (32) and the se |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN109073100A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN109073100A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN109073100A3</originalsourceid><addsrcrecordid>eNrjZNBw9AxyDnJ0C1Fw9XP39HNVcAt19VFwBgqGeoYohDn6hLkqBPt4urjyMLCmJeYUp_JCaW4GRTfXEGcP3dSC_PjU4oLE5NS81JJ4Zz9DA0sDc2NDAwNHY2LUAADvyCPJ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AIRCRAFT ENGINE FUEL CIRCUIT VALVE SLIDE</title><source>esp@cenet</source><creator>PORA LOIC ; CEBILLE CHRISTOPHE ; BERNARD CLEMENT</creator><creatorcontrib>PORA LOIC ; CEBILLE CHRISTOPHE ; BERNARD CLEMENT</creatorcontrib><description>The present invention relates to a slide (22) for a fuel circuit valve (20) of an aircraft engine extending along a longitudinal axis (23), and comprising a narrowed intermediate portion (32) extending between two cylindrical end portions (29, 31), a first end portion (29) being separated from the narrowed intermediate portion (32) by a shoulder (36) having a surface (37) arranged overall perpendicular to the longitudinal axis (23), the narrowed intermediate portion (32) including in turn, as an extension of the shoulder (36), at least one cylindrical portion (34), the shoulder (36) comprisingat least one groove (38) which extends radially from the cylindrical surface (30) of the first end portion (29), towards the longitudinal axis (23), and which forms a fuel recirculation area (40) which provides the generation of a jet of fuel on the cylindrical portion (34) of the narrowed intermediate portion (32), when fuel flows along the first end portion (29) towards the narrowed intermediate portion (32) and the se</description><language>chi ; eng</language><subject>ACTUATING-FLOATS ; BLASTING ; COCKS ; DEVICES FOR VENTING OR AERATING ; ENGINEERING ELEMENTS AND UNITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; TAPS ; THERMAL INSULATION IN GENERAL ; VALVES ; 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=20181221&DB=EPODOC&CC=CN&NR=109073100A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20181221&DB=EPODOC&CC=CN&NR=109073100A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PORA LOIC</creatorcontrib><creatorcontrib>CEBILLE CHRISTOPHE</creatorcontrib><creatorcontrib>BERNARD CLEMENT</creatorcontrib><title>AIRCRAFT ENGINE FUEL CIRCUIT VALVE SLIDE</title><description>The present invention relates to a slide (22) for a fuel circuit valve (20) of an aircraft engine extending along a longitudinal axis (23), and comprising a narrowed intermediate portion (32) extending between two cylindrical end portions (29, 31), a first end portion (29) being separated from the narrowed intermediate portion (32) by a shoulder (36) having a surface (37) arranged overall perpendicular to the longitudinal axis (23), the narrowed intermediate portion (32) including in turn, as an extension of the shoulder (36), at least one cylindrical portion (34), the shoulder (36) comprisingat least one groove (38) which extends radially from the cylindrical surface (30) of the first end portion (29), towards the longitudinal axis (23), and which forms a fuel recirculation area (40) which provides the generation of a jet of fuel on the cylindrical portion (34) of the narrowed intermediate portion (32), when fuel flows along the first end portion (29) towards the narrowed intermediate portion (32) and the se</description><subject>ACTUATING-FLOATS</subject><subject>BLASTING</subject><subject>COCKS</subject><subject>DEVICES FOR VENTING OR AERATING</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>TAPS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>VALVES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNBw9AxyDnJ0C1Fw9XP39HNVcAt19VFwBgqGeoYohDn6hLkqBPt4urjyMLCmJeYUp_JCaW4GRTfXEGcP3dSC_PjU4oLE5NS81JJ4Zz9DA0sDc2NDAwNHY2LUAADvyCPJ</recordid><startdate>20181221</startdate><enddate>20181221</enddate><creator>PORA LOIC</creator><creator>CEBILLE CHRISTOPHE</creator><creator>BERNARD CLEMENT</creator><scope>EVB</scope></search><sort><creationdate>20181221</creationdate><title>AIRCRAFT ENGINE FUEL CIRCUIT VALVE SLIDE</title><author>PORA LOIC ; CEBILLE CHRISTOPHE ; BERNARD CLEMENT</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN109073100A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2018</creationdate><topic>ACTUATING-FLOATS</topic><topic>BLASTING</topic><topic>COCKS</topic><topic>DEVICES FOR VENTING OR AERATING</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>TAPS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>VALVES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>PORA LOIC</creatorcontrib><creatorcontrib>CEBILLE CHRISTOPHE</creatorcontrib><creatorcontrib>BERNARD CLEMENT</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PORA LOIC</au><au>CEBILLE CHRISTOPHE</au><au>BERNARD CLEMENT</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT ENGINE FUEL CIRCUIT VALVE SLIDE</title><date>2018-12-21</date><risdate>2018</risdate><abstract>The present invention relates to a slide (22) for a fuel circuit valve (20) of an aircraft engine extending along a longitudinal axis (23), and comprising a narrowed intermediate portion (32) extending between two cylindrical end portions (29, 31), a first end portion (29) being separated from the narrowed intermediate portion (32) by a shoulder (36) having a surface (37) arranged overall perpendicular to the longitudinal axis (23), the narrowed intermediate portion (32) including in turn, as an extension of the shoulder (36), at least one cylindrical portion (34), the shoulder (36) comprisingat least one groove (38) which extends radially from the cylindrical surface (30) of the first end portion (29), towards the longitudinal axis (23), and which forms a fuel recirculation area (40) which provides the generation of a jet of fuel on the cylindrical portion (34) of the narrowed intermediate portion (32), when fuel flows along the first end portion (29) towards the narrowed intermediate portion (32) and the se</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN109073100A |
| source | esp@cenet |
| subjects | ACTUATING-FLOATS BLASTING COCKS DEVICES FOR VENTING OR AERATING ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING TAPS THERMAL INSULATION IN GENERAL VALVES WEAPONS |
| title | AIRCRAFT ENGINE FUEL CIRCUIT VALVE SLIDE |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-08T01%3A37%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=PORA%20LOIC&rft.date=2018-12-21&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN109073100A%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 |