ASYMMETRIC FLOW EXTRACTION SYSTEM
A system for asymmetric flow extraction is described and claimed, the system comprising a flow path (17), a bleed slot (219) in the flow path (17), a bleed cavity (200) for receiving at least a portion of the fluid extracted from the flow path (17) and a bleed passage (100) in flow communication wit...
Gespeichert in:
| Hauptverfasser: | , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre |
| 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 | KRAMMER, ERICH ALOIS KUMAR, MANISH KIRK, DAVID CORY KARAFILLIS, APOSTOLOS PAVLOS MURUGANATHAN, KALYANASUNDARAM RULLI, SAMUEL SLAVIK, DONALD CHARLES |
| description | A system for asymmetric flow extraction is described and claimed, the system comprising a flow path (17), a bleed slot (219) in the flow path (17), a bleed cavity (200) for receiving at least a portion of the fluid extracted from the flow path (17) and a bleed passage (100) in flow communication with the bleed slot (219) and the bleed cavity (200) wherein the bleed passage (100) has at least one deflector (151) having a shape such that the width of the bleed passage cross section varies in a direction normal to the direction of fluid flow in the bleed passage (100). In another embodiment, the deflector (151) has an aerodynamic surface (175) having a shape such that the flow passage between the aerodynamic surface (175) and a surface (505) located away from it has a cross sectional shape that is non-axisymmetric. In another embodiment, the bleed passage (100) comprises an assembly of a plurality deflectors (151), arranged circumferentially. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CA2641074C</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CA2641074C</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CA2641074C3</originalsourceid><addsrcrecordid>eNrjZFB0DI709XUNCfJ0VnDz8Q9XcI0ICXJ0DvH091MIjgwOcfXlYWBNS8wpTuWF0twM8m6uIc4euqkF-fGpxQWJyal5qSXxzo5GZiaGBuYmzsaEVQAAtV0hmg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>ASYMMETRIC FLOW EXTRACTION SYSTEM</title><source>esp@cenet</source><creator>KRAMMER, ERICH ALOIS ; KUMAR, MANISH ; KIRK, DAVID CORY ; KARAFILLIS, APOSTOLOS PAVLOS ; MURUGANATHAN, KALYANASUNDARAM ; RULLI, SAMUEL ; SLAVIK, DONALD CHARLES</creator><creatorcontrib>KRAMMER, ERICH ALOIS ; KUMAR, MANISH ; KIRK, DAVID CORY ; KARAFILLIS, APOSTOLOS PAVLOS ; MURUGANATHAN, KALYANASUNDARAM ; RULLI, SAMUEL ; SLAVIK, DONALD CHARLES</creatorcontrib><description>A system for asymmetric flow extraction is described and claimed, the system comprising a flow path (17), a bleed slot (219) in the flow path (17), a bleed cavity (200) for receiving at least a portion of the fluid extracted from the flow path (17) and a bleed passage (100) in flow communication with the bleed slot (219) and the bleed cavity (200) wherein the bleed passage (100) has at least one deflector (151) having a shape such that the width of the bleed passage cross section varies in a direction normal to the direction of fluid flow in the bleed passage (100). In another embodiment, the deflector (151) has an aerodynamic surface (175) having a shape such that the flow passage between the aerodynamic surface (175) and a surface (505) located away from it has a cross sectional shape that is non-axisymmetric. In another embodiment, the bleed passage (100) comprises an assembly of a plurality deflectors (151), arranged circumferentially.</description><language>eng ; fre</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2016</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=20161108&DB=EPODOC&CC=CA&NR=2641074C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25569,76552</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20161108&DB=EPODOC&CC=CA&NR=2641074C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KRAMMER, ERICH ALOIS</creatorcontrib><creatorcontrib>KUMAR, MANISH</creatorcontrib><creatorcontrib>KIRK, DAVID CORY</creatorcontrib><creatorcontrib>KARAFILLIS, APOSTOLOS PAVLOS</creatorcontrib><creatorcontrib>MURUGANATHAN, KALYANASUNDARAM</creatorcontrib><creatorcontrib>RULLI, SAMUEL</creatorcontrib><creatorcontrib>SLAVIK, DONALD CHARLES</creatorcontrib><title>ASYMMETRIC FLOW EXTRACTION SYSTEM</title><description>A system for asymmetric flow extraction is described and claimed, the system comprising a flow path (17), a bleed slot (219) in the flow path (17), a bleed cavity (200) for receiving at least a portion of the fluid extracted from the flow path (17) and a bleed passage (100) in flow communication with the bleed slot (219) and the bleed cavity (200) wherein the bleed passage (100) has at least one deflector (151) having a shape such that the width of the bleed passage cross section varies in a direction normal to the direction of fluid flow in the bleed passage (100). In another embodiment, the deflector (151) has an aerodynamic surface (175) having a shape such that the flow passage between the aerodynamic surface (175) and a surface (505) located away from it has a cross sectional shape that is non-axisymmetric. In another embodiment, the bleed passage (100) comprises an assembly of a plurality deflectors (151), arranged circumferentially.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB0DI709XUNCfJ0VnDz8Q9XcI0ICXJ0DvH091MIjgwOcfXlYWBNS8wpTuWF0twM8m6uIc4euqkF-fGpxQWJyal5qSXxzo5GZiaGBuYmzsaEVQAAtV0hmg</recordid><startdate>20161108</startdate><enddate>20161108</enddate><creator>KRAMMER, ERICH ALOIS</creator><creator>KUMAR, MANISH</creator><creator>KIRK, DAVID CORY</creator><creator>KARAFILLIS, APOSTOLOS PAVLOS</creator><creator>MURUGANATHAN, KALYANASUNDARAM</creator><creator>RULLI, SAMUEL</creator><creator>SLAVIK, DONALD CHARLES</creator><scope>EVB</scope></search><sort><creationdate>20161108</creationdate><title>ASYMMETRIC FLOW EXTRACTION SYSTEM</title><author>KRAMMER, ERICH ALOIS ; KUMAR, MANISH ; KIRK, DAVID CORY ; KARAFILLIS, APOSTOLOS PAVLOS ; MURUGANATHAN, KALYANASUNDARAM ; RULLI, SAMUEL ; SLAVIK, DONALD CHARLES</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2641074C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2016</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KRAMMER, ERICH ALOIS</creatorcontrib><creatorcontrib>KUMAR, MANISH</creatorcontrib><creatorcontrib>KIRK, DAVID CORY</creatorcontrib><creatorcontrib>KARAFILLIS, APOSTOLOS PAVLOS</creatorcontrib><creatorcontrib>MURUGANATHAN, KALYANASUNDARAM</creatorcontrib><creatorcontrib>RULLI, SAMUEL</creatorcontrib><creatorcontrib>SLAVIK, DONALD CHARLES</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KRAMMER, ERICH ALOIS</au><au>KUMAR, MANISH</au><au>KIRK, DAVID CORY</au><au>KARAFILLIS, APOSTOLOS PAVLOS</au><au>MURUGANATHAN, KALYANASUNDARAM</au><au>RULLI, SAMUEL</au><au>SLAVIK, DONALD CHARLES</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ASYMMETRIC FLOW EXTRACTION SYSTEM</title><date>2016-11-08</date><risdate>2016</risdate><abstract>A system for asymmetric flow extraction is described and claimed, the system comprising a flow path (17), a bleed slot (219) in the flow path (17), a bleed cavity (200) for receiving at least a portion of the fluid extracted from the flow path (17) and a bleed passage (100) in flow communication with the bleed slot (219) and the bleed cavity (200) wherein the bleed passage (100) has at least one deflector (151) having a shape such that the width of the bleed passage cross section varies in a direction normal to the direction of fluid flow in the bleed passage (100). In another embodiment, the deflector (151) has an aerodynamic surface (175) having a shape such that the flow passage between the aerodynamic surface (175) and a surface (505) located away from it has a cross sectional shape that is non-axisymmetric. In another embodiment, the bleed passage (100) comprises an assembly of a plurality deflectors (151), arranged circumferentially.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre |
| recordid | cdi_epo_espacenet_CA2641074C |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | ASYMMETRIC FLOW EXTRACTION SYSTEM |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-15T21%3A52%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=KRAMMER,%20ERICH%20ALOIS&rft.date=2016-11-08&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECA2641074C%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 |