EP0564662
A method for controlling the boundary layer by suction of the air from vortex chambers provided in the aft part of the aerodynamic surface of the flying vehicle (FV), wherein the speed of the air suction is regulated being first increased until the boundary layer joins the streamlined surface and th...
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| creator | SCHUKIN LEV NIKOLAEVICH SHIBANOV ANATOLY PETROVICH SCHUKIN ILYA LVOVICH SAVITSKY ANATOLY IVANOVICH PUSHKIN ROSTISLAV MIKHAILOVICH MASS ALEXANDR MIKHAILOVICH FISCHENKO SERGEI VIKTOROVICH KARELIN VIKTOR GEORGIEVICH |
| description | A method for controlling the boundary layer by suction of the air from vortex chambers provided in the aft part of the aerodynamic surface of the flying vehicle (FV), wherein the speed of the air suction is regulated being first increased until the boundary layer joins the streamlined surface and then decreased until the pressure starts to drop at the aft part of the FV. An FV provided with a boundary layer control system comprising a number of vortex chambers (1) housing streamlined bodies (2) and connected by a common channel (9) through a receiver (8) to a low pressure source (4). |
| format | Patent |
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An FV provided with a boundary layer control system comprising a number of vortex chambers (1) housing streamlined bodies (2) and connected by a common channel (9) through a receiver (8) to a low pressure source (4).</description><edition>5</edition><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>1995</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=19950705&DB=EPODOC&CC=EP&NR=0564662A4$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19950705&DB=EPODOC&CC=EP&NR=0564662A4$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SCHUKIN LEV NIKOLAEVICH</creatorcontrib><creatorcontrib>SHIBANOV ANATOLY PETROVICH</creatorcontrib><creatorcontrib>SCHUKIN ILYA LVOVICH</creatorcontrib><creatorcontrib>SAVITSKY ANATOLY IVANOVICH</creatorcontrib><creatorcontrib>PUSHKIN ROSTISLAV MIKHAILOVICH</creatorcontrib><creatorcontrib>MASS ALEXANDR MIKHAILOVICH</creatorcontrib><creatorcontrib>FISCHENKO SERGEI VIKTOROVICH</creatorcontrib><creatorcontrib>KARELIN VIKTOR GEORGIEVICH</creatorcontrib><title>EP0564662</title><description>A method for controlling the boundary layer by suction of the air from vortex chambers provided in the aft part of the aerodynamic surface of the flying vehicle (FV), wherein the speed of the air suction is regulated being first increased until the boundary layer joins the streamlined surface and then decreased until the pressure starts to drop at the aft part of the FV. An FV provided with a boundary layer control system comprising a number of vortex chambers (1) housing streamlined bodies (2) and connected by a common channel (9) through a receiver (8) to a low pressure source (4).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1995</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZOB0DTAwNTMxMzPiYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxcPWOJsZEKAEA1Lkamg</recordid><startdate>19950705</startdate><enddate>19950705</enddate><creator>SCHUKIN LEV NIKOLAEVICH</creator><creator>SHIBANOV ANATOLY PETROVICH</creator><creator>SCHUKIN ILYA LVOVICH</creator><creator>SAVITSKY ANATOLY IVANOVICH</creator><creator>PUSHKIN ROSTISLAV MIKHAILOVICH</creator><creator>MASS ALEXANDR MIKHAILOVICH</creator><creator>FISCHENKO SERGEI VIKTOROVICH</creator><creator>KARELIN VIKTOR GEORGIEVICH</creator><scope>EVB</scope></search><sort><creationdate>19950705</creationdate><title>EP0564662</title><author>SCHUKIN LEV NIKOLAEVICH ; SHIBANOV ANATOLY PETROVICH ; SCHUKIN ILYA LVOVICH ; SAVITSKY ANATOLY IVANOVICH ; PUSHKIN ROSTISLAV MIKHAILOVICH ; MASS ALEXANDR MIKHAILOVICH ; FISCHENKO SERGEI VIKTOROVICH ; KARELIN VIKTOR GEORGIEVICH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP0564662A43</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1995</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>SCHUKIN LEV NIKOLAEVICH</creatorcontrib><creatorcontrib>SHIBANOV ANATOLY PETROVICH</creatorcontrib><creatorcontrib>SCHUKIN ILYA LVOVICH</creatorcontrib><creatorcontrib>SAVITSKY ANATOLY IVANOVICH</creatorcontrib><creatorcontrib>PUSHKIN ROSTISLAV MIKHAILOVICH</creatorcontrib><creatorcontrib>MASS ALEXANDR MIKHAILOVICH</creatorcontrib><creatorcontrib>FISCHENKO SERGEI VIKTOROVICH</creatorcontrib><creatorcontrib>KARELIN VIKTOR GEORGIEVICH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SCHUKIN LEV NIKOLAEVICH</au><au>SHIBANOV ANATOLY PETROVICH</au><au>SCHUKIN ILYA LVOVICH</au><au>SAVITSKY ANATOLY IVANOVICH</au><au>PUSHKIN ROSTISLAV MIKHAILOVICH</au><au>MASS ALEXANDR MIKHAILOVICH</au><au>FISCHENKO SERGEI VIKTOROVICH</au><au>KARELIN VIKTOR GEORGIEVICH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>EP0564662</title><date>1995-07-05</date><risdate>1995</risdate><abstract>A method for controlling the boundary layer by suction of the air from vortex chambers provided in the aft part of the aerodynamic surface of the flying vehicle (FV), wherein the speed of the air suction is regulated being first increased until the boundary layer joins the streamlined surface and then decreased until the pressure starts to drop at the aft part of the FV. An FV provided with a boundary layer control system comprising a number of vortex chambers (1) housing streamlined bodies (2) and connected by a common channel (9) through a receiver (8) to a low pressure source (4).</abstract><edition>5</edition><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | EP0564662 |
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