A MULTI-CONTOUR DUCT
Disclosed is a multi-contour duct (100) including a front part (102) configured to entrain ambient air, an intermediate part (104) configured to convert the pressure head into the velocity head for the entrained air and a rear part (106) configured to egress the entrained air with converted velocity...
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| creator | VIKRAMAN, Vinayan FRANCIS, Nivin SUDIL, Advaith S ELAYATH, Balachandran S AFEENA K F, Mary S G, Silpa |
| description | Disclosed is a multi-contour duct (100) including a front part (102) configured to entrain ambient air, an intermediate part (104) configured to convert the pressure head into the velocity head for the entrained air and a rear part (106) configured to egress the entrained air with converted velocity head exhibiting a greater exit velocity of the air than the velocity of the air entering into the multi-contour duct (100).
L'invention concerne un conduit multi-contour (100) comprenant une partie avant (102) conçue pour entraîner l'air ambiant, une partie intermédiaire (104) conçue pour convertir la hauteur de pression en charge dynamique pour l'air entraîné et une partie arrière (106) conçue pour évacuer l'air entraîné avec la charge dynamique issue de la conversion présentant une vitesse de sortie plus grande de l'air que la vitesse de l'air entrant dans le conduit multi-contour (100). |
| format | Patent |
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L'invention concerne un conduit multi-contour (100) comprenant une partie avant (102) conçue pour entraîner l'air ambiant, une partie intermédiaire (104) conçue pour convertir la hauteur de pression en charge dynamique pour l'air entraîné et une partie arrière (106) conçue pour évacuer l'air entraîné avec la charge dynamique issue de la conversion présentant une vitesse de sortie plus grande de l'air que la vitesse de l'air entrant dans le conduit multi-contour (100).</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2022</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=20220527&DB=EPODOC&CC=WO&NR=2022107172A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220527&DB=EPODOC&CC=WO&NR=2022107172A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>VIKRAMAN, Vinayan</creatorcontrib><creatorcontrib>FRANCIS, Nivin</creatorcontrib><creatorcontrib>SUDIL, Advaith S</creatorcontrib><creatorcontrib>ELAYATH, Balachandran S</creatorcontrib><creatorcontrib>AFEENA K F, Mary</creatorcontrib><creatorcontrib>S G, Silpa</creatorcontrib><title>A MULTI-CONTOUR DUCT</title><description>Disclosed is a multi-contour duct (100) including a front part (102) configured to entrain ambient air, an intermediate part (104) configured to convert the pressure head into the velocity head for the entrained air and a rear part (106) configured to egress the entrained air with converted velocity head exhibiting a greater exit velocity of the air than the velocity of the air entering into the multi-contour duct (100).
L'invention concerne un conduit multi-contour (100) comprenant une partie avant (102) conçue pour entraîner l'air ambiant, une partie intermédiaire (104) conçue pour convertir la hauteur de pression en charge dynamique pour l'air entraîné et une partie arrière (106) conçue pour évacuer l'air entraîné avec la charge dynamique issue de la conversion présentant une vitesse de sortie plus grande de l'air que la vitesse de l'air entrant dans le conduit multi-contour (100).</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBBxVPAN9Qnx1HX29wvxDw1ScAl1DuFhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfHh_kYGRkaGBuaG5kaOhsbEqQIA7T0fbg</recordid><startdate>20220527</startdate><enddate>20220527</enddate><creator>VIKRAMAN, Vinayan</creator><creator>FRANCIS, Nivin</creator><creator>SUDIL, Advaith S</creator><creator>ELAYATH, Balachandran S</creator><creator>AFEENA K F, Mary</creator><creator>S G, Silpa</creator><scope>EVB</scope></search><sort><creationdate>20220527</creationdate><title>A MULTI-CONTOUR DUCT</title><author>VIKRAMAN, Vinayan ; FRANCIS, Nivin ; SUDIL, Advaith S ; ELAYATH, Balachandran S ; AFEENA K F, Mary ; S G, Silpa</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2022107172A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2022</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>VIKRAMAN, Vinayan</creatorcontrib><creatorcontrib>FRANCIS, Nivin</creatorcontrib><creatorcontrib>SUDIL, Advaith S</creatorcontrib><creatorcontrib>ELAYATH, Balachandran S</creatorcontrib><creatorcontrib>AFEENA K F, Mary</creatorcontrib><creatorcontrib>S G, Silpa</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>VIKRAMAN, Vinayan</au><au>FRANCIS, Nivin</au><au>SUDIL, Advaith S</au><au>ELAYATH, Balachandran S</au><au>AFEENA K F, Mary</au><au>S G, Silpa</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>A MULTI-CONTOUR DUCT</title><date>2022-05-27</date><risdate>2022</risdate><abstract>Disclosed is a multi-contour duct (100) including a front part (102) configured to entrain ambient air, an intermediate part (104) configured to convert the pressure head into the velocity head for the entrained air and a rear part (106) configured to egress the entrained air with converted velocity head exhibiting a greater exit velocity of the air than the velocity of the air entering into the multi-contour duct (100).
L'invention concerne un conduit multi-contour (100) comprenant une partie avant (102) conçue pour entraîner l'air ambiant, une partie intermédiaire (104) conçue pour convertir la hauteur de pression en charge dynamique pour l'air entraîné et une partie arrière (106) conçue pour évacuer l'air entraîné avec la charge dynamique issue de la conversion présentant une vitesse de sortie plus grande de l'air que la vitesse de l'air entrant dans le conduit multi-contour (100).</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS |
| title | A MULTI-CONTOUR DUCT |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-27T12%3A51%3A41IST&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=VIKRAMAN,%20Vinayan&rft.date=2022-05-27&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EWO2022107172A1%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 |