PRESSURE INFLUENCING ASSEMBLY FOR AN AIRCRAFT AUXILIARY SYSTEM
An exemplary pressure influencing assembly for an aircraft auxiliary system an inlet opening to an aircraft auxiliary system and an exhaust opening from the aircraft auxiliary system. Both the inlet opening and the exhaust opening face at least partially radially away from an axis. At least some of...
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| creator | THAYALAKHANDAN, NAGAMANY HAGSHENAS, BEHZAD NAGER, ERIC ANDREW JONES, ANTHONY C |
| description | An exemplary pressure influencing assembly for an aircraft auxiliary system an inlet opening to an aircraft auxiliary system and an exhaust opening from the aircraft auxiliary system. Both the inlet opening and the exhaust opening face at least partially radially away from an axis. At least some of the inlet opening is circumferentially aligned with at least some of the exhaust opening relative to the axis.
Un ensemble de modification de pression exemplaire pour un système auxiliaire daéronef, un orifice dadmission menant à un système auxiliaire daéronef et un orifice dévacuation à partir du système auxiliaire daéronef. Lorifice dadmission et lorifice déchappement sont orientés au moins partiellement radialement à lopposé dun axe. Au moins une partie de lorifice dadmission est alignée circonférentiellement avec au moins une partie de lorifice dévacuation par rapport laxe. |
| format | Patent |
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Un ensemble de modification de pression exemplaire pour un système auxiliaire daéronef, un orifice dadmission menant à un système auxiliaire daéronef et un orifice dévacuation à partir du système auxiliaire daéronef. Lorifice dadmission et lorifice déchappement sont orientés au moins partiellement radialement à lopposé dun axe. Au moins une partie de lorifice dadmission est alignée circonférentiellement avec au moins une partie de lorifice dévacuation par rapport laxe.</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</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=20180522&DB=EPODOC&CC=CA&NR=2783036C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76418</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180522&DB=EPODOC&CC=CA&NR=2783036C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>THAYALAKHANDAN, NAGAMANY</creatorcontrib><creatorcontrib>HAGSHENAS, BEHZAD</creatorcontrib><creatorcontrib>NAGER, ERIC ANDREW</creatorcontrib><creatorcontrib>JONES, ANTHONY C</creatorcontrib><title>PRESSURE INFLUENCING ASSEMBLY FOR AN AIRCRAFT AUXILIARY SYSTEM</title><description>An exemplary pressure influencing assembly for an aircraft auxiliary system an inlet opening to an aircraft auxiliary system and an exhaust opening from the aircraft auxiliary system. Both the inlet opening and the exhaust opening face at least partially radially away from an axis. At least some of the inlet opening is circumferentially aligned with at least some of the exhaust opening relative to the axis.
Un ensemble de modification de pression exemplaire pour un système auxiliaire daéronef, un orifice dadmission menant à un système auxiliaire daéronef et un orifice dévacuation à partir du système auxiliaire daéronef. Lorifice dadmission et lorifice déchappement sont orientés au moins partiellement radialement à lopposé dun axe. Au moins une partie de lorifice dadmission est alignée circonférentiellement avec au moins une partie de lorifice dévacuation par rapport laxe.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLALCHINDg4NclXw9HPzCXX1c_b0c1dwDA529XXyiVRw8w9ScPRTcPQMcg5ydAtRcAyN8PTxdAyKVAiODA5x9eVhYE1LzClO5YXS3Azybq4hzh66qQX58anFBYnJqXmpJfHOjkbmFsYGxmbOxoRVAADbyimP</recordid><startdate>20180522</startdate><enddate>20180522</enddate><creator>THAYALAKHANDAN, NAGAMANY</creator><creator>HAGSHENAS, BEHZAD</creator><creator>NAGER, ERIC ANDREW</creator><creator>JONES, ANTHONY C</creator><scope>EVB</scope></search><sort><creationdate>20180522</creationdate><title>PRESSURE INFLUENCING ASSEMBLY FOR AN AIRCRAFT AUXILIARY SYSTEM</title><author>THAYALAKHANDAN, NAGAMANY ; HAGSHENAS, BEHZAD ; NAGER, ERIC ANDREW ; JONES, ANTHONY C</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2783036C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2018</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>THAYALAKHANDAN, NAGAMANY</creatorcontrib><creatorcontrib>HAGSHENAS, BEHZAD</creatorcontrib><creatorcontrib>NAGER, ERIC ANDREW</creatorcontrib><creatorcontrib>JONES, ANTHONY C</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>THAYALAKHANDAN, NAGAMANY</au><au>HAGSHENAS, BEHZAD</au><au>NAGER, ERIC ANDREW</au><au>JONES, ANTHONY C</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PRESSURE INFLUENCING ASSEMBLY FOR AN AIRCRAFT AUXILIARY SYSTEM</title><date>2018-05-22</date><risdate>2018</risdate><abstract>An exemplary pressure influencing assembly for an aircraft auxiliary system an inlet opening to an aircraft auxiliary system and an exhaust opening from the aircraft auxiliary system. Both the inlet opening and the exhaust opening face at least partially radially away from an axis. At least some of the inlet opening is circumferentially aligned with at least some of the exhaust opening relative to the axis.
Un ensemble de modification de pression exemplaire pour un système auxiliaire daéronef, un orifice dadmission menant à un système auxiliaire daéronef et un orifice dévacuation à partir du système auxiliaire daéronef. Lorifice dadmission et lorifice déchappement sont orientés au moins partiellement radialement à lopposé dun axe. Au moins une partie de lorifice dadmission est alignée circonférentiellement avec au moins une partie de lorifice dévacuation par rapport laxe.</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 COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | PRESSURE INFLUENCING ASSEMBLY FOR AN AIRCRAFT AUXILIARY SYSTEM |
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