AVIATION COMPLEX (MODIFICATIONS)
FIELD: aircraft fuel systems. ^ SUBSTANCE: the complex has a carrier aeroplane, located on the assembly of the external store of which is a separable unmanned flight vehicle with a cruise engine located in the cavity of its fuselage for its extraction to the working position behind the fuselage cont...
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| creator | TEREKHOV V.I ZAKOTA A.I OBREZCHIKOV V.V KUCHERENKO JU.S KARPOV S.I SELEZNEV I.S TRUSOV V.N MISHCHENKO A.P |
| description | FIELD: aircraft fuel systems. ^ SUBSTANCE: the complex has a carrier aeroplane, located on the assembly of the external store of which is a separable unmanned flight vehicle with a cruise engine located in the cavity of its fuselage for its extraction to the working position behind the fuselage contours. The fuel systems of the carrier aeroplane and the unmanned flight vehicle are interconnected by a communication line with a detachable coupler, with stop valves installed before and after it. The fuel system of the unmanned flight vehicle at the inlet of the communication line has an additional squeezed elastic fuel tank, located in the cavity of the fuselage for spreading in the point of location of the extractable engine, and a system of fuel utilization from the elastic fuel tank. ^ EFFECT: enhanced unrefuelled range. ^ 11 cl, 9 dwg |
| format | Patent |
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The fuel systems of the carrier aeroplane and the unmanned flight vehicle are interconnected by a communication line with a detachable coupler, with stop valves installed before and after it. The fuel system of the unmanned flight vehicle at the inlet of the communication line has an additional squeezed elastic fuel tank, located in the cavity of the fuselage for spreading in the point of location of the extractable engine, and a system of fuel utilization from the elastic fuel tank. ^ EFFECT: enhanced unrefuelled range. ^ 11 cl, 9 dwg</description><edition>7</edition><language>eng ; rus</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>2004</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=20041220&DB=EPODOC&CC=RU&NR=2242404C2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20041220&DB=EPODOC&CC=RU&NR=2242404C2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TEREKHOV V.I</creatorcontrib><creatorcontrib>ZAKOTA A.I</creatorcontrib><creatorcontrib>OBREZCHIKOV V.V</creatorcontrib><creatorcontrib>KUCHERENKO JU.S</creatorcontrib><creatorcontrib>KARPOV S.I</creatorcontrib><creatorcontrib>SELEZNEV I.S</creatorcontrib><creatorcontrib>TRUSOV V.N</creatorcontrib><creatorcontrib>MISHCHENKO A.P</creatorcontrib><title>AVIATION COMPLEX (MODIFICATIONS)</title><description>FIELD: aircraft fuel systems. ^ SUBSTANCE: the complex has a carrier aeroplane, located on the assembly of the external store of which is a separable unmanned flight vehicle with a cruise engine located in the cavity of its fuselage for its extraction to the working position behind the fuselage contours. The fuel systems of the carrier aeroplane and the unmanned flight vehicle are interconnected by a communication line with a detachable coupler, with stop valves installed before and after it. The fuel system of the unmanned flight vehicle at the inlet of the communication line has an additional squeezed elastic fuel tank, located in the cavity of the fuselage for spreading in the point of location of the extractable engine, and a system of fuel utilization from the elastic fuel tank. ^ EFFECT: enhanced unrefuelled range. ^ 11 cl, 9 dwg</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>2004</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBwDPN0DPH091Nw9vcN8HGNUNDw9XfxdPN0BosGa_IwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUkvigUCMjEyMTAxNnI2MilAAAsxIhig</recordid><startdate>20041220</startdate><enddate>20041220</enddate><creator>TEREKHOV V.I</creator><creator>ZAKOTA A.I</creator><creator>OBREZCHIKOV V.V</creator><creator>KUCHERENKO JU.S</creator><creator>KARPOV S.I</creator><creator>SELEZNEV I.S</creator><creator>TRUSOV V.N</creator><creator>MISHCHENKO A.P</creator><scope>EVB</scope></search><sort><creationdate>20041220</creationdate><title>AVIATION COMPLEX (MODIFICATIONS)</title><author>TEREKHOV V.I ; ZAKOTA A.I ; OBREZCHIKOV V.V ; KUCHERENKO JU.S ; KARPOV S.I ; SELEZNEV I.S ; TRUSOV V.N ; MISHCHENKO A.P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2242404C23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2004</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>TEREKHOV V.I</creatorcontrib><creatorcontrib>ZAKOTA A.I</creatorcontrib><creatorcontrib>OBREZCHIKOV V.V</creatorcontrib><creatorcontrib>KUCHERENKO JU.S</creatorcontrib><creatorcontrib>KARPOV S.I</creatorcontrib><creatorcontrib>SELEZNEV I.S</creatorcontrib><creatorcontrib>TRUSOV V.N</creatorcontrib><creatorcontrib>MISHCHENKO A.P</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TEREKHOV V.I</au><au>ZAKOTA A.I</au><au>OBREZCHIKOV V.V</au><au>KUCHERENKO JU.S</au><au>KARPOV S.I</au><au>SELEZNEV I.S</au><au>TRUSOV V.N</au><au>MISHCHENKO A.P</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AVIATION COMPLEX (MODIFICATIONS)</title><date>2004-12-20</date><risdate>2004</risdate><abstract>FIELD: aircraft fuel systems. ^ SUBSTANCE: the complex has a carrier aeroplane, located on the assembly of the external store of which is a separable unmanned flight vehicle with a cruise engine located in the cavity of its fuselage for its extraction to the working position behind the fuselage contours. The fuel systems of the carrier aeroplane and the unmanned flight vehicle are interconnected by a communication line with a detachable coupler, with stop valves installed before and after it. The fuel system of the unmanned flight vehicle at the inlet of the communication line has an additional squeezed elastic fuel tank, located in the cavity of the fuselage for spreading in the point of location of the extractable engine, and a system of fuel utilization from the elastic fuel tank. ^ EFFECT: enhanced unrefuelled range. ^ 11 cl, 9 dwg</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| language | eng ; rus |
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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 | AVIATION COMPLEX (MODIFICATIONS) |
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