AEROPLANO
The aircraft has main power units (1) and an auxiliary power unit (2) set at the rear portion of the fuselage (3), in which the auxiliary power unit is transversely set relative to the fuselage longitudinal axis, at the rear of the main power units. An independent claim is also included for an air i...
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| creator | NARISCHKIN VITALIY JURYEVICH EFANOV ALEXANDER GENADIEVICH MATVEEV ANDREY IVANOVICH SCHKOLIN VLADIMIR PETROVICH KODOLA VALERIY GRIGORIEVICH DEMCHENKO OLEG FEDOROVICH PJATERNEV SERGEY VLADIMIROVICH POPOVICH KONSTANTIN FEDOROVICH AGAPOV SERGEY STEPANOVICH |
| description | The aircraft has main power units (1) and an auxiliary power unit (2) set at the rear portion of the fuselage (3), in which the auxiliary power unit is transversely set relative to the fuselage longitudinal axis, at the rear of the main power units. An independent claim is also included for an air intake. |
| format | Patent |
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An independent claim is also included for an air intake.</description><edition>7</edition><language>ita</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; 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=20041025&DB=EPODOC&CC=IT&NR=TO20030319A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20041025&DB=EPODOC&CC=IT&NR=TO20030319A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NARISCHKIN VITALIY JURYEVICH</creatorcontrib><creatorcontrib>EFANOV ALEXANDER GENADIEVICH</creatorcontrib><creatorcontrib>MATVEEV ANDREY IVANOVICH</creatorcontrib><creatorcontrib>SCHKOLIN VLADIMIR PETROVICH</creatorcontrib><creatorcontrib>KODOLA VALERIY GRIGORIEVICH</creatorcontrib><creatorcontrib>DEMCHENKO OLEG FEDOROVICH</creatorcontrib><creatorcontrib>PJATERNEV SERGEY VLADIMIROVICH</creatorcontrib><creatorcontrib>POPOVICH KONSTANTIN FEDOROVICH</creatorcontrib><creatorcontrib>AGAPOV SERGEY STEPANOVICH</creatorcontrib><title>AEROPLANO</title><description>The aircraft has main power units (1) and an auxiliary power unit (2) set at the rear portion of the fuselage (3), in which the auxiliary power unit is transversely set relative to the fuselage longitudinal axis, at the rear of the main power units. An independent claim is also included for an air intake.</description><subject>AEROPLANES</subject><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>HELICOPTERS</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>eNrjZOB0dA3yD_Bx9PPnYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXxniEh_kYGBsYGxoaWjobGxKkCALjmHNk</recordid><startdate>20041025</startdate><enddate>20041025</enddate><creator>NARISCHKIN VITALIY JURYEVICH</creator><creator>EFANOV ALEXANDER GENADIEVICH</creator><creator>MATVEEV ANDREY IVANOVICH</creator><creator>SCHKOLIN VLADIMIR PETROVICH</creator><creator>KODOLA VALERIY GRIGORIEVICH</creator><creator>DEMCHENKO OLEG FEDOROVICH</creator><creator>PJATERNEV SERGEY VLADIMIROVICH</creator><creator>POPOVICH KONSTANTIN FEDOROVICH</creator><creator>AGAPOV SERGEY STEPANOVICH</creator><scope>EVB</scope></search><sort><creationdate>20041025</creationdate><title>AEROPLANO</title><author>NARISCHKIN VITALIY JURYEVICH ; EFANOV ALEXANDER GENADIEVICH ; MATVEEV ANDREY IVANOVICH ; SCHKOLIN VLADIMIR PETROVICH ; KODOLA VALERIY GRIGORIEVICH ; DEMCHENKO OLEG FEDOROVICH ; PJATERNEV SERGEY VLADIMIROVICH ; POPOVICH KONSTANTIN FEDOROVICH ; AGAPOV SERGEY STEPANOVICH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_ITTO20030319A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ita</language><creationdate>2004</creationdate><topic>AEROPLANES</topic><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>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>NARISCHKIN VITALIY JURYEVICH</creatorcontrib><creatorcontrib>EFANOV ALEXANDER GENADIEVICH</creatorcontrib><creatorcontrib>MATVEEV ANDREY IVANOVICH</creatorcontrib><creatorcontrib>SCHKOLIN VLADIMIR PETROVICH</creatorcontrib><creatorcontrib>KODOLA VALERIY GRIGORIEVICH</creatorcontrib><creatorcontrib>DEMCHENKO OLEG FEDOROVICH</creatorcontrib><creatorcontrib>PJATERNEV SERGEY VLADIMIROVICH</creatorcontrib><creatorcontrib>POPOVICH KONSTANTIN FEDOROVICH</creatorcontrib><creatorcontrib>AGAPOV SERGEY STEPANOVICH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NARISCHKIN VITALIY JURYEVICH</au><au>EFANOV ALEXANDER GENADIEVICH</au><au>MATVEEV ANDREY IVANOVICH</au><au>SCHKOLIN VLADIMIR PETROVICH</au><au>KODOLA VALERIY GRIGORIEVICH</au><au>DEMCHENKO OLEG FEDOROVICH</au><au>PJATERNEV SERGEY VLADIMIROVICH</au><au>POPOVICH KONSTANTIN FEDOROVICH</au><au>AGAPOV SERGEY STEPANOVICH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AEROPLANO</title><date>2004-10-25</date><risdate>2004</risdate><abstract>The aircraft has main power units (1) and an auxiliary power unit (2) set at the rear portion of the fuselage (3), in which the auxiliary power unit is transversely set relative to the fuselage longitudinal axis, at the rear of the main power units. An independent claim is also included for an air intake.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| language | ita |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | AEROPLANO |
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