FLIGHT VEHICLE WITH ROTATING TAIL UNIT OF AERODYNAMIC SURFACES
FIELD: structural and aerodynamic members of flight vehicles. SUBSTANCE: the flight vehicle has a fuselage joined to the body of the tail unit through the rotation assembly, and cantilevers fastened on the body. Every cantilever is installed through the assembly unit with an axis perpendicular to th...
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| creator | POLONSKIJ Z.A GOLOBOROD'KO V.E KLIKODUEV N.G KARPOV S.I MISHCHENKO A.P CHERNOV L.A LYCHEV I.P |
| description | FIELD: structural and aerodynamic members of flight vehicles. SUBSTANCE: the flight vehicle has a fuselage joined to the body of the tail unit through the rotation assembly, and cantilevers fastened on the body. Every cantilever is installed through the assembly unit with an axis perpendicular to the body surface. V- shaped recesses are made in the fuselage in the area of the joint to the rotating tail unit. The front lower parts of each cantilever enter the respective recess. EFFECT: automatic stabilization of a definite position relative to the fuselage of the tail unit at action of the disturbing aerodynamic rolling moment the cantilever. 7 cl, 4 dwg |
| format | Patent |
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SUBSTANCE: the flight vehicle has a fuselage joined to the body of the tail unit through the rotation assembly, and cantilevers fastened on the body. Every cantilever is installed through the assembly unit with an axis perpendicular to the body surface. V- shaped recesses are made in the fuselage in the area of the joint to the rotating tail unit. The front lower parts of each cantilever enter the respective recess. EFFECT: automatic stabilization of a definite position relative to the fuselage of the tail unit at action of the disturbing aerodynamic rolling moment the cantilever. 7 cl, 4 dwg</description><edition>7</edition><language>eng ; rus</language><subject>AEROPLANES ; AIRCRAFT ; AMMUNITION ; AVIATION ; BLASTING ; COSMONAUTICS ; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</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=20040227&DB=EPODOC&CC=RU&NR=2224969C1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20040227&DB=EPODOC&CC=RU&NR=2224969C1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>POLONSKIJ Z.A</creatorcontrib><creatorcontrib>GOLOBOROD'KO V.E</creatorcontrib><creatorcontrib>KLIKODUEV N.G</creatorcontrib><creatorcontrib>KARPOV S.I</creatorcontrib><creatorcontrib>MISHCHENKO A.P</creatorcontrib><creatorcontrib>CHERNOV L.A</creatorcontrib><creatorcontrib>LYCHEV I.P</creatorcontrib><title>FLIGHT VEHICLE WITH ROTATING TAIL UNIT OF AERODYNAMIC SURFACES</title><description>FIELD: structural and aerodynamic members of flight vehicles. SUBSTANCE: the flight vehicle has a fuselage joined to the body of the tail unit through the rotation assembly, and cantilevers fastened on the body. Every cantilever is installed through the assembly unit with an axis perpendicular to the body surface. V- shaped recesses are made in the fuselage in the area of the joint to the rotating tail unit. The front lower parts of each cantilever enter the respective recess. EFFECT: automatic stabilization of a definite position relative to the fuselage of the tail unit at action of the disturbing aerodynamic rolling moment the cantilever. 7 cl, 4 dwg</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AMMUNITION</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2004</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLBz8_F09whRCHP18HT2cVUI9wzxUAjyD3EM8fRzVwhx9PRRCPXzDFHwd1NwdA3yd4n0c_T1dFYIDg1yc3R2DeZhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfFBoUZGRiaWZpbOhsZEKAEABuQp4g</recordid><startdate>20040227</startdate><enddate>20040227</enddate><creator>POLONSKIJ Z.A</creator><creator>GOLOBOROD'KO V.E</creator><creator>KLIKODUEV N.G</creator><creator>KARPOV S.I</creator><creator>MISHCHENKO A.P</creator><creator>CHERNOV L.A</creator><creator>LYCHEV I.P</creator><scope>EVB</scope></search><sort><creationdate>20040227</creationdate><title>FLIGHT VEHICLE WITH ROTATING TAIL UNIT OF AERODYNAMIC SURFACES</title><author>POLONSKIJ Z.A ; GOLOBOROD'KO V.E ; KLIKODUEV N.G ; KARPOV S.I ; MISHCHENKO A.P ; CHERNOV L.A ; LYCHEV I.P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2224969C13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2004</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AMMUNITION</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>POLONSKIJ Z.A</creatorcontrib><creatorcontrib>GOLOBOROD'KO V.E</creatorcontrib><creatorcontrib>KLIKODUEV N.G</creatorcontrib><creatorcontrib>KARPOV S.I</creatorcontrib><creatorcontrib>MISHCHENKO A.P</creatorcontrib><creatorcontrib>CHERNOV L.A</creatorcontrib><creatorcontrib>LYCHEV I.P</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>POLONSKIJ Z.A</au><au>GOLOBOROD'KO V.E</au><au>KLIKODUEV N.G</au><au>KARPOV S.I</au><au>MISHCHENKO A.P</au><au>CHERNOV L.A</au><au>LYCHEV I.P</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>FLIGHT VEHICLE WITH ROTATING TAIL UNIT OF AERODYNAMIC SURFACES</title><date>2004-02-27</date><risdate>2004</risdate><abstract>FIELD: structural and aerodynamic members of flight vehicles. SUBSTANCE: the flight vehicle has a fuselage joined to the body of the tail unit through the rotation assembly, and cantilevers fastened on the body. Every cantilever is installed through the assembly unit with an axis perpendicular to the body surface. V- shaped recesses are made in the fuselage in the area of the joint to the rotating tail unit. The front lower parts of each cantilever enter the respective recess. EFFECT: automatic stabilization of a definite position relative to the fuselage of the tail unit at action of the disturbing aerodynamic rolling moment the cantilever. 7 cl, 4 dwg</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| language | eng ; rus |
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| subjects | AEROPLANES AIRCRAFT AMMUNITION AVIATION BLASTING COSMONAUTICS EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS |
| title | FLIGHT VEHICLE WITH ROTATING TAIL UNIT OF AERODYNAMIC SURFACES |
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