发明名称 AIRCRAFT SWEPT WING AND AEROFOIL SECTION (VERSIONS)
摘要 FIELD: transport. ^ SUBSTANCE: swept wing incorporates five aerofoil sections arranged along outer wing and jointed together by unary and bicurvature surfaces. Engine pylons are arranged under the first bicurvature surface. Wing features the arrangement of aerofoil section medium lines below chord in their central part and in above chord in their tail parts, and availability of additional parts in front parts of aerofoil sections wherein medium line runs above the chord on outer wing adjoining fuselage. In every version, aerofoil section incorporates conjugate convex and concave areas. ^ EFFECT: high aerodynamic characteristics plus possibility to arranged large-sized engines under wing. ^ 30 cl, 25 dwg, 10 tbl
申请公布号 RU2406647(C1) 申请公布日期 2010.12.20
申请号 RU20090122524 申请日期 2009.06.15
申请人 ZAKRYTOE AKTSIONERNOE OBSHCHESTVO "GRAZHDANSKIE SAMOLETY SUKHOGO";MINISTERSTVO PROMYSHLENNOSTI I TORGOVLI ROSSIJSKOJ FEDERATSII 发明人 SUBBOTIN VIKTOR VLADIMIROVICH;IVASHECHKIN JURIJ VIKTOROVICH;KOVALENKO EVGENIJ NIKOLAEVICH;LITVINOV MAKSIM SERGEEVICH;TEREKHIN VLADIMIR ALEKSEEVICH;SHEVJAKOV VLADIMIR IVANOVICH;KANTEMIROV DMITRIJ VIKTOROVICH;JASHCHENKO BORIS VLADISLAVOVICH;ANDREEV ROMAN VIKTOROVICH;BUZOVERJA NIKOLAJ PETROVICH;BOLSUNOVSKIJ ANATOLIJ LONGENOVICH;SKOMOROKHOV SERGEJ IVANOVICH;KUR'JANSKIJ MIKHAIL KIRILLOVICH
分类号 B64C3/14 主分类号 B64C3/14
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