发明名称 FLYING VEHICLE SPAR
摘要 FIELD: aircraft manufacture; manufacture of load-bearing structural members. SUBSTANCE: one of cross-sections of spar has boundary line of section; part of this line is made in form of fragment or combination of fragments of oblique taper section of right circular cone. EFFECT: improved strength characteristics (rigidity) during operation under cyclic flexure; enhanced efficiency of fixation between body and adjoining part. 16 cl, 24 dwg
申请公布号 RU2144488(C1) 申请公布日期 2000.01.20
申请号 RU19990113804 申请日期 1999.07.06
申请人 ZAKRYTOE AKTSIONERNOE OBSHCHESTVO "INTELLEKT" 发明人 LOBKO V.P.;TORITSYN I.V.
分类号 B64C3/18 主分类号 B64C3/18
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