发明名称 SWEPT-FORWARD WING WITH SWIVEL PART OF OUTER WING PANELS
摘要 FIELD: aeronautical engineering. ^ SUBSTANCE: each outer panel of proposed wing includes wing extension with sweep-back leading edge, root section with swept-forward leading edge and trailing edge; swivel part of wing outer panel is articulated with this section relative to vertical axis of flying vehicle; it may be turned backward in way of flow so that sweep angle of leading edge may change from initial swept-forward to swept-back magnitudes. ^ EFFECT: increased critical velocity of aero-elastic divergence. ^ 2 dwg
申请公布号 RU2296082(C1) 申请公布日期 2007.03.27
申请号 RU20050125577 申请日期 2005.08.12
申请人 MUDZHIRISHVILI GOCHA INDIKOEVICH 发明人 MUDZHIRISHVILI GOCHA INDIKOEVICH
分类号 B64C3/48 主分类号 B64C3/48
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