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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|