发明名称 |
STAROVEROV' WING (VERSIONS) |
摘要 |
FIELD: transport.SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft hardware intended for improving landing capabilities. Aircraft wing consists of outer wings. Note here that outer wings or their part turn about axis located in plan between perpendicular to aircraft axis and outer wing axis. Outer wing may turn relative to line making in plan with aircraft lengthwise axis the angle exceeding its sweep angle.EFFECT: short landing run, efficient braking by wheels.4 cl, 2 dwg |
申请公布号 |
RU2480375(C1) |
申请公布日期 |
2013.04.27 |
申请号 |
RU20110151975 |
申请日期 |
2011.12.19 |
申请人 |
STAROVEROV NIKOLAJ EVGEN'EVICH |
发明人 |
STAROVEROV NIKOLAJ EVGEN'EVICH |
分类号 |
B64C9/32;B64C3/38;B64C3/56 |
主分类号 |
B64C9/32 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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