发明名称 |
AIRCRAFT FOLDING CONTROL SURFACE |
摘要 |
FIELD: transport. ^ SUBSTANCE: proposed control surface comprises root section and support. Root section is arranged aircraft airframe to turn thereon. Said root section accommodates support to turn about axis perpendicular to root section center surface. With support folded, part of control surface area ahead of root section turn axle is related to that behind said axle as 1:1 to 3:1. Folded control surface in unfolded position corresponds to condition of axial compensation. ^ EFFECT: reduced moment load in folded position. ^ 4 cl, 7 dwg |
申请公布号 |
RU2446988(C1) |
申请公布日期 |
2012.04.10 |
申请号 |
RU20100142164 |
申请日期 |
2010.10.15 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "KORPORATSIJA "TAKTICHESKOE RAKETNOE VOORUZHENIE" |
发明人 |
JURKONENKO ALEKSEJ NIKOLAEVICH |
分类号 |
B64C9/34;F42B10/14 |
主分类号 |
B64C9/34 |
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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