发明名称 |
ADAPTIVE TWIST SYSTEM FOR A ROTOR BLADE |
摘要 |
The system of the present application includes an adaptive twist system for a rotor blade. The adaptive twist system includes a slider mechanism coupled to a spar and to a skin. The slider mechanism provides structural connectivity between the spar and the skin while also selectively translated the skin relative to the spar, thereby causing the rotor blade to twist. A control system is used to operate the slider mechanism so that the rotor blade is automatically twisted into the optional shape during changes in flight modes. |
申请公布号 |
CA2817089(C) |
申请公布日期 |
2016.02.16 |
申请号 |
CA20102817089 |
申请日期 |
2010.11.12 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
BRUNKEN, JOHN E. |
分类号 |
B64C27/72;B64C3/52;B64C11/16;B64C13/28;B64C27/46 |
主分类号 |
B64C27/72 |
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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