发明名称 |
Two-motion wing-fold mechanism with independent load path |
摘要 |
An aircraft wing folding system folds an outboard wing section relative to an inboard wing section between a deployed position and a stored position in two discrete motions where each motion has an independent load path separate of the loading of the wing experienced by in-flight aerodynamic forces. The wing-fold mechanism of the present invention includes a fold assembly comprising a twist component and a fold component operable to fold the outboard wing section from the deployed position to the stored position that remains substantially unloaded with respect to in-flight aerodynamic forces when the wing is in the deployed or flight configuration. |
申请公布号 |
US8157206(B2) |
申请公布日期 |
2012.04.17 |
申请号 |
US20090482308 |
申请日期 |
2009.06.10 |
申请人 |
GIONTA MATTHEW;CROCOLL JAMES;KARKOW JON;NICHOLAS PAUL;BLEDSOE SCOTT;ICON AIRCRAFT, INC. |
发明人 |
GIONTA MATTHEW;CROCOLL JAMES;KARKOW JON;NICHOLAS PAUL;BLEDSOE SCOTT |
分类号 |
B64C3/56 |
主分类号 |
B64C3/56 |
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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