发明名称 |
MANUAL WING-FOLD MECHANISM |
摘要 |
A manual wing-fold mechanism provides a means by which to reconfigure the wing of an aircraft between a flight configuration and one that can be easily stowed and transported. The folding mechanism includes an extension tube that enables the outboard portion of the wing to be extended away from the inboard section of the wing, rotated about the lateral axis of the aircraft and then pivoted rearward so that the wing is aligned with the longitudinal axis of the aircraft along side the fuselage. The wing-fold mechanism is independent of the structural components of the wing used to convey aerodynamic loads during flight and provides a means for the user to bring the outboard wing section into a near alignment position while the wing-fold mechanism thereafter assists to refine the alignment into its final flight configuration. |
申请公布号 |
WO2015057286(A1) |
申请公布日期 |
2015.04.23 |
申请号 |
WO2014US47433 |
申请日期 |
2014.07.21 |
申请人 |
ICON AIRCRAFT, INC. |
发明人 |
GIONTA, MATTHEW;KARKOW, JON;WILDING, JOSEPH;JAGEMANN, MICHAEL |
分类号 |
B64C3/00;B64C3/56 |
主分类号 |
B64C3/00 |
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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