FOLDABLE AIRCRAFT WITH ANHEDRAL STABILIZING WINGS |
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| 申请号 | US15272311 | 申请日 | 2016-09-21 | 公开(公告)号 | US20180079488A1 | 公开(公告)日 | 2018-03-22 |
| 申请人 | Bell Helicopter Textron Inc.; | 发明人 | Brad J. Roberts; Steven R. Ivans; | ||||
| 摘要 | An aircraft including a fuselage having a longitudinal axis extending through the fuselage front end and the fuselage rear end; a foldable wing located on the fuselage and being movable between a flight position wherein the wing is generally perpendicular to the longitudinal axis, and a stowed position wherein the wing is generally parallel to the longitudinal axis; and a pair of stabilizing wings having an anhedral orientation disposed on the fuselage. | ||||||
| 权利要求 | |||||||
| 说明书全文 | |||||||
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