Aircraft wing shift device

申请号 US15088615 申请日 2016-04-01 公开(公告)号 US10046850B2 公开(公告)日 2018-08-14
申请人 Lockheed Martin Corporation; 发明人 Dustin Eli Gamble; Matthew Curran;
摘要 An aerial vehicle includes a fuselage, a wing, and a wing shift device. The wing shift device is configured to be coupled to the fuselage. The wing shift device comprises a plurality of apertures for coupling the wing to the aerial vehicle. The plurality of apertures are configured to permit the wing to be shifted in a forward or aft direction along the fuselage based on a center of gravity of the aerial vehicle.
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