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公开(公告)号:US20240327045A1
公开(公告)日:2024-10-03
申请号:US18681408
申请日:2022-08-05
申请人: University of Kansas
IPC分类号: B64U30/299 , B64U20/30 , B64U60/50
CPC分类号: B64U30/299 , B64U20/30 , B64U60/50
摘要: This disclosure generally relates to aerial vehicles that may convert from hover-mode to missile-mode flight and back via body tilt for efficient flight and can strike wires such that neither the wires nor the aircraft are damaged, and divergence is prevented. This includes an aerial vehicle having an elongate fuselage having a nose tip, a plurality of engines connected to the fuselage, and at least three protective members connected substantially near the nose tip of the fuselage longitudinally beyond the plurality of engines.