公开(公告)号：US12162583B2

公开(公告)日：2024-12-10

申请号：US17094608

申请日：2020-11-10

Applicant: Bell Textron Inc.

Inventor： Michael Dean Dearman

IPC: B64C39/08 ,  B64C29/02 ,  B64U10/20 ,  B64U30/10 ,  B64U30/20 ,  B64U50/13 ,  B64U50/15 ,  B64U101/15

Abstract: An anti-aircraft system is described and includes an unmanned aerial vehicle (UAV) comprising a body; a wing connected to the body; and propulsion systems associated with the wing, wherein the propulsion systems comprise pylons releasably connected to opposite ends of the wing such that the propulsion systems may be selectively released from the wing during flight of the UAV.

公开(公告)号：US20220144426A1

公开(公告)日：2022-05-12

申请号：US17094608

申请日：2020-11-10

Applicant: Bell Textron Inc.

Inventor： Michael Dean Dearman

IPC: B64C39/02 ,  B64D27/02 ,  B64C7/00 ,  B64C39/08

Abstract: An anti-aircraft system is described and includes an unmanned aerial vehicle (UAV) comprising a body; a wing connected to the body; and propulsion systems associated with the wing, wherein the propulsion systems comprise pylons releasably connected to opposite ends of the wing such that the propulsion systems may be selectively released from the wing during flight of the UAV.