公开(公告)号：US12091149B2

公开(公告)日：2024-09-17

申请号：US17225352

申请日：2021-04-08

申请人： Abbott Aerospace Canada Ltd.

发明人： Richard Paul Abbott

IPC分类号： B64C29/02 ,  B64C3/14 ,  B64C9/00 ,  B64D9/00 ,  B64D27/24 ,  B64U10/20 ,  B64U20/40 ,  B64U30/14 ,  B64U30/295 ,  B64U50/13 ,  B64U60/70 ,  B64D7/00 ,  B64U20/60 ,  B64U50/19 ,  B64U101/15 ,  B64U101/31 ,  F42B23/24

CPC分类号： B64C29/02 ,  B64C3/14 ,  B64C9/00 ,  B64D9/00 ,  B64D27/24 ,  B64U10/20 ,  B64U20/40 ,  B64U30/14 ,  B64U30/295 ,  B64U50/13 ,  B64U60/70 ,  B64C2009/005 ,  B64C2211/00 ,  B64D7/00 ,  B64U20/60 ,  B64U50/19 ,  B64U2101/15 ,  B64U2101/31 ,  F42B23/24

摘要： The present specification relates generally to unmanned aerial vehicles, and specifically to a vertical take-off and lift unmanned aerial vehicle configured for high speed, long-distance flight, and vertical take-off and lift, while carrying a significant payload. The aerial vehicle includes a first propeller and a second propeller, each comprising at least two blades and each disposed on opposite lateral edges of the aerial vehicle; a tail segment forming a trailing edge of the aerial vehicle, wherein the tail segment comprises: an elevator; and a first wing and a second wing, each comprising an aileron. The aerial vehicle further includes four fins, wherein the four fins are affixed to lateral edges behind the first propeller or the second propeller and configured as endplates; a motor; and a power supply.

公开(公告)号：US20220324561A1

公开(公告)日：2022-10-13

申请号：US17225352

申请日：2021-04-08

申请人： Abbott Aerospace Canada Ltd.

发明人： Richard Paul Abbott

IPC分类号： B64C39/02 ,  B64C29/02 ,  B64C9/00 ,  B64D27/24 ,  B64D9/00 ,  B64C3/14

摘要： The present specification relates generally to unmanned aerial vehicles, and specifically to a vertical take-off and lift unmanned aerial vehicle configured for high speed, long-distance flight, and vertical take-off and lift, while carrying a significant payload. The aerial vehicle includes a first propeller and a second propeller, each comprising at least two blades and each disposed on opposite lateral edges of the aerial vehicle; a tail segment forming a trailing edge of the aerial vehicle, wherein the tail segment comprises: an elevator; and a first wing and a second wing, each comprising an aileron. The aerial vehicle further includes four fins, wherein the four fins are affixed to lateral edges behind the first propeller or the second propeller and configured as endplates; a motor; and a power supply.