公开(公告)号：US10155585B2

公开(公告)日：2018-12-18

申请号：US14775793

申请日：2014-03-13

Applicant: AERYON LABS INC.

Inventor： Glen Johannesson ,  David Kroetsch ,  Michael Peasgood ,  Stephen Marchetti

IPC: B64C27/50 ,  B64C39/02

Abstract: Folding propeller system for safe packing and shipping, and easy deployment.

公开(公告)号：US20160001879A1

公开(公告)日：2016-01-07

申请号：US14775793

申请日：2014-03-13

Applicant: AERYON LABS INC.

Inventor： Glen Johannesson ,  David Kroetsch ,  Michael Peasgood ,  Stephen Marchetti

IPC: B64C27/50 ,  B64C39/02

CPC classification number: B64C27/50 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/20

Abstract: Folding propeller system for safe packing and shipping, and easy deployment.

Abstract translation: 折叠螺旋桨系统，安全包装和运输，易于部署。

公开(公告)号：US09783294B2

公开(公告)日：2017-10-10

申请号：US14436310

申请日：2013-10-17

Applicant: AERYON LABS INC.

Inventor： Glen Johannesson ,  David Kroetsch ,  Michael Peasgood ,  Stephen Marchetti

IPC: B64C27/00 ,  B64C39/02 ,  B64C27/08 ,  B64C1/30

CPC classification number: B64C39/024 ,  B64C1/30 ,  B64C27/08 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/165 ,  B64C2201/20

Abstract: In an aspect, an apparatus includes a hovering unmanned aerial vehicle (HUAV). The HUAV includes an arm assembly configured to support a propeller in such a way that propeller drag of the propeller is decoupled from yaw torque requirements associated with the hovering unmanned aerial vehicle. In another aspect, an apparatus includes an HUAV that has an arm assembly that is field-foldable relative to the HUAV between a flight-ready state and a folded state. In another aspect, an apparatus includes an HUAV having an arm assembly that is keyed in such a way as to facilitate field-assembly relative to the HUAV.

公开(公告)号：US20150259066A1

公开(公告)日：2015-09-17

申请号：US14436310

申请日：2013-10-17

Applicant: AERYON LABS INC.

Inventor： Glen Johannesson ,  David Kroetsch ,  Michael Peasgood ,  Stephen Marchetti

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C1/30 ,  B64C27/08 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/165 ,  B64C2201/20

Abstract: In an aspect, an apparatus includes a hovering unmanned aerial vehicle (HUAV). The HUAV includes an arm assembly configured to support a propeller in such a way that propeller drag of the propeller is decoupled from yaw torque requirements associated with the hovering unmanned aerial vehicle. In another aspect, an apparatus includes an HUAV that has an arm assembly that is field-foldable relative to the HUAV between a flight-ready state and a folded state. In another aspect, an apparatus includes an HUAV having an arm assembly that is keyed in such a way as to facilitate field-assembly relative to the HUAV.

Abstract translation: 一方面，一种装置包括悬停无人机（HUAV）。 HUAV包括臂组件，其构造成支撑螺旋桨，使螺旋桨的螺旋桨阻力与悬停的无人驾驶飞行器相关的偏航扭矩要求分离。 在另一方面，一种装置包括具有臂组件的HUAV，所述臂组件相对于在待飞状态和折叠状态之间的HUAV是可折叠的。 在另一方面，一种装置包括具有臂组件的HUAV，该臂组件以便于相对于HUAV的现场组装的方式键入。