公开(公告)号：US20150203201A1

公开(公告)日：2015-07-23

申请号：US14592362

申请日：2015-01-08

Applicant: AEROVIRONMENT, INC.

Inventor： TONY SHUO TAO ,  NATHAN OLSON ,  CARLOS THOMAS MIRALLES ,  ROBERT NICKERSON PLUMB

IPC: B64C39/02 ,  B64C9/08 ,  B64C9/18

CPC classification number: B64C3/56 ,  B64C3/44 ,  B64C3/50 ,  B64C5/12 ,  B64C9/02 ,  B64C9/08 ,  B64C9/18 ,  B64C11/00 ,  B64C13/18 ,  B64C13/34 ,  B64C39/024 ,  B64C2009/005 ,  B64C2201/021 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/121 ,  B64C2201/14 ,  B64C2201/145 ,  B64C2201/146

Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) configured to control pitch, roll, and/or yaw via airfoils having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns. Embodiments include one or more rudder elements which may be rotatably attached and actuated by an effector member disposed within the fuselage housing and extendible in part to engage the one or more rudder elements.

Abstract translation: 一种包括飞行器或无人驾驶飞行器（UAV）的系统，其构造成经由具有弹性安装的后缘的机翼来控制俯仰，滚动和/或偏航，所述后翼与机身偏转致动器角相对。 实施例包括一个或多个舵元件，其可以由设置在机身壳体内的效应器构件可旋转地附接和致动，并且部分地可部分地接合一个或多个舵元件。

公开(公告)号：US20170144749A1

公开(公告)日：2017-05-25

申请号：US15428974

申请日：2017-02-09

Applicant: AEROVIRONMENT, INC.

Inventor： TONY SHUO TAO ,  NATHAN OLSON ,  CARLOS THOMAS MIRALLES ,  ROBERT NICKERSON PLUMB

IPC: B64C13/28 ,  B64C3/50 ,  B64C11/00 ,  B64C39/02 ,  B64C9/02

Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) configured to control pitch, roll, and/or yaw via airfoils having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns. Embodiments include one or more rudder elements which may be rotatably attached and actuated by an effector member disposed within the fuselage housing and extendible in part to engage the one or more rudder elements.

公开(公告)号：US20160185445A1

公开(公告)日：2016-06-30

申请号：US14796906

申请日：2015-07-10

Applicant: AEROVIRONMENT, INC.

Inventor： CARLOS THOMAS MIRALLES ,  ROBERT NICKERSON PLUMB ,  TONY SHUO TAO ,  NATHAN OLSON

IPC: B64C3/56 ,  B64C39/02 ,  B64C9/02

Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) configured to control pitch, roll, and/or yaw via airfoils having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns. Embodiments include one or more rudder elements which may be rotatably attached and actuated by an effector member disposed within the fuselage housing and extendible in part to engage the one or more rudder elements.