-
公开(公告)号：AU2019200135B2
公开(公告)日：2020-09-17
申请号：AU2019200135
申请日：2019-01-10
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAO TONY SHUO , OLSON NATHAN
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. WO 2011/066031 PCT/US2O1O/0-48323 coo CDo ,I
-
公开(公告)号：CA2789726C
公开(公告)日：2019-09-03
申请号：CA2789726
申请日：2010-09-09
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAU SHUO , OLSEN NATHAN
Abstract: Described in one aspect an aerial vehicle comprising: a fuselage housing a first fuselage-mounted effector; a first airfoil comprising a first control surface resiliently mounted to the first airfoil, wherein the first control surface is opposed by the first fuselage-mounted effector; a second airfoil, rotatably attached to the fuselage housing; and a second fuselage-mounted effector disposed within the fuselage housing and extendible in part to engage the second airfoil, wherein the first fuselage-mounted effector is a first actuator horn extendible via a first fuselage aperture.
-
公开(公告)号：AU2010325108A1
公开(公告)日：2012-04-19
申请号：AU2010325108
申请日：2010-09-09
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAU SHUO , OLSEN NATHAN
Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100,400,1000,1500) configured to control pitch, roll, and/or yaw via airfoils (141,142,1345,1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621,622). Embodiments include one or more rudder elements (1045, 1046,1145, 1146,1245, 1345, 1346,1445, 1446,1545, 1546) which may be rotatably attached and actuated by an effector member (1049,1149,1249,1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.
-
公开(公告)号：AU2016262762A1
公开(公告)日：2016-12-15
申请号：AU2016262762
申请日：2016-11-25
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAO TONY SHUO , OLSON NATHAN
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. coo m0 0 d
-
公开(公告)号：CA2789726A1
公开(公告)日：2011-06-03
申请号：CA2789726
申请日：2010-09-09
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAU SHUO , OLSEN NATHAN
Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100,400,1000,1500) configured to control pitch, roll, and/or yaw via airfoils (141,142,1345,1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621,622). Embodiments include one or more rudder elements (1045, 1046,1145, 1146,1245, 1345, 1346,1445, 1446,1545, 1546) which may be rotatably attached and actuated by an effector member (1049,1149,1249,1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.
-
Patent Agency Ranking
公开(公告)号：WO2011066031A3
公开(公告)日：2011-08-11
申请号：PCT/US2010048323
申请日：2010-09-09
Applicant: AEROVIRONMENT INC , MIRALLES CARLOS THOMAS , PLUMB NICK , TAU SHUO , OLSEN NATHAN
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAU SHUO , OLSEN NATHAN
CPC classification number: B64C13/28 , B64C3/44 , B64C3/50 , B64C3/56 , B64C5/12 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64C13/18 , 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) (100,400,1000,1500) configured to control pitch, roll, and/or yaw via airfoils (141,142,1345,1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621,622). Embodiments include one or more rudder elements (1045, 1046,1145, 1146,1245, 1345, 1346,1445, 1446,1545, 1546) which may be rotatably attached and actuated by an effector member (1049,1149,1249,1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.
Abstract translation: 一种包括被配置成经由翼型件（141,142,1345,1346）来控制俯仰，滚转和/或偏航的飞行器或无人飞行器（UAV）（100,400,1000,1500）的系统，所述翼型具有弹性安装的后缘， （621,622）。 实施例包括一个或多个方向舵元件（1045,1046,1145,1146,1245,1345,1346,1445,1446,1545,1545），其可以可旋转地附接并由执行器构件（1049,1149,1249,1349）致动， 设置在机身外壳（1001）内并且可部分延伸以接合一个或多个方向舵元件。
-
公开(公告)号：AU2019200135A1
公开(公告)日：2019-01-31
申请号：AU2019200135
申请日：2019-01-10
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAO TONY SHUO , OLSON NATHAN
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. WO 2011/066031 PCT/US2O1O/0-48323 coo CDo ,I
-
公开(公告)号：DK2475575T3
公开(公告)日：2017-12-11
申请号：DK10833732
申请日：2010-09-09
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , OLSEN NATHAN , TAO TONY SHUO
-
公开(公告)号：AU2010325108B2
公开(公告)日：2016-09-01
申请号：AU2010325108
申请日：2010-09-09
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAO TONY SHUO , OLSON NATHAN
Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100,400,1000,1500) configured to control pitch, roll, and/or yaw via airfoils (141,142,1345,1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621,622). Embodiments include one or more rudder elements (1045, 1046,1145, 1146,1245, 1345, 1346,1445, 1446,1545, 1546) which may be rotatably attached and actuated by an effector member (1049,1149,1249,1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.
-
公开(公告)号：EP2475575A4
公开(公告)日：2015-07-08
申请号：EP10833732
申请日：2010-09-09
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAO TONY SHUO , OLSEN NATHAN
CPC classification number: B64C13/28 , B64C3/44 , B64C3/50 , B64C3/56 , B64C5/12 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64C13/18 , 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) (100, 400, 1000, 1500) configured to control pitch, roll, and/or yaw via airfoils (141, 142, 1345, 1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621, 622). Embodiments include one or more rudder elements (1045, 1046, 1145, 1146, 1245, 1345, 1346, 1445, 1446, 1545, 1546) which may be rotatably attached and actuated by an effector member (1049, 1149, 1249, 1349) disposed within the fuselage housing (1001) 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，其被配置为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喇叭相对。 实施例包括一个或多个方向舵元件，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。
-
-
-
-
-
-
-
-
-
Search Results
10
records
(took 0.035 seconds)
