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公开(公告)号：US20200307763A1
公开(公告)日：2020-10-01
申请号：US16875609
申请日：2020-05-15
Applicant: AeroVironment, Inc.
Inventor： Carlos Thomas Miralles , Robert Nickerson Plumb , Tony Shuo Tao , Nathan Olson
IPC: B64C3/56 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/02 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00
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.
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公开(公告)号：US20210261234A1
公开(公告)日：2021-08-26
申请号：US17174571
申请日：2021-02-12
Applicant: AeroVironment, Inc.
Inventor： Tony Shuo Tao , Nathan Olson , Carlos Thomas Miralles , Robert Nickerson Plumb
IPC: B64C3/56 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/02 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00
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.
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公开(公告)号：US12043382B2
公开(公告)日：2024-07-23
申请号：US18096479
申请日：2023-01-12
Applicant: AeroVironment, Inc.
Inventor： Tony Shuo Tao , Nathan Olson , Carlos Thomas Miralles , Robert Nickerson Plumb
IPC: B64C13/34 , B64C3/44 , B64C3/50 , B64C3/56 , B64C5/12 , B64C9/02 , B64C9/08 , B64C9/18 , B64C9/36 , B64C11/00 , B64C13/18 , B64C39/02 , B64U40/10 , B64C9/00 , B64U10/25 , B64U20/50 , B64U30/12 , B64U70/00 , B64U101/15
CPC classification number: B64C3/56 , B64C3/44 , B64C3/50 , B64C5/12 , B64C9/02 , B64C9/08 , B64C9/18 , B64C9/36 , B64C11/00 , B64C13/18 , B64C13/34 , B64C39/024 , B64U40/10 , B64C2009/005 , B64U10/25 , B64U20/50 , B64U30/12 , B64U70/00 , B64U2101/15 , B64U2201/00 , B64U2201/104 , B64U2201/20
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.
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公开(公告)号：US11667373B2
公开(公告)日：2023-06-06
申请号：US17177974
申请日：2021-02-17
Applicant: AeroVironment, Inc.
Inventor： Carlos Thomas Miralles , Robert Nickerson Plumb , Tony Shuo Tao , Nathan Olson
IPC: B64C3/56 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/02 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64U10/25 , B64U30/12 , B64U70/00 , B64U101/15 , B64C9/00
CPC classification number: B64C3/56 , B64C3/44 , B64C3/50 , B64C5/12 , B64C9/02 , B64C9/08 , B64C9/18 , B64C9/36 , B64C11/00 , B64C13/18 , B64C13/34 , B64C39/024 , B64C2009/005 , B64U10/25 , B64U30/12 , B64U70/00 , B64U2101/15 , B64U2201/00 , B64U2201/104 , B64U2201/20
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.
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公开(公告)号：US20230150649A1
公开(公告)日：2023-05-18
申请号：US18096479
申请日：2023-01-12
Applicant: AeroVironment, Inc.
Inventor： Tony Shuo Tao , Nathan Olson , Carlos Thomas Miralles , Robert Nickerson Plumb
IPC: B64C3/56 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/02 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00
CPC classification number: B64C3/56 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/024 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64U10/25
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.
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Patent Agency Ranking
公开(公告)号：US20230264805A1
公开(公告)日：2023-08-24
申请号：US18139187
申请日：2023-04-25
Applicant: AeroVironment, Inc.
Inventor： Carlos Thomas Miralles , Robert Nickerson Plumb , Tony Shuo Tao , Nathan Olson
IPC: B64C3/56 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/02 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00
CPC classification number: B64C3/56 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/024 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64U10/25
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.
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公开(公告)号：US20210261235A1
公开(公告)日：2021-08-26
申请号：US17177974
申请日：2021-02-17
Applicant: AeroVironment, Inc.
Inventor： Carlos Thomas Miralles , Robert Nickerson Plumb , Tony Shuo Tao , Nathan Olson
IPC: B64C3/56 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/02 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00
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.
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公开(公告)号：US10960968B2
公开(公告)日：2021-03-30
申请号：US16875609
申请日：2020-05-15
Applicant: AeroVironment, Inc.
Inventor： Carlos Thomas Miralles , Robert Nickerson Plumb , Tony Shuo Tao , Nathan Olson
IPC: B64C3/56 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/02 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64C9/00
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.
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公开(公告)号：US10696375B2
公开(公告)日：2020-06-30
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 , B64C13/34 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C9/36 , B64C39/02 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64C9/00
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.
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公开(公告)号：US10583910B2
公开(公告)日：2020-03-10
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: B64C3/56 , B64C9/36 , B64C5/12 , B64C13/34 , B64C3/44 , B64C3/50 , B64C13/18 , B64C39/02 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64C9/00
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.
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