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公开(公告)号：US20200156785A1
公开(公告)日：2020-05-21
申请号：US16524008
申请日：2019-07-27
Applicant: Transition Robotics, Inc.
Inventor： Jeffrey Kyle Gibboney , Pranay Sinha
Abstract: A manned/unmanned aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as opposed to horizontal flight attitude which takes off in this vertical attitude and then transitions to a horizontal flight path. A tailless airplane which uses a control system that takes inputs for a traditional tailed airplane and translates those inputs to provide control utilizing non-traditional control methods.
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公开(公告)号：US10377482B2
公开(公告)日：2019-08-13
申请号：US15143625
申请日：2016-05-01
Applicant: Transition Robotics, Inc.
Inventor： Jeffrey Kyle Gibboney , Pranay Sinha
Abstract: A manned/unmanned aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as opposed to horizontal flight attitude which takes off in this vertical attitude and then transitions to a horizontal flight path. An aerial vehicle system which has removable wing sections which allow for re-configuration with different wing section types, allowing for configurations adapted for a particular flight profile. A method of customizing a configuration of an unmanned aerial vehicle based upon flight profile factors such as duration, stability, and maneuverability.
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公开(公告)号：US20180265193A1
公开(公告)日：2018-09-20
申请号：US15143625
申请日：2016-05-01
Applicant: Transition Robotics, Inc.
Inventor： Jeffrey Kyle Gibboney , Pranay Sinha
CPC classification number: B64C39/024 , B64C3/54 , B64C39/08 , B64C2201/021 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/165
Abstract: A manned/unmanned aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as opposed to horizontal flight attitude which takes off in this vertical attitude and then transitions to a horizontal flight path. An aerial vehicle system which has removable wing sections which allow for re-configuration with different wing section types, allowing for configurations adapted for a particular flight profile. A method of customizing a configuration of an unmanned aerial vehicle based upon flight profile factors such as duration, stability, and maneuverability.
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公开(公告)号：US11414191B2
公开(公告)日：2022-08-16
申请号：US16524008
申请日：2019-07-27
Applicant: Transition Robotics, Inc.
Inventor： Jeffrey Kyle Gibboney , Pranay Sinha
Abstract: A manned/unmanned aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as opposed to horizontal flight attitude which takes off in this vertical attitude and then transitions to a horizontal flight path. A tailless airplane which uses a control system that takes inputs for a traditional tailed airplane and translates those inputs to provide control utilizing non-traditional control methods.
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