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公开(公告)号：US10752346B2
公开(公告)日：2020-08-25
申请号：US15787093
申请日：2017-10-18
发明人： Andrew Paul Haldeman , Dalton T. Hampton , Frank Bradley Stamps , John Lloyd , Gilberto Morales
摘要： A rotor assembly has a composite driveshaft extending between a transmission and a yoke for providing torque from the transmission to the yoke to cause rotation of the yoke and a plurality of rotor blade assemblies attached thereto. The rotor hub also has a composite static mast coupled to the yoke and a frame. The static mast being configured to carry the lift and thrust forces from the yoke to the frame.
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公开(公告)号：US20180208305A1
公开(公告)日：2018-07-26
申请号：US15860601
申请日：2018-01-02
发明人： John Lloyd , Kirk Landon Groninga
CPC分类号： B64C29/0033 , B60L50/61 , B60L50/90 , B60L53/12 , B60L2200/10 , B64C11/001
摘要： Systems and methods include providing an aircraft with a flight control system, a hybrid electrical or hybrid hydraulic propulsion system, and three ducted fan configuration. Each of two ducted fore fans include a single rotor system having multiple rotor blades, and a single ducted aft fan includes dual, coaxial, counter-rotating rotor systems each having multiple rotor blades. The aircraft is a vertical takeoff and landing (VTOL) aircraft that is capable of operation in an airplane mode and a helicopter mode and designed to provide an urban air-taxi that would relieve ground traffic congestion, reduce carbon emissions, and increase productivity, thereby providing a faster, more efficient means of transportation.
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公开(公告)号：US10717526B2
公开(公告)日：2020-07-21
申请号：US15620310
申请日：2017-06-12
发明人： Levi Charles Hefner , Danielle Lynn Moore , Andrea Chavez , Kirk Landon Groninga , John Lloyd , Daniel Bryan Robertson
IPC分类号： B64C39/02
摘要： An Unmanned Aerial Vehicle (UAV) has a fuselage, a rotor system, and a wing configured for selective positioning during flight of the UAV to a deployed position, a stowed position, and to positions between the deployed position and the stowed position. The UAV has a flexible wing skin at least partially carried by a leading arm and the leading arm is rotatable relative to the fuselage.
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公开(公告)号：US20180354619A1
公开(公告)日：2018-12-13
申请号：US15620310
申请日：2017-06-12
发明人： Levi Charles Hefner , Danielle Lynn Moore , Andrea Chavez , Kirk Landon Groninga , John Lloyd , Daniel Bryan Robertson
CPC分类号： B64C39/024 , B64C2201/102 , B64C2201/108
摘要： An Unmanned Aerial Vehicle (UAV) has a fuselage, a rotor system, and a wing configured for selective positioning during flight of the UAV to a fully deployed position, a fully stowed position, and to positions between the fully deployed position and the fully stowed position.
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公开(公告)号：US11208207B2
公开(公告)日：2021-12-28
申请号：US15860601
申请日：2018-01-02
发明人： John Lloyd , Kirk Landon Groninga
摘要： Systems and methods include providing an aircraft with a flight control system, a hybrid electrical or hybrid hydraulic propulsion system, and three ducted fan configuration. Each of two ducted fore fans include a single rotor system having multiple rotor blades, and a single ducted aft fan includes dual, coaxial, counter-rotating rotor systems each having multiple rotor blades. The aircraft is a vertical takeoff and landing (VTOL) aircraft that is capable of operation in an airplane mode and a helicopter mode and designed to provide an urban air-taxi that would relieve ground traffic congestion, reduce carbon emissions, and increase productivity, thereby providing a faster, more efficient means of transportation.
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公开(公告)号：US10730622B2
公开(公告)日：2020-08-04
申请号：US15623328
申请日：2017-06-14
摘要： In a first aspect, there is a personal air vehicle including a body having a forward portion, a central portion and an aft portion; a first ducted fan supported by the forward portion of the body; a second ducted fan supported by the aft portion of the body; and third and fourth ducted fans supported by the left and right sides of the body and pivotable relative to the body. An aspect provides a method of flying the personal air vehicle.
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公开(公告)号：US20190112041A1
公开(公告)日：2019-04-18
申请号：US15787093
申请日：2017-10-18
发明人： Andrew Paul Haldeman , Dalton T. Hampton , Frank Bradley Stamps , John Lloyd , Gilberto Morales
摘要： A rotor assembly has a composite driveshaft extending between a transmission and a yoke for providing torque from the transmission to the yoke to cause rotation of the yoke and a plurality of rotor blade assemblies attached thereto. The rotor hub also has a composite static mast coupled to the yoke and a frame. The static mast being configured to carry the lift and thrust forces from the yoke to the frame.
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公开(公告)号：US20180362160A1
公开(公告)日：2018-12-20
申请号：US15623328
申请日：2017-06-14
摘要： In a first aspect, there is a personal air vehicle including a body having a forward portion, a central portion and an aft portion; a first ducted fan supported by the forward portion of the body; a second ducted fan supported by the aft portion of the body; and third and fourth ducted fans supported by the left and right sides of the body and pivotable relative to the body. An aspect provides a method of flying the personal air vehicle.
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