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1. 发明申请

US20190202542A1 SELF-RIGHTING AERONAUTICAL VEHICLE AND METHOD OF USE 审中-公开
公开(公告)号：US20190202542A1
公开(公告)日：2019-07-04
申请号：US16174353
申请日：2018-10-30
申请人： Gaofei YAN , James Dees
发明人： Gaofei YAN , James Dees
IPC分类号： B64C1/06 , B64C1/00 , G05D1/00 , A63H30/04 , B64C1/08 , B64C17/00 , A63H15/06 , A63H27/00 , A63H33/00 , B64C27/20 , G05D1/08 , B64C27/10 , B64C17/02 , B64D47/08 , B64C39/02
摘要： An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

2. 发明申请

US20160176494A1 SELF-RIGHTING FRAME AND AERONAUTICAL VEHICLE 审中-公开
标题翻译：自拍框和航空汽车
公开(公告)号：US20160176494A1
公开(公告)日：2016-06-23
申请号：US14977546
申请日：2015-12-21
申请人： Gaofei YAN , James DEES
发明人： Gaofei YAN , James DEES
IPC分类号： B64C1/06 , B64C1/08 , A63H15/06 , A63H27/00 , A63H30/04 , B64C27/10 , B64C17/00
CPC分类号： B64C1/061 , A63H15/06 , A63H27/12 , A63H30/04 , A63H33/005 , B64C1/00 , B64C1/08 , B64C17/00 , B64C27/10
摘要： An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting dome shaped vehicle body has an apex/protrusion preferably at a top of a central vertical axis. The apex/protrusion provides initial instability to begin a self-righting process when the vehicle is inverted on a surface. A lift and stabilization panel extends across an upper portion of said frame to provide lift, drag and/or stability. A propulsion system can be located within a central void of the frame assembly and oriented to provide a lifting force. An electronics assembly is also carried by the self-righting body for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a supporting surface. The body provides self-righting functionality and protection of elements carried therein.
摘要翻译：将自身从颠倒状态维持到直立状态的航空车辆具有优选地在中心垂直轴的顶部的顶角/突出部。当车辆在表面上倒置时，顶点/突起提供初始的不稳定性，以开始自我矫正过程。电梯和稳定板横跨所述框架的上部延伸以提供升力，阻力和/或稳定性。推进系统可以位于框架组件的中心空隙内并且被定向成提供提升力。电子组件也由自动矫正机构承载，用于接收遥控命令，并且通信地互连到电源，用于远程控制航空车辆起飞，飞行和着陆在支撑表面上。身体提供自我矫正的功能和保护其中所携带的元素。

3. 发明申请

US20180057135A1 SELF-RIGHTING AERONAUTICAL VEHICLE AND METHOD OF USE 审中-公开
公开(公告)号：US20180057135A1
公开(公告)日：2018-03-01
申请号：US15672262
申请日：2017-08-08
申请人： Gaofei YAN , James Dees
发明人： Gaofei YAN , James Dees
IPC分类号： B64C1/06 , A63H33/00 , A63H27/00 , A63H15/06 , B64C17/00 , B64C1/00 , A63H30/04 , B64C27/10 , B64C1/08
CPC分类号： B64C1/061 , A63H15/06 , A63H27/12 , A63H30/04 , A63H33/005 , B64C1/00 , B64C1/08 , B64C17/00 , B64C17/02 , B64C27/10 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/146 , B64D47/08 , G05D1/0011 , G05D1/0094
摘要： A self-righting aeronautical vehicle comprising a hollowed frame and a lift mechanism. The exterior of the frame and center of gravity are adapted to self-right the vehicle. The frame can include sealed, hollowed sections for use in bodies of water. The frame can be spherical in shape enabling inspection of internal surface of partially or fully enclosed structures. Inspection equipment can be integrated into the vehicle and acquired data can be stored or wireles sly communicated to a server. A controlled or other mass can be pivotally assembled to a pivot axle spanning across the interior of the frame. The pivot axis can rotate about a vertical axis (an axis perpendicular to the elongated axis). The propulsion mechanisms can be adapted for use as a terrestrial vehicle when enclosed in a sealed spherical shell.

4. 发明申请

US20160375983A1 SELF-RIGHTING FRAME AND AERONAUTICAL VEHICLE AND METHOD OF USE 审中-公开
标题翻译：自动车架和航空汽车及其使用方法
公开(公告)号：US20160375983A1
公开(公告)日：2016-12-29
申请号：US15257904
申请日：2016-09-06
申请人： Gaofei YAN , James DEES
发明人： Gaofei YAN , James DEES
IPC分类号： B64C17/02 , G05D1/00 , B64C1/08 , B64C27/10 , B64C39/02 , B64D47/08
CPC分类号： B64C17/02 , A63H15/06 , A63H27/12 , A63H30/04 , A63H33/005 , B64C1/00 , B64C1/061 , B64C1/08 , B64C17/00 , B64C27/10 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/12 , B64C2201/146 , B64D47/08 , G05D1/0011 , G05D1/0094
摘要： A self-righting aeronautical vehicle comprising a hollowed frame and a lift mechanism. The exterior of the frame and center of gravity are adapted to self-right the vehicle. The frame can include sealed, hollowed sections for use in bodies of water. The frame can be spherical in shape enabling inspection of internal surface of partially or fully enclosed structures. Inspection equipment can be integrated into the vehicle and acquired data can be stored or wirelessly communicated to a server. A controlled or other mass can be pivotally assembled to a pivot axle spanning across the interior of the frame. The pivot axis can rotate about a vertical axis (an axis perpendicular to the elongated axis). The propulsion mechanisms can be adapted for use as a terrestrial vehicle when enclosed in a sealed spherical shell.
摘要翻译：包括中空框架和提升机构的自动对准的航空运输车辆。框架的外部和重心适合车辆自行右转。框架可以包括用于水体的密封的中空部分。框架可以是球形的，使得能够检查部分或全部封闭结构的内表面。检查设备可以集成到车辆中，并且获取的数据可以被存储或无线地传送到服务器。受控或其他质量可以枢转地组装到横跨框架内部的枢转轴。枢转轴线可绕垂直轴线（垂直于细长轴线的轴线）旋转。当封闭在密封的球壳中时，推进机构可适用于陆地车辆。

5. 发明申请

US20150291272A1 SELF-RIGHTING FRAME AND AERONAUTICAL VEHICLE 审中-公开
标题翻译：自拍框和航空汽车
公开(公告)号：US20150291272A1
公开(公告)日：2015-10-15
申请号：US14751104
申请日：2015-06-25
申请人： Gaofei YAN , James DEES
发明人： Gaofei YAN , James DEES
IPC分类号： B64C1/08 , B64C17/00 , A63H27/00 , B64C1/06
CPC分类号： B64C1/061 , A63H15/06 , A63H27/12 , A63H30/04 , A63H33/005 , B64C1/00 , B64C1/08 , B64C17/00 , B64C27/10
摘要： An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has an apex preferably at a top of a central vertical axis. The apex provides initial instability to begin a self-righting process when the vehicle is inverted on a surface. A lift and stabilization panel extends across an upper portion of said frame to provide lift, drag and/or stability. A propulsion system can be located within a central void of the frame assembly and oriented to provide a lifting force. An electronics assembly is also carried by the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a supporting surface. The frame provides self-righting functionality and protection of elements carried therein.
摘要翻译：将自身从倒立状态转换为直立状态的航空车辆具有自对准框架组件，其顶点优选地在中心垂直轴线的顶部。当车辆在表面上倒置时，顶点提供初始的不稳定性以开始自动矫正过程。电梯和稳定板横跨所述框架的上部延伸以提供升力，阻力和/或稳定性。推进系统可以位于框架组件的中心空隙内并且被定向成提供提升力。电子组件也由自动对准框架承载，用于接收远程控制命令，并且通信地互连到电源，用于远程控制航空车辆起飞，飞行和着陆在支撑表面上。该框架提供自身的功能和对其中承载的元件的保护。

6. 发明申请

US20230060888A1 SELF-RIGHTING AERONAUTICAL VEHICLE AND METHOD OF USE 有权
公开(公告)号：US20230060888A1
公开(公告)日：2023-03-02
申请号：US17948500
申请日：2022-09-20
申请人： Gaofei YAN , James DEES
发明人： Gaofei YAN , James DEES
IPC分类号： B64C1/06 , A63H33/00 , A63H27/00 , A63H15/06 , B64C17/00 , B64C1/08 , A63H30/04 , B64C27/10 , B64C1/00 , B64C17/02 , B64C39/02 , B64D47/08 , G05D1/08 , B64C27/20 , G05D1/00
摘要： An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

7. 发明申请

US20200247522A1 SELF-RIGHTING AERONAUTICAL VEHICLE AND METHOD OF USE 审中-公开
公开(公告)号：US20200247522A1
公开(公告)日：2020-08-06
申请号：US16799799
申请日：2020-02-24
申请人： Gaofei YAN , James Dees
发明人： Gaofei YAN , James Dees
IPC分类号： B64C1/06 , G05D1/00 , B64C27/20 , G05D1/08 , B64D47/08 , B64C39/02 , B64C17/02 , B64C1/00 , B64C27/10 , A63H30/04 , B64C1/08 , B64C17/00 , A63H15/06 , A63H27/00 , A63H33/00
摘要： An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

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