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1. 发明申请

US20080308675A1 REDUCED-PERIMETER AIRCRAFT 有权
标题翻译：减速机 - 飞机
公开(公告)号：US20080308675A1
公开(公告)日：2008-12-18
申请号：US11764021
申请日：2007-06-15
申请人： Mithra M.K.V. Sankrithi , Cameron Carnegie , Kelly Boren , Peter Colebrook
发明人： Mithra M.K.V. Sankrithi , Cameron Carnegie , Kelly Boren , Peter Colebrook
IPC分类号： B64D11/06
CPC分类号： B64D11/0601 , B64D11/06 , Y02T50/46
摘要： Aircraft that have fuselages including a series of frames spaced apart according to a frame pitch. The series of frames are covered by an aircraft skin to define an interior volume of the aircraft. The interior volume contains a series of rows of seats separated according to a seat pitch. The seat pitch may be indexed to the frame pitch such that seats are located between adjacent ones of the series of frames to permit a reduced-perimeter aircraft fuselage with substantially equal passenger comfort metrics. In some embodiments, in addition, a series of windows are located adjacent outboard seats of the series of rows of seats to permit ergonomically appropriate viewing through the series of windows by passengers seated in the outboard seats.
摘要翻译：具有机身的飞机，包括根据帧间距间隔开的一系列帧。一系列框架被飞机皮肤覆盖以限定飞行器的内部空间。内部容积包含一系列根据座椅间距分开的座椅排。座椅间距可以被索引到框架间距，使得座椅位于相邻的一系列框架之间，以允许具有基本上相等的乘客舒适度量度的减少的周边飞行器机身。在一些实施例中，此外，一系列窗口位于一系列座椅的外侧座椅附近，以允许坐在外侧座椅上的乘客通过一系列窗户进行人体工程学适当的观察。

2. 发明授权

US07717372B2 Reduced-perimeter aircraft 有权
标题翻译：减速机
公开(公告)号：US07717372B2
公开(公告)日：2010-05-18
申请号：US11764021
申请日：2007-06-15
申请人： Mithra M. K. V. Sankrithi , Cameron Carnegie , Kelly Boren , Peter Colebrook
发明人： Mithra M. K. V. Sankrithi , Cameron Carnegie , Kelly Boren , Peter Colebrook
IPC分类号： B64D11/06
CPC分类号： B64D11/0601 , B64D11/06 , Y02T50/46
摘要： Aircraft that have fuselages including a series of frames spaced apart according to a frame pitch. The series of frames are covered by an aircraft skin to define an interior volume of the aircraft. The interior volume contains a series of rows of seats separated according to a seat pitch. The seat pitch may be indexed to the frame pitch such that seats are located between adjacent ones of the series of frames to permit a reduced-perimeter aircraft fuselage with substantially equal passenger comfort metrics. In some embodiments, in addition, a series of windows are located adjacent outboard seats of the series of rows of seats to permit ergonomically appropriate viewing through the series of windows by passengers seated in the outboard seats.
摘要翻译：具有机身的飞机，包括根据帧间距间隔开的一系列帧。一系列框架被飞机皮肤覆盖以限定飞行器的内部空间。内部容积包含一系列根据座椅间距分开的座椅排。座椅间距可以被索引到框架间距，使得座椅位于相邻的一系列框架之间，以允许具有基本上相等的乘客舒适度量度的减少的周边飞行器机身。在一些实施例中，此外，一系列窗口位于一系列座椅的外侧座椅附近，以允许坐在外侧座椅上的乘客通过一系列窗户进行人体工程学适当的观察。

3. 发明申请

US20220348319A1 Circuit Based Vehicle 有权
公开(公告)号：US20220348319A1
公开(公告)日：2022-11-03
申请号：US17853081
申请日：2022-06-29
申请人： Cameron Carnegie
发明人： Cameron Carnegie
IPC分类号： B64C27/20 , B64C39/02
摘要： A first embodiment includes a circuit based aerial vehicle including an enclosed air duct circuit with a plurality of fans within respective fan tunnels and a plurality of rotating archway assemblies. The rotating archway assemblies may include respective cylinder casings with medial archways, actuating collars at opposing ends of the cylinder casing, and a rotational cylinder rotatable along its longitudinal axis. The actuating collars may be structured to spin their respective cylinder casings along the cylinder casing longitudinal axes thereby orienting the rotational cylinders in different positions along their medial axes.
A second embodiment includes rounded cylinder assemblies with respective bulbous cylinder casings including medial actuating collars that rotate rather than the entire cylinder casing. The actuating collars themselves are structured to spin their respective rotational cylinders along the rotational cylinder longitudinal axes to orient the rotational cylinders in different positions along their medial axes.

4. 发明授权

US11414182B1 Circuit based unmanned aerial vehicle 有权
公开(公告)号：US11414182B1
公开(公告)日：2022-08-16
申请号：US17571131
申请日：2022-01-07
申请人： Cameron Carnegie
发明人： Cameron Carnegie
IPC分类号： B64C27/20 , B64C39/02 , B64C23/08 , B64C23/02
摘要： A first embodiment includes a circuit based unmanned aerial vehicle (UAV) including at least one enclosed air duct vertical z-force circuit, at least one enclosed air duct lateral y-force circuit, and at least one enclosed air duct longitudinal x-force circuit whereby each circuit includes a plurality of fans within respective fan tunnels and a plurality of rotational cylinders within archways. The UAV utilizes a magnus effect at strategic points along each respective circuit to apply navigational force thereon.
A second embodiment includes a circuit based unmanned aerial vehicle (UAV) including a first and second air duct circuit joined at a medial trunk. Each circuit includes a plurality of fans within respective fan tunnels and a plurality of rotational cylinders within archways. The second embodiment also utilizes the magnus effect at strategic points along each respective circuit to apply navigational force thereon.

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