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1. 发明申请

US20100264256A1 COUNTER-ROTATIONAL INERTIAL CONTROL OF ROTORCRAFT 失效
标题翻译：转轮的反转动态控制
公开(公告)号：US20100264256A1
公开(公告)日：2010-10-21
申请号：US12761842
申请日：2010-04-16
申请人： Mark Yim , Christopher Everett Thorne
发明人： Mark Yim , Christopher Everett Thorne
IPC分类号： B64C27/08 , B63H5/08
CPC分类号： B64C27/20 , B64C27/52 , B64C29/0033
摘要： A rotorcraft with two counter-rotating rotors and method for inertially controlling the rotorcraft. The rotorcraft includes a hinged frame configured such that at least one inter-rotor angle of the two counter-rotating rotors is controlled by at least one actuated hinge of the hinged frame and the rotational axes of the two counter-rotating rotors are substantially collinear when the actuated hinge is in a fully open position. The sum of the magnitudes of torque applied to the two counter-rotating rotors is varied to control the lift of the rotorcraft. The difference of the magnitudes of torque applied to the two counter-rotating rotors is varied to control the yaw of the rotorcraft. The at least one inter-rotor angle is varied using the at least one actuated hinge to control the pitch and/or roll of the rotorcraft.
摘要翻译：具有两个反转转子的旋翼航空器和用于惯性控制旋翼航空器的方法。旋翼航空器包括铰接框架，其被构造成使得两个反向旋转转子的至少一个转子间角度由铰链框架的至少一个致动铰链控制，并且两个反向旋转转子的旋转轴线基本上共线致动铰链处于完全打开位置。施加到两个反向旋转转子的扭矩的大小的总和被改变以控制旋翼航空器的升力。施加到两个反向旋转转子的扭矩的大小的差异被改变以控制旋翼航空器的偏航。使用至少一个致动的铰链来改变至少一个转子间角度，以控制旋翼航空器的俯仰和/或滚动。

2. 发明申请

US20210178579A1 INTELLIGENT GRIPPER WITH INDIVIDUAL CUP CONTROL 有权
公开(公告)号：US20210178579A1
公开(公告)日：2021-06-17
申请号：US17124812
申请日：2020-12-17
申请人： John Aaron Saunders , Christopher Everett Thorne , Matthew Paul Meduna , Joshua Timothy Geating
发明人： John Aaron Saunders , Christopher Everett Thorne , Matthew Paul Meduna , Joshua Timothy Geating
IPC分类号： B25J9/16 , B25J9/20 , B25J15/06
摘要： Systems and methods related to intelligent grippers with individual cup control are disclosed. One aspect of the disclosure provides a method of determining grip quality between a robotic gripper and an object. The method comprises applying a vacuum to two or more cup assemblies of the robotic gripper in contact with the object, moving the object with the robotic gripper after applying the vacuum to the two or more cup assemblies, and determining, using at least one pressure sensor associated with each of the two or more cup assemblies, a grip quality between the robotic gripper and the object.

3. 发明授权

US08464978B2 Counter-rotational inertial control of rotorcraft 失效
标题翻译：旋翼飞机的反转惯性控制
公开(公告)号：US08464978B2
公开(公告)日：2013-06-18
申请号：US12761842
申请日：2010-04-16
申请人： Mark Yim , Christopher Everett Thorne
发明人： Mark Yim , Christopher Everett Thorne
IPC分类号： B64C27/08 , B64C29/00
CPC分类号： B64C27/20 , B64C27/52 , B64C29/0033
摘要： A rotorcraft with two counter-rotating rotors and method for inertially controlling the rotorcraft. The rotorcraft includes a hinged frame configured such that at least one inter-rotor angle of the two counter-rotating rotors is controlled by at least one actuated hinge of the hinged frame and the rotational axes of the two counter-rotating rotors are substantially collinear when the actuated hinge is in a fully open position. The sum of the magnitudes of torque applied to the two counter-rotating rotors is varied to control the lift of the rotorcraft. The difference of the magnitudes of torque applied to the two counter-rotating rotors is varied to control the yaw of the rotorcraft. The at least one inter-rotor angle is varied using the at least one actuated hinge to control the pitch and/or roll of the rotorcraft.
摘要翻译：具有两个反转转子的旋翼航空器和用于惯性控制旋翼航空器的方法。旋翼航空器包括铰接框架，其被构造成使得两个反向旋转转子的至少一个转子间角度由铰链框架的至少一个致动铰链控制，并且两个反向旋转转子的旋转轴线基本上共线致动铰链处于完全打开位置。施加到两个反向旋转转子的扭矩的大小的总和被改变以控制旋翼航空器的升力。施加到两个反向旋转转子的扭矩的大小的差异被改变以控制旋翼航空器的偏航。使用至少一个致动的铰链来改变至少一个转子间角度，以控制旋翼航空器的俯仰和/或滚动。

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