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公开(公告)号：EP3299282A1
公开(公告)日：2018-03-28
申请号：EP15892572.7
申请日：2015-05-19
申请人： Aeronext Inc.
发明人： SUZUKI, Youichi
CPC分类号： B64C27/08 , B64C17/02 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64D47/08
摘要： A center C of a connecting portion 16 coincides with a center U of lift generated in a body of a rotary-wing aircraft 10. The center C of the connecting portion 16 is a point of action of gravitational force of a support rod 21 and a first mounting portion with respect to the connecting portion 16. The center U of the lift is a point of action of the lift on the rotary-wing aircraft 10 and is the center of rotation of the connecting portion 16. Since the center U of the lift generated in the rotary-wing aircraft 10 is positioned at the center C of the connecting portion as described above, even in the case where the body of the rotary-wing aircraft 10 is inclined, the support rod 21 and the first mounting portion rotate around the center C of the connecting portion, and thus no rotational moment due to heavy load such as a camera 28 occurs around the center U of the lift. This makes it possible to reduce, in a case where a rotary-wing aircraft including a plurality of rotary wings travels in the horizontal direction, the difference in the rotational speeds of rotary wings on the front side and on the rear side in the traveling direction compared with a conventional case.
摘要翻译： 连接部分16的中心C与在旋翼飞机10的主体中产生的升力的中心U重合。连接部分16的中心C是支撑杆21的重力的作用点， 第一安装部分相对于连接部分16的中心。升降机的中心U是旋翼飞行器10上升降机的作用点，并且是连接部分16的旋转中心。由于 即使在旋翼飞行器10的主体倾斜的情况下，旋转翼飞机10中产生的升力也位于连接部的中心C处，支撑杆21和第一安装部旋转 围绕连接部分的中心C，并且因此在升降机的中心U周围不会出现由诸如照相机28的重负载引起的转动力矩。 由此，在包含多个旋转翼的旋翼飞机沿水平方向行驶的情况下，能够减小行驶方向前侧和后侧的旋转翼的旋转速度差 与传统案例相比。
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公开(公告)号：EP3521163A1
公开(公告)日：2019-08-07
申请号：EP16918244.1
申请日：2016-10-03
申请人： Aeronext Inc.
发明人： SUZUKI, Youichi
摘要： Provided is a delivery rotary-wing aircraft capable of stably landing on a destination without being affected by an updraft occurring in a high-rise building or the like. This rotary-wing aircraft comprising a plurality of rotary wings, a central portion to which a plurality of arms for supporting the rotary wings are connected, a first mounting portion for loading a package, a second mounting portion which is located on the opposite side to the first mounting portion as viewed from the central portion, a first supporting member for coupling the first mounting portion with the central portion, and a connection portion between the central portion and the first supporting member, is characterized by being controlled in such a manner that the center point of lift occurring in the rotary-wing aircraft with the rotation of the plurality of rotary wings and the center point of gravity of the rotary-wing aircraft coincide with the center point of the connection portion, and the first supporting member is equipped with an adjustment mechanism for vertically downwardly extending the length of the first supporting member.
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公开(公告)号：EP3954609A1
公开(公告)日：2022-02-16
申请号：EP21193083.9
申请日：2015-05-19
申请人： Aeronext Inc.
发明人： SUZUKI, Youichi
摘要： A rotary-wing aircraft (10A) comprising a connecting portion (16A) connects a second mounting portion (26) disposed on the side opposite to the first mounting portion (25) as viewed from the connecting portion (16A) to the arm portions (14A, 14B, 14C, 14D) together with the first mounting portion (25). The second mounting portion (26) is connected to the first mounting portion (25) via a support rod (21) and a support rod (22).
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