公开(公告)号：US09016619B2

公开(公告)日：2015-04-28

申请号：US13384424

申请日：2010-07-27

申请人： Masaki Fuchiwaki ,  Tadatsugu Imura ,  Kazuhiro Tanaka

发明人： Masaki Fuchiwaki ,  Tadatsugu Imura ,  Kazuhiro Tanaka

IPC分类号： B64C33/02 ,  B64C33/00 ,  A63H27/00

CPC分类号： B64C33/02 ,  A63H27/008 ,  B64C33/00

摘要： A flapping flying robot including a body with a longitudinal side extending in a front to back direction, a left wing and a right wing respectively including a left front frame and a right front frame, base ends of the left and right front frames rotatably attached to a front side of the body, and a flapping structure mounted on an upper side of the body, the flapping structure powered by a rotary drive source, the flapping structure rotating the left and right front frames and thereby flapping the left and right wings and a duration of an upstroke of the left and right wings flapped by the flapping structure is shorter than a duration of a downstroke of the left and right wings to generate a lift force.

摘要翻译： 一种拍动飞行机器人，包括：前后方向延伸的纵向侧的主体，分别包括左前框架和右前框架的左翼和右翼，左前框架和右前框架的基端部可旋转地连接到 主体的前侧，以及安装在主体的上侧的拍动结构，由旋转驱动源供电的拍动结构，所述拍动结构使左右前框架旋转并由此拍动左右翼和一 由扑翼结构拍打的左右翼的上行时间短于左右翼的向下行程的持续时间，以产生提升力。

公开(公告)号：US20120115390A1

公开(公告)日：2012-05-10

申请号：US13384424

申请日：2010-07-27

申请人： Masaki Fuchiwaki ,  Tadatsugu Imura ,  Kazuhiro Tanaka

发明人： Masaki Fuchiwaki ,  Tadatsugu Imura ,  Kazuhiro Tanaka

IPC分类号： A63H27/00

CPC分类号： B64C33/02 ,  A63H27/008 ,  B64C33/00

摘要： A flapping flying robot includes: a body 11 with a longitudinal side extending in a front-back direction; left and right wings 14, 15 respectively including left and right front frames 12, 13, base ends of the left and right frames 12, 13 rotatably attached to a front of the body; and a flapping means 24 flapping the left and right wings 14, 15, the means 24 including a crank 17 in the body 11 with a shaft extending in the front-back direction and rotatably driven in one direction by a rotary drive source 16, first and second crank rods 20, 23 rotatably connecting first and second supports 18, 21 of the crank 17 respectively to left and right connecting portions 19, 22 of the left and right frames 12, 13; wherein duration of upstrokes of the left and right wings 14, 15 is shorter than duration of downstrokes of the same to generate lift forces.

摘要翻译： 拍打飞行机器人包括：主体11，其具有沿前后方向延伸的纵向侧; 分别包括左右前框架12,13的左右翼片14,15，可旋转地附接到主体前部的左右框架12,13的基端部; 以及拍动装置24，使左翼翼和右翼14,15振动，包括主体11中的曲柄17的装置24具有沿前后方向延伸的轴并且通过旋转驱动源16沿一个方向可旋转地驱动 以及将曲柄17的第一和第二支撑18,21分别旋转地连接到左右框架12,13的左右连接部19,22的第二曲柄杆20,23; 其中左翼翼14和右翼15的上冲持续时间短于其相同的下冲程度以产生升力。