发明名称 ORNITHOPTER
摘要 An ornithopter includes a main wing mounted on a fuselage, and a control system configured to control a flapping motion of the main wing. The main wing includes an inner spar, an outer spar, and a wrist portion disposed between the inner spar and the outer spar and which varies a bending angle, which is a relative angle between the inner spar and the outer spar, within a predetermined angle range. The control system includes an actuator which performs a raising motion and a lowering motion of the inner spar by moving the inner spar in an upward direction and in a downward direction, an angle sensor which measures the bending angle, and a control unit which controls the actuator to move the inner spar in response to the measured bending angle.
申请公布号 US2016009389(A1) 申请公布日期 2016.01.14
申请号 US201414759321 申请日期 2014.02.19
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 KURODA Satoshi;MORI Tomoyuki;HATTORI Kazuya;TAHARA Masato;TAKAYAMA Oki
分类号 B64C33/02 主分类号 B64C33/02
代理机构 代理人
主权项 1. An ornithopter comprising: a main wing mounted on a fuselage; and a control system configured to control a flapping motion of the main wing, wherein the main wing comprises: an inner spar extending outwardly from the fuselage; an outer spar extending outwardly from the inner spar; and a wrist portion disposed between the inner spar and the outer spar, and configured to vary a bending angle within a predetermined angle range, the bending angle being a relative angle between the inner spar and the outer spar, wherein the control system comprises: an actuator configured to perform a raising motion of the inner spar by moving the inner spar in an upward direction and to perform a lowering motion of the inner spar by moving the inner spar in a downward direction; an angle sensor mounted in the wrist portion, and configured to measure the bending angle; and a control unit configured to control the actuator to move the inner spar in response to the measured bending angle of the angle sensor.
地址 Minato-ku, Tokyo JP