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Alternative TitleAerodynamic force test device of flapping wing flying robot
李贵祥; 苏刚; 李洪谊
Rights Holder中国科学院沈阳自动化研究所
Patent Agent沈阳科苑专利商标代理有限公司 21002
Other AbstractThe utility model discloses an aerodynamic force test device of a flapping wing flying robot, which belongs to the technical field of stress-strain test. The aerodynamic force test device of the flapping wing flying robot comprises fixed supports, a horizontal force sensor, a vertical force sensor, a test platform skeleton, a driving motor, a flapping device and a wing width adjusting plate supports which are provided with the horizontal force sensor and the vertical force sensor are respectively arranged on the fixed supports the test platform skeleton is connected with connecting supports on the horizontal force sensor and the vertical force sensor respectively through a first flexible hinge and a second flexible hinge a test platform skeleton end which is close to the vertical force sensor is provided with a counterweight the flapping device which is connected with the driving motor is arranged on the test platform skeleton between the horizontal force sensor and the vertical force sensor a position on a vertical force sensor support which is close to the flapping device is provided with a diffusion switch and the horizontal force sensor, the vertical force sensor, the diffusion switch and the motor are respectively connected with an electric control part. The aerodynamic force test device of the flapping wing flying robot improves the force test precision, so that the interference of a non-force test direction force to the force sensors is reduced.
PCT Attributes
Application Date2011-03-04
Date Available2011-09-07
Application NumberCN201120055471.4
Open (Notice) NumberCN201964991U
Contribution Rank1
Document Type专利
Recommended Citation
GB/T 7714
李贵祥,苏刚,李洪谊. 一种扑翼飞行机器人气动力测试装置[P]. 2011-09-07.
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