摘要
为了产生使微扑翼飞行器上升的升力,翅翼在下拍时的面积要尽可能大,而上拍时要尽可能小。针对这种物理矛盾,应用TRIZ理论的动态法,提出了近30种翅翼运动规划方案,其中许多是不曾采用过的。为新的翅翼驱动机构的设计提供了一定的基础。
For the purpose of producing the lift power for a micro aerial vehicle （MAV） flapping wing, it is de- sired that the area of flapping wing is as large as possible in down - stroke, and small in up - stroke. This is regarded as a kind of physical conflicts in TRIZ theory. Using the dynamic method from TRIZ theory, almost 30 kinds of motion planning are proposed, some of them have not been presented in literatures. The results will provide some foundations for the design of new flapping wing mechanism.
出处
《机械传动》
CSCD
北大核心
2012年第7期7-13,共7页
Journal of Mechanical Transmission
基金
国家自然科学基金项目(50675180
51175437)
