摘要
结合辽宁通用航空研究院正在研发的油动四旋翼飞行器,阐述了飞行器整体的动力系统布局和参数匹配的原则,并且提出了相对于油动四旋翼的动力系统参数匹配和性能验证的方法。从四旋翼机的系统质量结构、飞行性能、实际应用性验证其系统的可行性。
Based on the piston powered quadrotor developed by Liaoning General Aviation Academy, the authors introduced the quadrotor＇s propulsion system＇s basic layout and parameter matching principle. The corresponding method for parameter matching and performance verification was also proposed. The quadrotor proves its feasibility from the aspects of the system＇s mass structure,flight performance and various applications.
出处
《沈阳航空航天大学学报》
2015年第6期44-49,共6页
Journal of Shenyang Aerospace University
关键词
四旋翼飞行器
油动力系统
参数匹配
活塞发动机
rotorcrafl
piston powered propulsion system
parameter matching
piston engine
