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自转旋翼机跳飞的旋翼诱导速度分布研究
引用本文:杨兴邦,项昌乐,徐彬.自转旋翼机跳飞的旋翼诱导速度分布研究[J].北京理工大学学报,2016,36(11):1166-1170,1199.
作者姓名:杨兴邦  项昌乐  徐彬
作者单位:北京理工大学机械与车辆学院,北京,100081;北京理工大学机械与车辆学院,北京100081;北京理工大学车辆传动国家重点实验室,北京100081
基金项目:国家部委预研项目(40401060104);国家自然科学基金资助项目(51505031)
摘    要:提出了一种自转旋翼机跳飞的旋翼叶素诱导速度随时间和径向站位的分布规律的分析方法.基于叶素理论和动量理论,建立总距突增时旋翼瞬态拉力和动态诱导速度的响应模型,通过NACA试验验证模型有效性.将响应模型引入考虑地面效应的自转旋翼机跳飞动力学模型,以总距突增和地面效应在跳飞中作用时间的起始点作为动力学模型数值求解的分段点求解方程.使用动力学模型对试验样机的跳飞性能进行仿真,并试验验证模型准确度.利用跳飞模型计算出试验样机跳飞中旋翼叶素诱导速度并分析其分布规律.结果表明某站位处诱导速度与时间的关系先呈线性后呈抛物线,某时刻诱导速度与径向站位近似呈线性. 

关 键 词:自转旋翼  总距突增  跳飞  诱导速度
收稿时间:8/4/2015 12:00:00 AM

Distribution Research on Rotor Induced Velocity in Gyroplane Jump Takeoff
YANG Xing-bang,XIANG Chang-le and XU Bin.Distribution Research on Rotor Induced Velocity in Gyroplane Jump Takeoff[J].Journal of Beijing Institute of Technology(Natural Science Edition),2016,36(11):1166-1170,1199.
Authors:YANG Xing-bang  XIANG Chang-le and XU Bin
Institution:1. School of Mechanical Engineering, Beijing Institute of Technology, Beijing 100081, China;2. State Key Laboratory of Vehicle Transmission, Beijing Institute of Technology, Beijing 100081, China
Abstract:A method was proposed to analyze the distribution principle of the induced velocity varying with the jump time and radial stand position in gyroplane. A novel response model was developed based on blade element theory and momentum theory for the dynamic induced velocity and transient thrust of rotor following a rapid blade-pitch increase, and it was experimentally validated with NACA data. Then the response model was introduced into a nonlinear jump takeoff model considering the ground effect of gyroplane. The piecewise numerical solution of the jump model was got by regarding the beginning and ending time as the piecewise point. The simulation results of a small scaled jump takeoff platform show good agreement with experiment data. Finally, the rotor induced velocity distribution of the test platform was worked out with the jump takeoff model. Results show that the induced velocity is a linear then parabola time function at the same radial stand position and an approximate linear function of the radial stand position at the same time.
Keywords:autorotative rotor  rapid blade-pitch increase  jump takeoff  induced velocity
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