Dynamic Modeling of Helicopter Rotor Blades

机译：直升机旋翼桨叶的动态建模

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

This paper is concerned with the dynamic analysis of a pre-twisted rotating composite rotor blade. General kinematical relations for a beam theory that treats finite rotation are established. Two sets of analyses are extracted from the 3-D nonlinear blade analysis: one the 2-D linear cross section analysis, and the other the 1-D nonlinear blade analysis. The Danielson-Hodges generalized measures and Green strain are introduced to calculate strain-displacement relations. In addition, rotor structural dynamics is developed with multi-body formulation. The Hartenberg-Denavit method is introduced and the recursive computation method for the position vector of a generic point in an inertial frame is derived. In comparison with measurements from Minguet's experiment and blade-droop stop impact tests, the results are in good agreement with them.

机译：本文涉及预扭旋转复合转子叶片的动力学分析。建立了处理有限旋转的梁理论的一般运动学关系。从3-D非线性叶片分析中提取了两组分析：一组是2-D线性横截面分析，而另一组是1-D非线性叶片分析。引入了Danielson-Hodges广义测度和格林应变来计算应变-位移关系。此外，转子的结构动力学是通过多体配方开发的。介绍了Hartenberg-Denavit方法，并推导了惯性系中通用点位置矢量的递推计算方法。与Minguet实验和叶片下降停止冲击试验的测量结果相比，结果与它们非常吻合。

著录项

来源
《2008 National Academic Symposium for Ph. D. Candidates and Tri-University Workshop on Aero-Structural Mechanics amp; Aerospace Engineering(NASPCTUWMAE2008)（2008年国际航天航空工程会议暨2008年博士生学术会议（力学））》|2008年|1-5|共5页
会议地点 Beijing(CN);Beijing(CN)
作者
Yi-Feng Wang; Hao-Wen Wang; Zheng Gao; Jing-Hui Deng; Yong-Hong Fang;
展开▼
作者单位

College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, PR China;

College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, PR China;

College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, PR China;

China Helicopter Research Development Institute, Jingdezhen 333001, PR China;

China Helicopter Research Development Institute, Jingdezhen 333001, PR China;

展开▼
会议组织
原文格式 PDF
正文语种
中图分类航空、航天;
关键词
Helicopter rotor; Finite rotation; Dynamics; Recursive computation method;

机译：直升机旋翼有限旋转动力学递推计算方法;

相似文献

外文文献
中文文献
专利

1. MODELING THE ELASTIC AND DAMPING PROPERTIES OF THE MULTILAYERED TORSION BAR-BLADE STRUCTURE OF ROTORS OF LIGHT HELICOPTERS OF THE NEW GENERATION 2. FINITE-ELEMENT APPROXIMATION OF BLADES AND A MODEL OF COUPLING OF THE TORSION BAR WITH THE BLADES [J] . Paimushin V. N., Shishkin V. M. Mechanics of composite materials . 2016,第6期

机译：新一代轻型直升机的转子多层扭转杆-叶片结构的弹性和阻尼特性建模2.叶片的有限元逼近以及扭转杆与叶片的耦合模型
2. Dynamic modeling of helicopter rotor blades [J] . Wang Yifeng, Wang Haowen, Gao Zheng Tsinghua Science and Technology . 2009,第S2期

机译：直升机旋翼桨叶的动态建模
3. Dynamic Modeling of Helicopter Rotor Blades [J] . WANG Yifeng, WANG Haowen, GAO Zheng 清华大学学报（英文版） . 2009,第0z1期
4. Dynamic Modeling of Helicopter Rotor Blades [C] . National academic symposium for Ph. D. candidates . 2008

机译：直升机转子叶片的动态建模
5. UNSTEADY AERODYNAMICS IN TIME AND FREQUENCY DOMAINS FOR FINITE-TIME ARBITRARY MOTION OF HELICOPTER ROTOR BLADES IN HOVER AND FORWARD FLIGHT (AEROELASTICITY, NONLINEAR PERIODIC SYSTEMS, CASCADE AERO, MODELING, RATIONAL APPROXIMATIONS). [D] . ASGHAR-HESSARI-DINYAVARI, MEHRAN. 1985

机译：悬停和向前飞行中直升机转子叶片有限时任意运动的时间和频率域非定常气动特性（气动弹性，非线性周期系统，级联气动，建模，有理近似）。
6. Process Modeling of Composite Materials for Wind-Turbine Rotor Blades: Experiments and Numerical Modeling [O] . Birgit Wieland, Sven Ropte 2017

机译：风力涡轮机转子叶片复合材料的过程建模：实验和数值建模
7. Nonlinear dynamics in the modeling of helicopter rotor blade lead/lag motion [O] . King Robert L. 1999

机译：直升机旋翼桨叶超前/滞后运动建模中的非线性动力学

Dynamic Modeling of Helicopter Rotor Blades

摘要

著录项

相似文献

相关主题

期刊订阅