| 直升机旋翼桨叶鸟撞动态响应计算 |
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| 引用本文： | 林长亮 王益锋 王浩文 陈仁良尚晓冬. 直升机旋翼桨叶鸟撞动态响应计算[J]. 振动与冲击, 2013, 32(10): 62-68. DOI: |
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| 作者姓名： | 林长亮 王益锋 王浩文 陈仁良尚晓冬 |
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| 作者单位： | 1. 南京航空航天大学 直升机旋翼动力学国家级重点实验室，江苏 南京，210016；2. 中国商用飞机有限责任公司 上海飞机设计研究院，上海，200232；3. 清华大学 航天航空学院，北京，1000844. 哈尔滨飞机工业集团有限责任公司，飞机设计研究所，黑龙江 哈尔滨 150066 |
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| 摘 要： | 基于旋翼综合气弹分析程序,求解出直升机旋翼桨叶在飞行过程中的稳态响应。以此作为鸟体撞击桨叶的初始状态,采用非线性流-固耦合算法,建立了直升机旋翼桨叶鸟撞动力学方程,利用直接数值积分方法求解桨叶的动态响应。并讨论了鸟体速度、质量、撞击位置、桨叶根部约束和离心力等参数对桨叶动态响应的影响,从而为直升机桨叶抗鸟撞设计提供一些理论依据。
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| 关 键 词： | 直升机 鸟撞 桨叶 动态响应 流-固耦合 |
| 收稿时间： | 2012-02-21 |
| 修稿时间： | 2012-06-21 |
COMPUTATION OF DYNAMIC RESPONSE FOR THE BIRD IMPACT ON HELICOPTER BLADE |
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| LIN Chang-liang,WANG Yi-feng,WANG Hao-wen,CHEN Ren-liang,SHANG Xiao-dong. COMPUTATION OF DYNAMIC RESPONSE FOR THE BIRD IMPACT ON HELICOPTER BLADE[J]. Journal of Vibration and Shock, 2013, 32(10): 62-68. DOI: |
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| Authors: | LIN Chang-liang WANG Yi-feng WANG Hao-wen CHEN Ren-liang SHANG Xiao-dong |
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| Affiliation: | 1.National Key Laboratory of Rotorcraft Aeromechanics , Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;2.Commercial Aircraft Corporation of China,Ltd, Shanghai Aircraft Design and Research Institute,Shanghai 200232,China;3.School of aerospace, Tsinghua University, Beijing 100084, China；4. Harbin Aircraft Industry Group Corporation, Institute of Aircraft Design，Harbin 150066, China |
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| Abstract: | The steady-state response of the helicopter rotor in flight is solved by using its comprehensive aeroelastic analysis program. The result is then used for the initial state of bird impact on the blade. The bird impact dynamic equation of helicopter rotor blade is established by adopting non-linear fluid-solid coupling algorithm. Finally the dynamic response of blades is solved by using direct numerical integration method.To provide some theoretical basis for the anti-bird impact on helicopter blade design, the system parameters such as bird speed、bird quality、impact position、blade root constraint and rotation speed were discussed in the paper. |
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| Keywords: | helicopterbird impactbladedynamic responsefluid-structure coupling |
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