Gust Response Characteristics of Helicopter Rotor Blade

机译：直升机转子叶片的阵风响应特性

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The deformation of blades effected by gust would endanger the safety of wind turbine. Based on blades elastic deformation theory, We established a model of blades rotation transient response, studied the characteristics of blades transient response effected by gust, and confirmed the procedure of blades response to gust.

机译：通过阵风实现的叶片的变形将危及风力涡轮机的安全性。基于叶片弹性变形理论，我们建立了叶片旋转瞬态响应的模型，研究了阵风的叶片瞬态响应的特性，并确认了叶片对阵风的反应的过程。

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《International Conference on Machinery, Materials Engineering, Chemical Engineering and Biotechnology》|2016年|505p|共4页
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作者
Ma Hong-ru; Sun Wen-sheng; Mu Zhi-tao; Yan Guang-yao;
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原文格式 PDF
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中图分类 TB3-53;
关键词
Helicopter; Rotor blade; Gust response;

机译：直升机;转子叶片;古响应;

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专利

1. 直升机阵风响应缓和控制律设计 [J] . 龚华军, 杨一栋南京航空航天大学学报（英文版） . 2004,第001期
2. Gust Response Analysis for Helicopter Rotors in the Hover and Forward Flights [J] . Wang Linpeng, Dai Yuting, Yang Chao Shock and vibration . 2017,第PTa4期

机译：悬停和前进飞行中直升机旋翼的阵风响应分析
3. About the impact of wind turbine blade tip vortices on helicopter rotor trim and rotor blade motion [J] . Berend G. van der Wall, Paul H. Lehmann CEAS Aeronautical Journal . 2018,第1期

机译：关于风力涡轮机叶片尖端涡流对直升机旋翼饰板和旋翼叶片运动的影响
4. Blade runners: Van Horn Aviation fast-tracks in-house testing to prove its composite helicopter rotor blades beat legacy metal rotors [J] . FRANK COLUCCI Aerospace Testing International . 2015,第Sepa期

机译：叶片赛跑者：Van Horn Aviation快速通道进行了内部测试，证明其复合直升机旋翼桨叶击败了传统金属旋翼
5. Gust Response Characteristics of Helicopter Rotor Blade [C] . Ma Hong-ru, Sun Wen-sheng, Mu Zhi-tao, International Conference on Machinery, Materials Engineering, Chemical Engineering and Biotechnology . 2016

机译：直升机转子叶片的阵风响应特性
6. Effects of rotating frame turbulence and dynamic stall on gust response of helicopter blades. [D] . Madhavan, R. 1990

机译：旋转架湍流和动态失速对直升机叶片阵风响应的影响。
7. Influence of Rotor Dynamic Scattering on Helicopter Radar Cross-Section [O] . Zeyang Zhou, Jun Huang 2020

机译：旋翼动态散射对直升机雷达截面的影响
8. A method for predicting the aerodynamic loads and dynamic response of the rotor blades of a tandem-rotor helicopter. [O] . Balcerak, John C. 1967

机译：一种预测串联旋翼直升机转子叶片的气动载荷和动态响应的方法。
9. Gust-Tunnel Investigation of the Effect of a Sharp-Edge Gust on the Flapwise Blade Bending Moments of a Model Helicopter Rotor [R] . Maglieri, D. J., Reisert, T. D. 1955

机译：锋利阵风对模型直升机旋翼叶片弯曲力矩影响的阵风研究

Gust Response Characteristics of Helicopter Rotor Blade

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