某直升机传动系统旋翼轴扭振计算及优化设计  

Calculation and Optimal Design of Rotor Shaft Torsional Vibration of a Helicopter Transmission System

作　　者：倪德 钟团结 魏静[2] 曹苗飞 彭斌 Ni De;Zhong Tuanjie;Wei Jing;Cao Miaofei;Peng Bin(AECC Hunan Aviation Powerplant Research Institute,Zhuzhou 412000,China;State Key Laboratory of Mechanical Transmission,Chongqing University,Chongqing 400044,China)

机构地区：[1]中国航发湖南动力机械研究所,湖南株洲412000 [2]重庆大学机械传动国家重点实验室,重庆400044

出　　处：《机械传动》2022年第1期80-86,共7页Journal of Mechanical Transmission

基　　金：国家自然科学基金(51775058)。

摘　　要：直升机传动系统旋翼轴系振动是影响其运行可靠性的重要因素,为了提高某共轴反转双旋翼传动系统旋翼轴系扭振安全裕度,在考虑轻量化设计的前提下,通过改变轴段直径尺寸或改变激励频率,使得扭振固有频率与激励频率错开,达到避免共振的目的,实现了轴系扭振调频的优化设计。优化后的轴系扭振安全裕度达到10%以上,扭振特性得到了有效改善。其计算与优化方法对直升机传动系统旋翼轴系的改进设计具有一定的指导意义。The rotor shaft vibration of the helicopter transmission system is an important factor affecting its operational reliability.In order to improve the safety margin of torsional vibration of the rotor shaft system of a coaxial counter-rotating double-rotor transmission system,under the premise of considering the lightweight design,by changing the shaft section diameter size or changing the excitation frequency makes the natural frequency of torsional vibration stagger with the excitation frequency,so as to avoid resonance and realize the optimized design of shafting torsional vibration frequency modulation.The torsional vibration safety margin of the optimized shaft system reaches more than 10%,and the torsional vibration characteristics are effectively improved.The calculation and optimization methods have certain guiding significance for the improved design of the rotor shafting of the helicopter transmission system.

关 键 词：直升机 轴系 扭转振动 优化设计 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计]