基于动力吸振原理的新型组合吸振器设计及直升机应用
Published in 应用数学和力学 • Jan 1, 2026
Authors:,,
Kunjian Jin
中国直升机设计研究所， 江西 景德镇 333001
Shuo FU
Abstract
Multi-order vibration loads on helicopter rotor systems are the main source inducing airframe vibrations, and conventional 1-way vibration absorbers are difficult to balance the multi-direction vibration requirements in flapping and lag directions. To reduce the 5/REV flapping loads and 6/REV lead l...
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