压电智能结构在直升机传动系统减振降噪中的应用与前景

徐鹏行; 张宗之; 陈蔚芳; 朱如鹏; 李苗苗; 朱欣华; 佘亦曦

doi:10.13224/j.cnki.jasp.20250176

压电智能结构在直升机传动系统减振降噪中的应用与前景

doi: 10.13224/j.cnki.jasp.20250176

徐鹏行^1,,
张宗之²,
陈蔚芳^1,*, ,,
朱如鹏^{1, 3},
李苗苗^{1, 3},
朱欣华⁴,
佘亦曦⁴

1.
南京航空航天大学机电学院，南京 210016
2.
中国人民解放军 32201部队，北京 100072
3.
南京航空航天大学直升机动力学全国重点实验室，南京 210016
4.
中国航发湖南动力机械研究所，湖南株洲 412002

基金项目: 国家自然科学基金（52275061）；某传动预研专项（KY-1044-2023-0493）

详细信息

作者简介:
徐鹏行（1997-），男，博士生，主要从事振动分析与控制、压电智能结构等方面的研究。E-mail：xu_penghang@nuaa.edu.cn

通讯作者:
陈蔚芳（1966-），女，教授，博士，主要从事智能制造、振动分析与控制等方面的研究。E-mail：meewfchen@nuaa.edu.cn

中图分类号: V275.1
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出版历程
- 收稿日期: 2025-04-14
- 网络出版日期: 2025-08-26

Application and prospect of piezoelectric smart structure in vibration and noise reduction of helicopter transmission system

XU Penghang^1
,,
ZHANG Zongzhi²,
CHEN Weifang^{1,*
, ,},
ZHU Rupeng^{1, 3},
LI Miaomiao^{1, 3},
ZHU Xinhua⁴,
SHE Yixi⁴

1.
College of Mechanical and Electrical Engineering，Nanjing University of Aeronautics and Astronautics，Nanjing 210016，China
2.
32201Troop，People’s Liberation Army of China，Beijing 100072，China
3.
National Key Laboratory of Helicopter Aeromechanics，Nanjing University of Aeronautics and Astronautics，Nanjing 210016，China
4.
Hunan Aviation Powerplant Research Institute，Aero Engine Corporation of China，Zhuzhou Hunan 412002，China

摘要

摘要:
为实现直升机传动系统振动噪声的有效控制，结合压电智能结构的特点，以传动部件、承载部件、尾传动部件以及支撑部件等减振渠道为切入点，归纳了国内外开展的采用压电智能结构进行噪声控制的发展状况，包括被动、主动和半主动控制方法。研究结果表明：在传动系统振动噪声控制方面，压电智能结构具有独特优势，国外已有部分研究开展了型号验证，为直升机整体减振降噪提供了技术支撑。中国在该领域的研究尚处于实验室验证阶段，技术成熟度不足，但也为进一步应用形成了诸多关键技术储备。根据目前国内外研究现状，结合直升机传动系统的装机需求，从压电智能材料、压电智能结构设计、压电智能控制、装机匹配性和封装可靠性这5个方面提出了该领域的一些研究方向，为直升机传动系统振动噪声控制技术提供发展思路。
- 直升机 /
- 传动系统 /
- 振动 /
- 压电智能结构 /
- 减振降噪
Abstract:
In order to realize the efficient control of vibration and noise of transmission system, combined with the characteristics of piezoelectric smart structure, the development status of noise control using piezoelectric intelligent structure was summarized from the aspects of transmission parts, bearing parts, tail transmission parts and supporting parts, including passive, active and semi-active control methods. The research results showed that the piezoelectric smart structure had unique advantages in the vibration and noise control of the transmission system. Some studies on the helicopter verification machine test were conducted, which provided technical support for the overall vibration and noise reduction of the helicopter. In this field, the research in China is still in the laboratory verification stage, and the technology maturity is insufficient. However, many key technical reserves for further application have been formed. According to the current research status, combined with the installation requirements of the helicopter transmission system, some research directions were proposed from five aspects: piezoelectric intelligent materials, piezoelectric intelligent structure design, piezoelectric intelligent control, installation matching and packaging reliability, which could provide development insights for vibration and noise control technology of helicopter transmission system.
- helicopter /
- transmission system /
- vibration /
- piezoelectric smart structure /
- vibration and noise reduction

HTML

图 1 S-76直升机舱内噪声频谱

Figure 1. Noise in the S-76 helicopter cabin

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图 2 压电智能结构振动控制途径

Figure 2. Methods of vibration control using piezoelectric structure

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图 3 4种齿轮振动控制概念

Figure 3. Four types of gear vibration control concept

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图 4 重庆大学的齿轮振动控制系统

Figure 4. Gear vibration control system of Chongqing University

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图 5 华侨大学的多级齿轮箱振动控制系统

Figure 5. Multistage gearbox vibration control system of Huaqiao University

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图 6 压电主动惯性致动器

Figure 6. Piezoelectric active inertial actuator

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图 7 装有压电叠堆的轴承座

Figure 7. Bearing seat equipped with piezoelectric stacks

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图 8 有源压电智能轴承

Figure 8. Active piezoelectric smart bearings

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图 9 切向压电主动作动器

Figure 9. Tangential piezoelectric active actuator

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图 10 NASA设计的减振环

Figure 10. Piezoelectric damping ring designed by NASA

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图 11 南京航空航天大学设计的减振环

Figure 11. Piezoelectric damping ring designed by Nanjing University of Aeronautics and Astronautics

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图 12 智能弹簧应用于转子-轴系统模型

Figure 12. Rotor-shaft system model with smart spring

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图 13 南京航空航天大学设计的智能弹簧支承

Figure 13. Smart spring support designed by Nanjing University of Aeronautics and Astronautics

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图 14 BK117直升机压电主动撑杆

Figure 14. BK117 helicopter piezoelectric active strut

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图 15 A109和Bell407直升机压电支撑结构

Figure 15. A109 and Bell407 helicopter piezoelectric support structure

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图 16 南京航空航天大学研究的压电智能撑杆

Figure 16. Piezoelectric strut studied by Nanjing University of Aeronautics and Astronautics

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