Friction damping for turbomachinery: A comprehensive review of modelling, design strategies, and testing capabilities

IF 11.5 1区工程技术 Q1 ENGINEERING, AEROSPACE Progress in Aerospace Sciences Pub Date : 2024-05-01 DOI:10.1016/j.paerosci.2024.101018

Jie Yuan , Chiara Gastaldi , Enora Denimal Goy , Benjamin Chouvion

{"title":"Friction damping for turbomachinery: A comprehensive review of modelling, design strategies, and testing capabilities","authors":"Jie Yuan , Chiara Gastaldi , Enora Denimal Goy , Benjamin Chouvion","doi":"10.1016/j.paerosci.2024.101018","DOIUrl":null,"url":null,"abstract":"<div><p>This paper presents a comprehensive review of recent advancements in modelling approaches, design strategies, and testing techniques applied to friction damping in turbomachinery. It critically evaluates experimental testing, design processes, and optimisation studies, along with the latest developments in numerical modelling techniques. The review begins with an overview of vibration mitigation methods and the historical development of friction dampers for bladed disk systems. Subsequent sections explore research efforts aimed at enhancing numerical and simulation modelling capabilities, encompassing contact friction models, reduced-order modelling methods, and numerical solvers suitable for real-world applications and industrial high-fidelity models. The paper also delves into available testing rigs for experimental validation and characterisation of various friction damper types, as well as the literature on uncertainty quantification in friction damping. It concludes by highlighting recent trends in novel concepts, modelling techniques, and testing technologies shaping the design of next-generation friction dampers.</p></div>","PeriodicalId":54553,"journal":{"name":"Progress in Aerospace Sciences","volume":"147 ","pages":"Article 101018"},"PeriodicalIF":11.5000,"publicationDate":"2024-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S0376042124000447/pdfft?md5=86f88d315071120aa1d1bdfaa67b6d6e&pid=1-s2.0-S0376042124000447-main.pdf","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Progress in Aerospace Sciences","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0376042124000447","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}

引用次数: 0

Abstract

This paper presents a comprehensive review of recent advancements in modelling approaches, design strategies, and testing techniques applied to friction damping in turbomachinery. It critically evaluates experimental testing, design processes, and optimisation studies, along with the latest developments in numerical modelling techniques. The review begins with an overview of vibration mitigation methods and the historical development of friction dampers for bladed disk systems. Subsequent sections explore research efforts aimed at enhancing numerical and simulation modelling capabilities, encompassing contact friction models, reduced-order modelling methods, and numerical solvers suitable for real-world applications and industrial high-fidelity models. The paper also delves into available testing rigs for experimental validation and characterisation of various friction damper types, as well as the literature on uncertainty quantification in friction damping. It concludes by highlighting recent trends in novel concepts, modelling techniques, and testing technologies shaping the design of next-generation friction dampers.

查看原文

微信好友朋友圈 QQ好友复制链接

本刊更多论文

涡轮机械的摩擦阻尼：全面回顾建模、设计策略和测试能力

本文全面回顾了应用于透平机械摩擦阻尼的建模方法、设计策略和测试技术的最新进展。它对实验测试、设计流程和优化研究以及数值建模技术的最新发展进行了严格评估。综述首先概述了振动缓解方法和叶盘系统摩擦阻尼器的历史发展。随后的章节探讨了旨在增强数值和模拟建模能力的研究工作，包括接触摩擦模型、降阶建模方法以及适合实际应用和工业高保真模型的数值求解器。本文还深入探讨了用于实验验证和表征各种摩擦阻尼器类型的可用测试平台，以及摩擦阻尼不确定性量化方面的文献。最后，论文重点介绍了影响下一代摩擦阻尼器设计的新概念、建模技术和测试技术的最新趋势。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

求助全文

约1分钟内获得全文去求助

来源期刊

Progress in Aerospace Sciences 工程技术-工程：宇航

CiteScore

20.20

自引率

3.10%

发文量

审稿时长

5 months

期刊介绍： "Progress in Aerospace Sciences" is a prestigious international review journal focusing on research in aerospace sciences and its applications in research organizations, industry, and universities. The journal aims to appeal to a wide range of readers and provide valuable information. The primary content of the journal consists of specially commissioned review articles. These articles serve to collate the latest advancements in the expansive field of aerospace sciences. Unlike other journals, there are no restrictions on the length of papers. Authors are encouraged to furnish specialist readers with a clear and concise summary of recent work, while also providing enough detail for general aerospace readers to stay updated on developments in fields beyond their own expertise.

期刊最新文献

Compressible vortex loops and their interactions A comprehensive review of lunar-based manufacturing and construction Space sails for achieving major space exploration goals: Historical review and future outlook Editorial Board Responsive tolerant control: An approach to extend adaptability of launch vehicles