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动力涡轮叶-盘结构模态特性的界面参数规律研究

张晨 温猛 吴玉萍 袁巍 梅庆 荆建平

噪声与振动控制2025,Vol.45Issue(3):15-20,6.
噪声与振动控制2025,Vol.45Issue(3):15-20,6.DOI:10.3969/j.issn.1006-1355.2025.03.003

动力涡轮叶-盘结构模态特性的界面参数规律研究

Interface Parameter Law of Modal Characteristics of Power Turbine Blade-disk Structures

张晨 1温猛 1吴玉萍 2袁巍 2梅庆 2荆建平1

作者信息

  • 1. 上海交通大学 机械系统与振动全国重点实验室,上海 200240
  • 2. 中国航发湖南动力机械研究所,湖南 株洲 412000
  • 折叠

摘要

Abstract

The blade disk coupling structure is a key structure in power turbomachinery.Analyzing and summarizing the influence laws of interface parameters on the modal characteristics of the blade-disk coupling system are the basis for ac-curate prediction of vibration characteristics and the design and development of the blade-disk structures.This article takes a power turbine as an example to establish a finite element simulation model of a blade-disk coupling structure with a fir-tree shaped discontinuous interface and a blade crown.Multiple sets of different interface parameters and operating states were set,and the modal characteristics of the blade-disk coupling system under different operating conditions were calculated.The influence of interface parameters on the modal characteristics of the blade-disk coupling system was analyzed.The research results indicate that the contact stiffness has the most significant impact on the vibration characteristics of the blade-disk structure among the interface parameters.This article provides a necessary theoretical support and technical guidance for the performance prediction and the improvement of the power turbine blade-disk coupling systems.

关键词

振动与波/叶-盘结构/非连续界面/界面参数/模态特性

Key words

vibration and wave/blade disk structure/discontinuous interface/interface parameters/modal characteris-tics

引用本文复制引用

张晨,温猛,吴玉萍,袁巍,梅庆,荆建平..动力涡轮叶-盘结构模态特性的界面参数规律研究[J].噪声与振动控制,2025,45(3):15-20,6.

基金项目

国家自然科学基金资助项目(12072190) (12072190)

国家科技重大专项资助项目(779608000000200007) (779608000000200007)

噪声与振动控制

OA北大核心

1006-1355

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