航空发动机失谐叶盘动态特性研究进展 |
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引用本文: | 姚建尧,高阳,王建军. 航空发动机失谐叶盘动态特性研究进展[J]. 航空制造技术, 2016, 0(21): 76-85. DOI: 10.16080/j.issn1671-833x.2016.21.076 |
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作者姓名: | 姚建尧 高阳 王建军 |
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作者单位: | 1. 重庆大学航空航天学院,重庆,400044;2. 中国航空工业集团公司贵州航空发动机研究所,贵阳,550081;3. 北京航空航天大学能源与动力工程学院,北京,100191 |
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基金项目: | 国家自然科学基金(11502037)。 |
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摘 要: | 航空发动机叶盘结构中不可避免存在的失谐会严重影响发动机的结构完整性和可靠性,国内外针对这一问题进行了大量深入的研究。详述了失谐叶盘建模、模型减缩、动态特性分析及评价等方面的研究现状,重点介绍多级叶盘和几何失谐叶盘的建模和动态特性分析等方面的最新研究进展,并对失谐叶盘未来研究方向进行了预测。
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关 键 词: | 叶盘结构 失谐 几何失谐 动态特性 模型减缩 |
A Review of Dynamic Characteristics of Mistuned Bladed Disks |
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Abstract: | The inevitable mistuning in aeroengine bladed disks can lead to considerable increase in vibratory ampli-tude and stress, and thus deteriorate the structural integrity and reliability. Therefore, the dynamic characteristics of mis-tuned bladed disks have been drawn great attention in both academic and engineering ifelds around the world. This paper presents a review of the modeling and analysis methods for mistuned bladed disks, with particular emphasis on the geomet-ric mistuning of integrally bladed rotors and multistage bladed disks. The recent researches on mathematical representation and reduced-order modeling of geometric mistuning are introduced. Important developments and future research directions in this area are highlighted. |
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Keywords: | Bladed disk Mistuning Geometric mistuning Dynamic characteristic Reduced-order model |
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