Numerical analysis of the coupling mechanisms between blade/disk friction and blade-tip/casing contacts on the state-of-the-art ECL5/Catana fan stage

IF 3.2 3区 工程技术 Q2 MECHANICS International Journal of Non-Linear Mechanics Pub Date : 2025-03-01 Epub Date: 2024-12-19 DOI:10.1016/j.ijnonlinmec.2024.104970
Thibaut Vadcard, Samuel Quaegebeur, Fabrice Thouverez
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Abstract

For the first time, the interaction between two contact nonlinearities, blade-tip/casing contact and blade/disk friction, is investigated simultaneously. This contribution addresses the associated complex coupling mechanisms on the state-of-the-art industrial fan stage ECL5/Catana open test case. Both contact interfaces are accounted for in nonlinear calculations using the harmonic balance method. First, a static analysis is performed to investigate the coupling mechanism between the friction coefficient and the static blade-tip gap. Then, the dynamics response of the blade is analyzed in forced response for two reference configurations: (1) with blade-tip/casing contacts only and (2) with blade/disk friction only. Particular attention is paid to the contact kinematics of both interfaces and the vibrational motion of the blade. The forced responses are analyzed using different local indicators of the contact interfaces. As the friction coefficient is usually uncertain, the robustness of the numerical strategy is then demonstrated by performing a large number of simulations on different root friction coefficients. In the end, even more computations are performed, as a part of sensitivity studies on first order parameters, in order to map out the different relevant quantities of both interfaces: number of contacting nodes at the tip, tip contact resultant force, energy dissipation. These large scale mappings allow to identify trends and inter-dependences between the kinematics of each interface. The originality of this paper lies in the thorough analysis of this seldom studied nonlinear interaction, that is crucially important for the design of safe and efficient aircraft engines. This work demonstrates that accounting for the blade/disk friction interface in numerical simulations strongly mitigates the dynamics of the blade-tip/casing contacts and can even prevent it for a specific range of friction coefficients.
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ECL5/Catana风机级叶片/盘摩擦与叶尖/机匣接触耦合机理的数值分析
首次同时研究了叶尖/机匣接触和叶盘摩擦两种非线性接触之间的相互作用。这一贡献解决了最先进的工业风扇阶段ECL5/Catana开放测试用例上相关的复杂耦合机制。在非线性计算中,采用谐波平衡法考虑了两种接触界面。首先,进行了静力分析,探讨了摩擦系数与静叶尖间隙之间的耦合机理。然后,分析了两种参考配置(1)叶片-叶尖/机匣接触和(2)叶片-盘摩擦时叶片的动力学响应。特别注意两个界面的接触运动学和叶片的振动运动。采用不同的接触面局部指标分析了接触面的强迫响应。由于摩擦系数通常是不确定的,然后通过对不同根摩擦系数进行大量模拟来证明数值策略的鲁棒性。最后,作为一阶参数敏感性研究的一部分,进行了更多的计算,以绘制出两个界面的不同相关量:尖端接触节点数,尖端接触合力,能量耗散。这些大规模的映射可以识别每个界面的运动学之间的趋势和相互依赖性。本文的创新之处在于深入分析了这种很少被研究的非线性相互作用,这对设计安全高效的航空发动机至关重要。这项工作表明,在数值模拟中考虑叶片/盘摩擦界面会大大减轻叶片-尖端/机匣接触的动力学,甚至可以在特定的摩擦系数范围内防止这种接触。
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来源期刊
CiteScore
5.50
自引率
9.40%
发文量
192
审稿时长
67 days
期刊介绍: The International Journal of Non-Linear Mechanics provides a specific medium for dissemination of high-quality research results in the various areas of theoretical, applied, and experimental mechanics of solids, fluids, structures, and systems where the phenomena are inherently non-linear. The journal brings together original results in non-linear problems in elasticity, plasticity, dynamics, vibrations, wave-propagation, rheology, fluid-structure interaction systems, stability, biomechanics, micro- and nano-structures, materials, metamaterials, and in other diverse areas. Papers may be analytical, computational or experimental in nature. Treatments of non-linear differential equations wherein solutions and properties of solutions are emphasized but physical aspects are not adequately relevant, will not be considered for possible publication. Both deterministic and stochastic approaches are fostered. Contributions pertaining to both established and emerging fields are encouraged.
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