Design of an Experimental Set‑up Concerning Interfacial Stress to Promote Measurement Accuracy of Adhesive Shear Strength Between Ice and Substrate  

考虑界面应力的高精度冰粘附力测量平台设计

作　　者：WANG Yusong HAN Liang ZHU Chunling ZHU Chengxiang LIU Zhenguo 王榆淞;韩亮;朱春玲;朱程香;刘振国(南京航空航天大学航空学院,南京210016;南京航空航天大学机械结构力学及控制国家重点实验室,南京210016)

机构地区：[1]College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China [2]State Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China

出　　处：《Transactions of Nanjing University of Aeronautics and Astronautics》2022年第5期561-568,共8页南京航空航天大学学报（英文版）

基　　金：supported by the National Natural Science Foundation of China(No.11832012).

摘　　要：Accumulation of ice on airfoils and engines seriously endangers the safety of the fight.The accurate measurement of adhesion strength at the ice-substrate interface plays a vital role in the design of anti/de-icing systems.In this pursuit,the present study envisages the evaluation of the stress at the icesubstrate interface to guide the design of experimental set-ups and improve the measurement accuracy of shear strength using the finite element analysis(FEA)method.By considering such factors as the peeling stress,maximum von-mises stress and uniformity of stress,the height and radius of ice and the loading height are investigated.Based on the simulation results,appropriate parameters are selected for the experimental validation.Simulation results show that the peeling stress is decreased by reducing the loading height and increasing the height of ice.Higher ice,increasing loading height and smaller ice radius are found to be beneficial for the uniformity of stress.To avoid cracks or ice-breaking,it is imperative that the ice should be of a small radius and greater height.Parameters including the ice height of 25 mm,radius of 20 mm,and loading height of 9 mm are adopted in the experiment.The results of FEA and the experimental validation can significantly enhance the measurement accuracy of shear strength.机翼和发动机上的积冰会对飞行安全带来严重威胁。准确测量冰‑基底界面的粘附强度对防/除冰系统的设计起着至关重要的作用。本文研究通过有限元分析(Finite element analysis,FEA)对冰‑基底界面的应力进行评估,以指导实验装置的设计,从而提高剪切粘附强度的测量精度。通过考虑剥离应力、最大冯‑诺斯应力和应力均匀性等因素,对冰的高度和半径以及加载高度进行了评估。根据仿真结果,为实验验证选择了适当的参数。仿真结果显示,通过降低加载高度和增加冰的高度,剥离应力有所下降。较高的冰层、增加加载高度和较小的冰层半径有利于提高应力均匀性。同时,为了避免裂纹产生或者冰层破碎,冰样必须满足小半径和大高度的条件。最终实验中采用的参数为冰高25 mm,半径20 mm,加载高度9 mm。有限元分析和实验验证的结果均表明,本研究能显著提高剪切粘附强度的测量精度。

关 键 词：aircraft de-icing adhesive shear strength finite element analysis(FEA) experimental set-up interfacial stress 

分 类 号：V244.15[航空宇航科学与技术—飞行器设计]