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新型螺旋焊管飞切机
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作者 孙子栋 《焊管》 1995年第4期55-56,共2页
介绍了一种适合于螺旋焊管生产的新型飞切机的结构和特点。该飞切机采用安装在飞切小车中部的顶紧同步机构,氧──乙炔气切割的方式.它与通常使用的夹紧同步,气体切割;夹紧同步,铣刀切断;抱辊同步,气体切割等形式的飞切机比较,... 介绍了一种适合于螺旋焊管生产的新型飞切机的结构和特点。该飞切机采用安装在飞切小车中部的顶紧同步机构,氧──乙炔气切割的方式.它与通常使用的夹紧同步,气体切割;夹紧同步,铣刀切断;抱辊同步,气体切割等形式的飞切机比较,其结构简单、造价低、同步精确、成型阻力极小,有较高的经济价值和较好的推广前景. 展开更多
关键词 螺旋焊接管 飞切机 顶紧同步
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New Cutting Force Modeling Approach for Flat End Mill 被引量:9
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作者 WAN Min ZHANG Wei-hong TAN Gang QIN Guo-hua 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2007年第3期282-288,共7页
A new mechanistic cutting force model for flat end milling using the instantaneous cutting force coefficients is proposed. An in-depth analysis shows that the total cutting forces can be separated into two terms: a no... A new mechanistic cutting force model for flat end milling using the instantaneous cutting force coefficients is proposed. An in-depth analysis shows that the total cutting forces can be separated into two terms: a nominal component independent of the runout and a perturbation component induced by the runout. The instantaneous value of the nominal component is used to calibrate the cutting force coefficients. With the help of the perturbation component and the cutting force coefficients obtained above, the cutter runout is identified. Based on simulation and experimental results, the validity of the identification approach is demonstrated. The advantage of the proposed method lies in that the calibration performed with data of one cutting test under a specific regime can be applied for a great range of cutting conditions. 展开更多
关键词 RUNOUT cutting force flat end mill CALIBRATION cutting force coefficient
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Design of an Experimental Set‑up Concerning Interfacial Stress to Promote Measurement Accuracy of Adhesive Shear Strength Between Ice and Substrate 被引量:2
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作者 WANG Yusong HAN Liang +2 位作者 ZHU Chunling ZHU Chengxiang LIU Zhenguo 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2022年第5期561-568,共8页
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 sy... 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. 展开更多
关键词 aircraft de-icing adhesive shear strength finite element analysis(FEA) experimental set-up interfacial stress
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