SUN Dingyi, KANG Renke, WANG Yidan, DONG Zhigang. Experimental Study on Ultrasonic Trepanning of Nomex Honeycomb Core. Aeronautical Manufacturing Technology, 2021, 64(17): 94-101.
SUN Dingyi, KANG Renke, WANG Yidan, DONG Zhigang. Experimental Study on Ultrasonic Trepanning of Nomex Honeycomb Core. Aeronautical Manufacturing Technology, 2021, 64(17): 94-101. DOI: 10.16080/j.issn1671-833x.2021.17.094.
Experimental Study on Ultrasonic Trepanning of Nomex Honeycomb Core
In order to solve the problems of complex machining and poor quality of the contour boundary along the axial direction in Nomex honeycomb core components
an ultrasonic trepanning method was proposed based on the trepanning process. The ultrasonic trepanning of Nomex honeycomb cores was carried out. Trepanning force measurement and incision quality observation tests were carried out under the tool spindle speed of 500–1500r/min and the feed speed of 1000–3000mm/min
respectively. The experimental results show that compared with the traditional trepanning process
the ultrasonic trepanning with the amplitude of 20μm can effectively reduce the trepanning force under the above machining parameters
with an average reduction of about 20%. The trepanning incision of Nomex honeycomb core processed by ultrasonic trepanning is smoother
more neat and without burrs than that of traditional trepanning. Combined with the experimental results
the relative motion relationship between the tool and the workpiece and the trepanning force during the ultrasonic trepanning process were further analyzed
and the reasons for the low trepanning force and good trepanning quality in ultrasonic trepanning process were theoretically explained.