1. Introduction
The composite-material laminate structure will inevitably encounter connection problems in use. Among them, mechanical connections are widely used in aerospace, automotive and other fields because of their high connection efficiency and reliable connection performance [1,2,3]. The drilling process is an indispensable process. During the processing, there are defects such as fiber pullout, tearing, peeling, delamination and burrs, which seriously affect the mechanical properties of the opening holes, further affecting the performance of composite structures. Therefore, it is of great research value to find a method that can reduce the occurrence of defects and improve the quality of holes [4].
Prasad and Chaitanya [5] used the Taguchi analysis method to study the delamination factors of laminates and optimized the processing parameters. The experimental results show that the peeling delamination is most affected by the thickness of the material, followed by the feed speed and fiber orientation, and the delamination rate is most affected by feed speed, followed by thickness, fiber orientation and spindle speed. Based on the numerical analysis of drilling images, Hrechuk et al. [6] carried out the non-destructive quantification of visible defects and proposed an overall parameter Q. The results of drilling experiments show that the drilling quality Q, the number of drillings, and the tool wear are linearly related. Liu et al. [7]. proposed a new delamination scheme in which delamination caused by thrust exerted by the chisel and cutting edges is considered. Amaro et al. [8] found that the presence of holes increased the energy absorbed by the damaged and delaminated regions. The delamination distribution is also affected due to the change in the interlayer shear-stress distribution, which is the main reason for the delamination between layers with different orientations. Tsao et al. [9] proposed a new method for the equivalent delamination factor and compared it with the adjusted delamination factor and the conventional delamination factor, which is suitable for characterizing delamination at the hole exit after drilling composites. Sugita et al. [10] proposed the design of a drilling tool that is shaped to suppress burrs and delamination during composite drilling. Loja et al. [11] used four different types of tools to conduct drilling experiments on glass-fiber laminates to analyze and evaluate the delamination effect and its maximum temperature. The experiments showed that the higher the drilling speed, the higher the temperature generated by friction, and the greater the damage to the aperture diameter. Velaga et al. [12] used a double-flute twist drill with a diameter of 10 mm to conduct drilling experiments on epoxy-resin/glass-fiber composites. The experimental results found that the rotation speed of 700 rpm and the feed rate of 0.4 mm/rev were used for the optimum drilling parameters of the selected tool. Guo [13] conducted cutting experiments on continuous-glass-fiber-reinforced-polypropylene composites at different cutting angles to analyze the characteristics of right-angle cutting and the causes of damage. The experiment found that the fiber cutting angle has a significant impact on the cutting process: at 0° there is groove damage; at 45° the cutting surface is the best; at 90° there is a slight burr; at 135° the resin interface cracks and many burrs are generated. Mustari et al. [14]. investigated the effect of glass-fiber content in glass-fiber composites on the drilling process. The results show that the drilling surface quality is closely related to the percentage of fiber content in the sample. In terms of roundness deviation, delamination, fiber pull-out and taper angle, the composite samples performed better when the glass-fiber content was lower. Patel et al. [15] aimed to examine the effect of tool geometry, spindle speed and feed on thrust and delamination in hybrid hemp-glass composites. Palanikumar et al. [16] studied the parameters affecting the thrust of glass-fiber-reinforced polypropylene (GFRPP) in boreholes and established an empirical relationship for determining the thrust of GFRTP drilling. Srinivasan et al. [17] used the “Brad and Spur” drill bit to drill the GFRPP matrix composites with the aim of testing the effect of drilling parameters on the roundness error, using the Box-Behnken design (BBD) technique to determine the cutting parameters that were evaluated and optimized. The results show that the model can be effectively used to predict the response variable and thus control the roundness error. Palanikumar et al. [18] studied the effect of various feed rates on thrust, spindle speed, and bit geometry using Brad and straight plunger bits, and the experimental results showed that delamination is entirely dependent on the feed rate.
In this paper, GFRPP laminates are taken as the research object to investigate the effects of different cutters and process parameters on the hole quality. The delamination factor and burr area were taken as the index to characterize the opening quality. After determining the optimal milling tool, the process window was obtained according to the appearance of the milling hole. Afterwards, the response surface method (RSM) was utilized to analyze the influence of the process parameters on the opening quality.
2. Materials and Methods
This experimental sample was made of GFRPP prepreg in order to prepare composite material laminate, and glass-fiber-reinforced-polypropylene prepreg with a thickness of 0.3 mm was fiber reinforced using [0/45/-45/90]s. Composite laminate, milled to 2.4 mm through holes using the hot press (Qingdao Huabo Machinery Technology Co., Ltd., Qingdao, China), according to the process parameters in [19]. Milling experiments were conducted by a CNC (Computer Numerical Control) engraving machine (JingYan Instruments & Technology CO., Ltd., Dongguan, China). As shown in Figure 1, milling tools included a single-edge spiral milling cutter, double-edged spiral milling cutter, corn milling cutter and PCB (Printed Circuit Board) alloy drill with the same size where L1 = 38 mm, L2 = 12 mm, d = 3.175 mm. First, the comparison among milling tools was made under the same spindle speed and feed speed of 6000 r/min and 800 mm/min, respectively. Five holes with a diameter of 8 mm were milled by each tool. The visual-inspection method was used to choose the optimal mill tool based on the macroscopic appearance near the hole.
In the milling process of traditional composite laminates, the local thermal shock [20] caused by the presence of abrasives and fibers and the low thermal conductivity of composite materials limit the temperature dissipation during hole opening, resulting in heat accumulation at the hole exit and excessively high temperature, and even in the case of improper heat dissipation treatment, the temperature will often be higher than the glass transition temperature, resulting in a decrease in the performance of the resin matrix and a significant reduction in the quality of openings [21]. In the milling experiment, the temperature change is often mainly affected by the spindle speed and feed rate [22]. Due to the wide selection of parameters in this experiment, the effect of temperature on the quality of the opening cannot be excluded from the experimental results.
Therefore, a real-time temperature-observation platform was built, and special parameter-processing points were selected to study the effect of temperature changes on the quality of the opening during milling, as depicted in Figure 2. The infrared thermal imager was supported and fixed to the main shaft of the cutting machine by a movable bracket and was able to move on the same trajectory with the main shaft of the cutting machine. The thermal-imaging camera directly captures the milling hole, and is connected to an external receiving software device, which can display the milling temperature change on the screen in real time. A Canon digital camera (EOS 200DⅡ, Canon (CHINA) CO., Ltd., Beijing, China) was used to take pictures of the openings, and ImageJ and Photoshop software were used to process the pictures to calculate the delamination factor and burr area during milling, as shown in Figure 3. The delamination factor was defined as the actual diameter divided by the designed diameter, referring to Equation (1). The delamination factor and burr area were taken as the index to characterize the opening quality. After determining the optimal milling tool, the process window was obtained according to the appearance of the milling hole. Afterwards, the response surface method (RSM) was utilized to analyze the influence of the process parameters on the opening quality.
(1)
where D is the designed diameter of the hole and Dmax is the actual diameter.3. Results
3.1. Determining the Process Window
As seen in Figure 4, under the spindle speed of 6000 r/min and feed speed 800 mm/min, the four milling tools had different defects. The single-edged milling cutters, double-edged milling cutters, and PCB alloy drill had many burrs and serious fiber delamination. For the corn milling cutter, no visual severe delamination was found and relatively less burrs appeared compared with the other three tools. Loja et al. [11] used four drilling tools to evaluate the delamination and maximum temperature caused by drilling in fiberglass laminates. For milling cutters and twist drills, the higher the drilling speed, the higher the temperature generated by friction, and the greater the damage to the aperture. The experimental results and literature data have certain commonality. The quality of the milling effect of the corn milling cutter was better than that of the spiral milling cutter and twist drill. The subsequent experiment was conducted by the corn milling cutter.
In this step, spindle speed and feed speed were varied from 700 r/min to 24,000 r/min and 300 mm/min to 1500 mm/min, respectively, as listed in Table 1. A total of 27 groups of experiments were made and two holes were milled under each group of parameters to ensure the results. The influence of the process parameters on milling property is shown in Figure 5, where three typical situations known as tool fracture, delamination and burr were found. When the spindle speed was too low, 700 r/min, tool fracture appeared. When the spindle speed was lower than 3000 r/min, the delamination of fibers near the hole was found. On the contrary, the burr became dominant when the spindle speed was higher than 6000 r/min. Between the range of 3000 r/min to 6000 r/min was the transition zone where delamination and burr coexisted. From Figure 6, three combinations of processing parameters named F1–S2, F3–S5, and F6–S9 were selected as the thermal-imaging objects. It was shown in Figure 6 that with the increase in the spindle speed and feed speed, the maximum temperature increases, but the maximum temperature was 49.3 °C below the melting temperature of PP.
3.2. Optimizing the Process Parameters
Based on the above process window, the process parameters were refined. Feed speed was chosen as 1200 mm/min, 1500 mm/min, and 1800 mm/min, and the spindle speed was chosen as 12,000 r/min, 18,000 r/min, and 24,000 r/min. The response-surface-method analysis was carried out to determine the optimal process parameters. The factor-level design table is shown in Table 2 with two factors and three levels. The experimental trials were design as in Table 3 with the corresponding characterization variables named delamination factor and burr area. It can be seen that with the change in the processing parameters, the delamination factor is the lowest at 1.0046 and the highest at 1.0374. Taking the delamination factor as the dependent variable and the specific level of each factor as the independent variable, the quadratic regression equation was established to obtain the following results as Equation (2):
(2)
The significance analysis of each item in the quadratic regression equation is shown in Table 4. It shows that under the selected experimental interval, the F value of this model is 15.21628 and the probability of data error is 1.04%. The analysis of variance for the model is shown in Table 5, showing that 95% of the experimental data can be explained by this model. Adj R2 and Pred R2 had higher values and the difference was within 0.2, indicating that the regression model can fully fit the test results. However, Table 6 shows that the relationship between burr area and the model was not significant, although the burr area decreased with the increase in the processing parameters.
From the above, it can be concluded that when the machining parameters were low, the hole quality was not ideal. With the increase in the spindle speed and feed speed, the hole quality was gradually improved. When the machining parameters were increased to a certain range, the effect of improving the quality of the opening became weaker. The results of the response surface method show that when the spindle speed was 18,000 r/min and the feed speed was 1500 mm/min, the hole quality was the best, and the delamination factor and the burr area were both the minimum.
4. Conclusions
In this paper, GFRPP laminates were taken as the research object to investigate the effects of different cutters and process parameters on the hole quality. The specific conclusions are as follows:
(1). Different tools have a great influence on the hole quality, and the corn milling cutter used for GFRPP laminates has the best opening quality.
(2). In the selected region, with the increase in spindle speed and feed speed, the change in temperature distribution in the entry surface near the hole is not significant, and the maximum temperature does not reach the resin-melting temperature.
(3). Using the delamination factor and burr area to represent the hole quality is feasible. The quadratic regression model is significant for delamination factor while insignificant for burr area. The reason is because that the calculation of the burr area is greatly affected by the experimental error.
(4). In the milling of presented GFRPP laminate, the best hole quality is achieved when the spindle speed is 18,000 r/min and the feed speed is 1500 mm/min with the corn milling cutter.
Conceptualization, H.H., B.D. and L.C.; Data curation, X.Z. (Xiaodong Zhang) and Z.W.; Funding acquisition, B.D.; Investigation, C.N. and X.Z. (Xiaodong Zhang); Methodology, H.H. and X.Z. (Xianjun Zeng); Resources, Z.W. and Y.X.; Software, C.N. and Y.X.; Validation, C.N.; Visualization, X.Z. (Xianjun Zeng); Writing—original draft, H.H.; Writing—review & editing, B.D. and L.C. All authors have read and agreed to the published version of the manuscript.
This research was funded by Chongqing Natural Science Foundation (cstc2020jcyj-msxmX0559), Science and Technology Research Program of Chongqing Municipal Education Commission (KJQN202101531), Research Foundation (ckrc2019024) and College Students Science and Technology Innovation Training Program (2021194) of Chongqing University of Science and Technology.
Not applicable.
Not applicable.
The data presented in this study are available on request from the corresponding author.
The authors declare no conflict of interest.
Publisher’s Note: MDPI stays neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Figure 1. Schematic of cutting tools: (a) Single-edge milling cutter; (b) Double-edge milling cutter; (c) Corn milling cutter; (d) PCB alloy drill.
Figure 3. Schematic diagram of evaluation parameters: (a) Delamination factor; (b) Burr area.
Figure 4. Morphology of milling holes: (a) Single-edge milling cutter; (b) Double-edge milling cutter; (c) Corn milling cutter; (d) PCB alloy drill.
Number of process parameters.
| Feeding Speed |
No. | Spindle Speed |
No. |
|---|---|---|---|
| 300 | F1 | 700 | S1 |
| 600 | F2 | 1400 | S2 |
| 900 | F3 | 2000 | S3 |
| 1200 | F4 | 3000 | S4 |
| 1500 | F5 | 6000 | S5 |
| 1800 | F6 | 10,000 | S6 |
| 12,000 | S7 | ||
| 18,000 | S8 | ||
| 24,000 | S9 |
Factor-level design table of response surface method.
| Level | A: Feeding Speed |
B: Spindle Speed |
|---|---|---|
| −1 | 2000 | 300 |
| 0 | 10,000 | 900 |
| 1 | 18,000 | 1500 |
Design and test results of response surface method.
| No. | A: Spindle Speed |
B: Feeding Speed |
Delamination Factor | Burr Area |
|---|---|---|---|---|
| 1 | 2000 | 300 | 1.0352 | 15.17 |
| 2 | 18,000 | 300 | 1.0237 | 23.67 |
| 3 | 2000 | 1500 | 1.0374 | 25.07 |
| 4 | 18,000 | 1500 | 1.0046 | 8.94 |
| 5 | 2000 | 900 | 1.0322 | 30.94 |
| 6 | 18,000 | 900 | 1.0173 | 17.54 |
| 7 | 10,000 | 300 | 1.0313 | 20.67 |
| 8 | 10,000 | 1500 | 1.0158 | 12.99 |
| 9 | 10,000 | 900 | 1.0179 | 21.11 |
| 10 | 10,000 | 900 | 1.0179 | 24.49 |
Significance analysis of delamination factor.
| Source | Sum of Squares | d f | Mean Square | F-Value | p-Value |
|
|---|---|---|---|---|---|---|
| Model | 0.000934 | 5 | 0.000187 | 15.21628 | 0.0104 | significant |
| A–Spindle speed | 0.000585 | 1 | 0.000585 | 47.66917 | 0.0023 | |
| B–Feeding speed | 0.000175 | 1 | 0.000175 | 14.23207 | 0.0196 | |
| AB | 0.000112 | 1 | 0.000112 | 9.159819 | 0.0389 | |
| A 2 | 3.53 × 10−5 | 1 | 3.53 × 10−5 | 2.871886 | 0.1654 | |
| B 2 | 1.66 × 10−5 | 1 | 1.66 × 10−5 | 1.352159 | 0.3095 | |
| Residual | 4.91 × 10−5 | 4 | 1.23 × 10−5 | |||
| Lack of Fit | 4.91 × 10−5 | 3 | 1.64 × 10−5 |
ANOVA results of delamination factor.
| R 2 | Adj R2 | Pred R2 | Adeq Precisior |
|---|---|---|---|
| 0.9501 | 0.8876 | 0.5152 | 11.254 |
Significance analysis of burr area.
| Source | Sum of Squares | d f | Mean Square | F-Value | p-Value |
|
|---|---|---|---|---|---|---|
| Model | 335.7867 | 5 | 67.15734 | 5.901067 | 0.0551 | not significant |
| A–Spindle speed | 73.70933 | 1 | 73.70933 | 6.476785 | 0.0636 | |
| B–Feeding speed | 26.07555 | 1 | 26.07555 | 2.29124 | 0.2047 | |
| AB | 151.5951 | 1 | 151.5951 | 13.32055 | 0.0218 | |
| A 2 | 4.637278 | 1 | 4.637278 | 0.407474 | 0.5580 | |
| B 2 | 84.00382 | 1 | 84.00382 | 7.381355 | 0.0532 | |
| Residual | 45.52217 | 4 | 11.38054 | |||
| Lack of Fit | 39.81506 | 3 | 13.27169 | 2.325465 | 0.4412 | not significant |
References
1. Xing, L.Y.; Bao, J.W.; Li, S.M.; Chen, X.B. Development status and facing challenge of advanced polymer matrix composites. Acta Mater. Compos. Sin.; 2016; 33, pp. 1327-1338.
2. Wu, L.H.; Yuan, Y.H. Applications of advanced fiber-reinforced composite materials in large commercial aircraft. Ordnance Mater. Sci. Eng.; 2018; 41, pp. 100-103.
3. Thoppul, S.D.; Finegan, J.; Gibson, R.F. Mechanics of mechanically fastened joints in polymer–matrix composite structures—A review. Compos. Sci. Technol.; 2009; 69, pp. 301-329. [DOI: https://dx.doi.org/10.1016/j.compscitech.2008.09.037]
4. Jia, Z.Y.; Bi, G.J.; Wand, F.J.; Wang, X.N.; Zhang, B.Y. The research of machining mechanism of carbon fiber reinforced plastic. J. Mech. Eng.; 2018; 54, pp. 199-208. [DOI: https://dx.doi.org/10.3901/JME.2018.23.199]
5. Prasad, K.S.; Chaitanya, G. Analysis of delamination in drilling of GFRP composites using Taguchi Technique. Mater. Today: Proc.; 2019; 18, pp. 3252-3261. [DOI: https://dx.doi.org/10.1016/j.matpr.2019.07.201]
6. Hrechuk, A.; Bushlya, V.; Ståhl, J.-E. Hole-quality evaluation in drilling fiber-reinforced composites. Compos. Struct.; 2018; 204, pp. 378-387. [DOI: https://dx.doi.org/10.1016/j.compstruct.2018.07.105]
7. Liu, S.; Yang, T.; Liu, C.; Jin, Y.; Sun, D.; Shen, Y. Modelling and experimental validation on drilling delamination of aramid fiber reinforced plastic composites. Compos. Struct.; 2020; 236, 111907. [DOI: https://dx.doi.org/10.1016/j.compstruct.2020.111907]
8. Amaro, A.M.; Reis, P.N.B.; de Moura, M.; Neto, M.A. Influence of open holes on composites delamination induced by low velocity impact loads. Compos. Struct.; 2013; 97, pp. 239-244. [DOI: https://dx.doi.org/10.1016/j.compstruct.2012.09.041]
9. Tsao, C.C.; Kuo, K.L.; Hsu, I.C. Evaluation of novel approach on delamination factor after drilling composite laminates. Key Engineering Materials; Trans Tech Publications Ltd.: Zurich, Switzerland, 2010; 443, pp. 626-630.
10. Sugita, N.; Shu, L.; Kimura, K.; Arai, G.; Arai, K. Dedicated drill design for reduction in burr and delamination during the drilling of composite materials. CIRP Ann.; 2019; 68, pp. 89-92. [DOI: https://dx.doi.org/10.1016/j.cirp.2019.04.094]
11. Loja, M.A.R.; Alves, M.S.F.; Bragança, I.M.F.; Rosa, R.S.B.; Barbosa, I.C.J.; Barbosa, J.I. An assessment of thermally influenced and delamination-induced regions by composites drilling. Compos. Struct.; 2018; 202, pp. 413-423. [DOI: https://dx.doi.org/10.1016/j.compstruct.2018.02.046]
12. Velaga, M.; Cadambi, R.M. Drilling of GFRP composites for minimising delamination effect. Mater. Today Proc.; 2017; 4, pp. 11229-11236. [DOI: https://dx.doi.org/10.1016/j.matpr.2017.09.044]
13. Guo, H.B. Analysis of Formation Mechanism and Restraining Methods of GFRPP Composites Drilling Damage. Master’s Dissertation; Dalian University of Technology: Dalian, China, 2018.
14. Mustari, A.; Chakma, P.; Sobhan, R.; Dhar, N. Investigation on roundness and taper of holes in drilling GFRP composites with variable weight percentages of glass fiber. Mater. Today Proc.; 2020; 38, pp. 2578-2583. [DOI: https://dx.doi.org/10.1016/j.matpr.2020.07.685]
15. Patel, K.; Gohil, P.P.; Chaudhary, V. Investigations on drilling of hemp/glass hybrid composites. Mater. Manuf. Process.; 2018; 33, pp. 1714-1725. [DOI: https://dx.doi.org/10.1080/10426914.2018.1453150]
16. Palanikumar, K.; Srinivasan, T.; Rajagopal, K.; Latha, B. Thrust Force Analysis in Drilling Glass Fiber Reinforced/Polypropylene (GFR/PP) Composites. Mater. Manuf. Process.; 2014; 31, pp. 581-586. [DOI: https://dx.doi.org/10.1080/10426914.2014.961478]
17. Srinivasan, T.; Palanikumar, K.; Rajagopal, K. Roundness Error Evaluation in Drilling of Glass Fiber Reinforced Polypropylene (GFR/PP) Composites Using Box Behnken Design (BBD). Applied Mechanics and Materials; Trans Tech Publications Ltd.: Zurich, Switzerland, 2015; 766–767, pp. 844-851. [DOI: https://dx.doi.org/10.4028/www.scientific.net/amm.766-767.844]
18. Srinivasan, T.; Palanikumar, K.; Rajagopal, K. Influence of Process Parameters on Delamination of Drilling of (GF/PC) Glass Fiber Reinforced Polycarbonate Matrix Composites. Adv. Mater. Res.; 2014; 984–985, pp. 355-359. [DOI: https://dx.doi.org/10.4028/www.scientific.net/AMR.984-985.355]
19. Du, B.; Chen, L.M.; Liu, H.C.; He, Q.H.; Li, W.G. Resistance Welding of Glass Fiber Reinforced Thermoplastic Composite: Ex-perimental Investigation and Process Parameter Optimization. Chin. J. Aeronaut.; 2020; 33, pp. 3469-3478. [DOI: https://dx.doi.org/10.1016/j.cja.2020.02.018]
20. Sorrentino, L.; Turchetta, S.; Bellini, C. In process monitoring of cutting temperature during the drilling of FRP laminate. Compos. Struct.; 2017; 168, pp. 549-561. [DOI: https://dx.doi.org/10.1016/j.compstruct.2017.02.079]
21. Hou, G.; Luo, B.; Zhang, K.; Luo, Y.; Cheng, H.; Cao, S.; Li, Y. Investigation of high temperature effect on CFRP cutting mechanism based on a temperature controlled orthogonal cutting experiment. Compos. Struct.; 2021; 268, 113967. [DOI: https://dx.doi.org/10.1016/j.compstruct.2021.113967]
22. Giasin, K.; Ayvar-Soberanis, S. Evaluation of Workpiece Temperature during Drilling of GLARE Fiber Metal Laminates Using Infrared Techniques: Effect of Cutting Parameters, Fiber Orientation and Spray Mist Application. Materials; 2016; 9, 622. [DOI: https://dx.doi.org/10.3390/ma9080622] [PubMed: https://www.ncbi.nlm.nih.gov/pubmed/28773757]
You have requested "on-the-fly" machine translation of selected content from our databases. This functionality is provided solely for your convenience and is in no way intended to replace human translation. Show full disclaimer
Neither ProQuest nor its licensors make any representations or warranties with respect to the translations. The translations are automatically generated "AS IS" and "AS AVAILABLE" and are not retained in our systems. PROQUEST AND ITS LICENSORS SPECIFICALLY DISCLAIM ANY AND ALL EXPRESS OR IMPLIED WARRANTIES, INCLUDING WITHOUT LIMITATION, ANY WARRANTIES FOR AVAILABILITY, ACCURACY, TIMELINESS, COMPLETENESS, NON-INFRINGMENT, MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. Your use of the translations is subject to all use restrictions contained in your Electronic Products License Agreement and by using the translation functionality you agree to forgo any and all claims against ProQuest or its licensors for your use of the translation functionality and any output derived there from. Hide full disclaimer
© 2022 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
Abstract
The composite-material laminate structure will inevitably encounter connection problems in use. Among them, mechanical connections are widely used in aerospace, automotive and other fields because of their high connection efficiency and reliable connection performance. Milling parameters are important for the opening quality. In this paper, continuous-glass-fiber-reinforced-polypropylene (GFRPP) laminates were chosen to investigate the effects of different cutters and process parameters on the hole quality. The delamination factor and burr area were taken as the index to characterize the opening quality. After determining the optimal milling tool, the process window was obtained according to the appearance of the milling hole. In the selected process parameter, the maximum temperature did not reach the PP melting temperature. The best hole quality was achieved when the spindle speed was 18,000 r/min and the feed speed was 1500 mm/min with the corn milling cutter.
You have requested "on-the-fly" machine translation of selected content from our databases. This functionality is provided solely for your convenience and is in no way intended to replace human translation. Show full disclaimer
Neither ProQuest nor its licensors make any representations or warranties with respect to the translations. The translations are automatically generated "AS IS" and "AS AVAILABLE" and are not retained in our systems. PROQUEST AND ITS LICENSORS SPECIFICALLY DISCLAIM ANY AND ALL EXPRESS OR IMPLIED WARRANTIES, INCLUDING WITHOUT LIMITATION, ANY WARRANTIES FOR AVAILABILITY, ACCURACY, TIMELINESS, COMPLETENESS, NON-INFRINGMENT, MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. Your use of the translations is subject to all use restrictions contained in your Electronic Products License Agreement and by using the translation functionality you agree to forgo any and all claims against ProQuest or its licensors for your use of the translation functionality and any output derived there from. Hide full disclaimer
Details
1 School of Aeronautics, Chongqing Jiaotong University, Chongqing 400074, China;
2 Chongqing Key Laboratory of Nano–Micro Composite Materials and Devices, School of Metallurgy and Materials Engineering, Chongqing University of Science and Technology, Chongqing 401331, China;
3 Chongqing Key Laboratory of Nano–Micro Composite Materials and Devices, School of Metallurgy and Materials Engineering, Chongqing University of Science and Technology, Chongqing 401331, China;
4 The Green Aerotechnics Research Institute of CQJTU, Chongqing 401120, China;
5 College of Aerospace Engineering, Chongqing University, Chongqing 400030, China




