Hasil Pencarian  ::  Simpan CSV :: Kembali

"[Penelitian ini bertujuan untuk mengetahui pengaruh kekasaran, proses phosphating, serta ketebalan adhesive bonding terhadap ketahanan delaminasi komposit laminat. Variasi kekasaran substrat, yaitu pada rentang 5-8 μm dan 10-13 μm, variasi terhadap proses phosphating, yaitu ada yang melalui proses phosphating dan ada yang tidak, serta variasi ketebalan adhesive baik primer ataupun topcoat dengan rentang 1-5 μm, 6-10 μm, serta 11-15 μm. Pembentukan komposit laminat ini dilakukan melalui proses transfer moulding pada suhu 160 C selama 450 detik. Komposit laminat yang sudah terbentuk kemudian diuji peel-off untuk mengetahui kekuatan delaminasinya lalu dikarakterisasi dengan SEM-EDX. Hasil menunjukan bahwa kekasaran permukaan, lapisan zinc phosphate, serta ketebalan adhesive bonding mempengaruhi ketahanan delaminasi komposit laminat yang diinterpretasikan dengan kekuatan ikat antarlapisan dan visual delaminasi. Kekasaran optimum terjadi pada rentang 10-13 μm dengan kekuatan ikat 179,68 N dan visual delaminasi R-R sebanyak 35%. Adanya lapisan zinc phosphate memberikan nilai kekuatan ikat optimum sebesar 157,38 N dan visual delaminasi R-R sebanyak 50%. Ketebalan adhesive primer optimum terjadi pada rentang 1-5 μm dengan kekuatan ikat 163,35 N dan visual delaminasi R-R sebanyak 50%. Ketebalan adhesive topcoat optimum terjadi pada rentang 6-10 μm dengan kekuatan ikat sebesar 154,65 N dan visual delaminasi R-R sebanyak 41,6%.;This study aims to determine the effect of roughness, phosphating process, and the thickness of the adhesive bonding into delamination resistance of laminate composite. Variation of the substrate roughness are 5-8 μm and 10-13 μm. Some substrates are coated by zinc phosphate and other substrate are uncoated. Variations of the thickness of adhesive primer and adhesive topcoat are in a range of 1-5 μm, 6-10 μm, and 11-15 μm. The process of forming the laminate composite occurs through transfer molding process at 1600C in 450 seconds. Laminate composite that has been formed then tested by peel-off test to determine the strength of delamination. Visual of delamination was characterized by SEM-EDX. The results showed that the optimum surface roughness occurs in the range of 10-13 μm with bonding strength 179.68 N and 35% of R-R visual. The coated substrate has a higher bonding strength compared to uncoated substrate, which is 157.38 N and 50% of R-R visual. The optimum thickness of adhesive primer occurs in the range of 1-5 μm with bonding strength is 163.35 N and 50% of R-R visual. While the optimum thickness of adhesive topcoat occurs in the range of 6-10 μm with a bonding strength is 154.65 N and 41,6% of R-R visual;This study aims to determine the effect of roughness, phosphating process, and the thickness of the adhesive bonding into delamination resistance of laminate composite. Variation of the substrate roughness are 5-8 μm and 10-13 μm. Some substrates are coated by zinc phosphate and other substrate are uncoated. Variations of the thickness of adhesive primer and adhesive topcoat are in a range of 1-5 μm, 6-10 μm, and 11-15 μm. The process of forming the laminate composite occurs through transfer molding process at 1600C in 450 seconds. Laminate composite that has been formed then tested by peel-off test to determine the strength of delamination. Visual of delamination was characterized by SEM-EDX. The results showed that the optimum surface roughness occurs in the range of 10-13 μm with bonding strength 179.68 N and 35% of R-R visual. The coated substrate has a higher bonding strength compared to uncoated substrate, which is 157.38 N and 50% of R-R visual. The optimum thickness of adhesive primer occurs in the range of 1-5 μm with bonding strength is 163.35 N and 50% of R-R visual. While the optimum thickness of adhesive topcoat occurs in the range of 6-10 μm with a bonding strength is 154.65 N and 41,6% of R-R visual, This study aims to determine the effect of roughness, phosphating process, and the thickness of the adhesive bonding into delamination resistance of laminate composite. Variation of the substrate roughness are 5-8 μm and 10-13 μm. Some substrates are coated by zinc phosphate and other substrate are uncoated. Variations of the thickness of adhesive primer and adhesive topcoat are in a range of 1-5 μm, 6-10 μm, and 11-15 μm. The process of forming the laminate composite occurs through transfer molding process at 1600C in 450 seconds. Laminate composite that has been formed then tested by peel-off test to determine the strength of delamination. Visual of delamination was characterized by SEM-EDX. The results showed that the optimum surface roughness occurs in the range of 10-13 μm with bonding strength 179.68 N and 35% of R-R visual. The coated substrate has a higher bonding strength compared to uncoated substrate, which is 157.38 N and 50% of R-R visual. The optimum thickness of adhesive primer occurs in the range of 1-5 μm with bonding strength is 163.35 N and 50% of R-R visual. While the optimum thickness of adhesive topcoat occurs in the range of 6-10 μm with a bonding strength is 154.65 N and 41,6% of R-R visual]"

"ABSTRAKInteraksi yang kompleks antar lamina pada suatu laminat saat mengalami beban tarik menyebabkan perbedaan kuat tarik dan jenis kerusakan pada komposit laminat karbon/epoksi dengan susunan lamina yang berbeda. Untuk mengetahui pengaruh susunan lamina terhadap kuat tarik dan jenis kerusakan komposit laminat, 5 komposit laminat dibuat dengan metode hand lay up dengan susunan (0)5, (0/0/90)s, (0/45/-45/901/2)s, (0/45/-45/90)s dan (0/90/-45/45)s. Hasil uji tarik menunjukkan kuat tarik dari komposit laminat (0)5, (0/0/90)s, (0/45/-45/901/2)s, (0/45/-45/90)s dan (0/90/-45/45)s secara berturut-turut adalah ( 1988,97 ± 156,69 ) MPa, ( 1745,47 ± 19,53 ) MPa, ( 929,70 ± 32,79 ) MPa, ( 992,82 ± 26,63 ) MPa dan ( 941,86 ± 24,21 ) MPa. Hasil pengamatan dengan mikroskop optik pada bagian pinggir komposit laminat menunjukkan bahwa kerusakan yang terjadi pada setiap komposit laminat adalah delaminasi, retak mikro matriks dan perpatahan serat.

---

ABSTRAKA complex interaction between lamina in laminate composites when receive an applied load causes different tensile strength values and types of damage on the carbon/epoxy laminate composites with different lamina stacking sequence. To know the effect of lamina stacking sequence on tensile strength value and the types of damage, five types of laminate composites were made by hand lay up method where the stacking sequence were (0)5, (0/0/90)s, (0/45/- 45/901/2)s, (0/45/-45/90)s dan (0/90/-45/45)s. The test results showed that the tensile strength value of the (0)5, (0/0/90)s, (0/45/-45/901/2)s, (0/45/-45/90)s and (0/90/-45/45)s laminates are ( 1988,97 ± 156,69 ) MPa, ( 1745,47 ± 19,53 ) MPa, ( 929,70 ± 32,79 ) MPa, ( 992,82 ± 26,63 ) MPa and ( 941,86 ± 24,21 ) MPa respectively. An observation with optical micrograph at the edge of laminate composites showed that the type of damages that occured on that laminates were delamination, matrix microcracking and fiber breakag"

"Penekanan setelah impak merupakan salah satu parameter penting pada komposit dengan penguat serat sebagai material struktur. Penelitian ini bertujuan untuk memperoleh nilai tekan sesudah impak dan kerusakannya pada komposit epoksi-kevlar, epoksi-gelas dan epoksi-hibrid-kevlar/gelas. Spesimen komposit difabrikasi dengan metode hand lay-up dengan variasi energi impak yang diberikan adalah 4 J, 8 J dan 15 J. Pengamatan dengan Through Transmission Ultrasonic setelah impak menunjukkan bahwa kerusakan yang terjadi adalah delaminasi. Komposit terbaik ditinjau dari nilai kuat tekan yang tinggi dan ukuran delaminasi yang paling kecil. Dapat dikatakan bahwa nilai kuat tekan tertinggi adalah epoksi-gelas yaitu sebesar 119,85 8,31 MPa.

---

Compression after impact is one of important parameter of fiber reinforced composites as structural materials. This research aimed to obtain the values of compression after impact and their resulting damage on kevlar epoxy, glass epoxy, and kevlar glass epoxy hybrid composites. The composite specimens were fabricated by a hand lay up method. These materials were experienced impact energy with a variation of 4 J, 8 J, and 15 J. Observation by Through Transmission Ultrasonic showed that the type of resulting damage after impact was delamination. From this research, the highest compressive strength and the smallest delamination belongs to the glass epoxy composite, with the value of 119,85 8,31 MPa as the highest value of compression strength."