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All Journal Al-Fiziya: Journal of Materials Science, Geophysics, Instrumentation and Theoretical Physics JPP IPTEK (Jurnal Pengabdian dan Penerapan IPTEK) Teknika STTKD: : Jurnal Teknik, Elektronik, Engine Jurnal Ilmiah Teknik Mesin, Elektro dan Komputer (JURITEK) Journal of Applied Mechanical Engineering and Renewable Energy (JAMERE) INJECTION: Indonesian Journal of Vocational Mechanical Engineering Jurnal Mahasiswa Kreatif Journal of Education Transportation and Business
Ferry Setiawan
Sekolah Tinggi Teknologi Kedirgantaraan (STTKD) Yogyakarta
Religion Agriculture, Biological Sciences & Forestry Humanities Automotive Engineering Chemical Engineering, Chemistry & Bioengineering Civil Engineering, Building, Construction & Architecture Computer Science & IT Control & Systems Engineering Decision Sciences, Operations Research & Management Earth & Planetary Sciences Economics, Econometrics & Finance Education Electrical & Electronics Engineering Energy Engineering Environmental Science Industrial & Manufacturing Engineering Languange, Linguistic, Communication & Media Law, Crime, Criminology & Criminal Justice Materials Science & Nanotechnology Mechanical Engineering Physics Public Health Social Sciences Transportation Other

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PERENCANAAN PREVENTIVE MAINTENANCE MENGGUNAKAN METODE RELIABILITY PADA ELECTRICAL SISTEM AUXILIARY POWER UNIT BOEING 737-500 Ferry Setiawan; Mohammed Taaqbier; Muh Anhar
Injection: Indonesian Journal of Vocational Mechanical Engineering Vol 2 No 1 (2022): Februari 2022
Publisher : Politeknik Negeri Ketapang

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (512.673 KB) | DOI: 10.58466/injection.v2i1.279

Abstract

Electrical sistem Auxiliary Power Unit pada pesawat Boing 737-500 sering mengalami kegagalan operasional karena adanya kerusakan pada komponen di dalam sistem tersebut, kejadian ini menimbulkan kerugian operasional yang cukup besar sehingga diperlukan sebuah metode perawatan yang tepat untuk menghilangkan faktor – faktor penyebab kegagalan pada Electrical sistem Auxiliary Power Unit. Tujuan penelitian ini adalah merencanakan aktivitas preventive maintenance pada Electrical sistem Auxiliary Power Unit sehingga kerusakan part yang menyebabkan terjadinya kegagalan dapat ditanggulangi dengan baik. Metode reliability dihitung menggunakan distribusi Weibull sehingga didapatkan batas kritis waktu operasional pada Electrical sistem Auxiliary Power Unit. Dari hasil perhitungan didapatkan Batas kritis operasional Electrical sistem Auxiliary Power Unit adalah 271 flight cycle dengan kerusakan utama adalah pada komponen start Relay, dengan kegiatan maintenance berupa aktivitas Inspection, repair, testing dan cleaning.
Uji Impact Material Komposit Campuran Serat Bambu Dan Pasir Besi Menggunakan Metode Hand Lay Up Ferry Setiawan; Dendy Syaputra Pratama; Rio Saputra Lubis; Edy Sofyan
Journal of Applied Mechanical Engineering and Renewable Energy Vol 3 No 1: Februari2023
Publisher : Indonesian Society of Applied Science

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.52158/jamere.v3i1.399

Abstract

A composite is one of the materials that is a mixture of two or more materials to form a third, more useful material. In this study, researchers chose bamboo fiber and iron sand as reinforcement for composite materials because the selection of bamboo fiber as a research material took into account the potential of bamboo fiber in Indonesia which is abundant and has not been utilized properly. The purpose of making bamboo fibrous composite materials aims to find a material that is lighter stronger and more elastic, can be developed into other products such as the manufacture of drone frames, aircraft bodies, brake pads. The method used is an experiment with making specimens using the hand lay up method and testing using impact testing and micro photo testing. Impact testing is used to determine the properties and characteristics of the material in the form of strength, hardness, and ductility of the material while for micro photos it is used to determine the bond of the material composition with the best impact test. The test standards used are ASTM D6110-10 with random fiber arrangement and ASTM D6110-04 with the arrangement of woven fibers, with variations in volume composition of bamboo fiber and iron sand particles. In the D6110-10 specimens, the best specimens were found in the variation with the most bamboo fibers, namely 35S10 P with an impact energy of 4.27 J and an impact price of 0.04 J / mm2, while the lowest variation was found in the most iron sand, namely 35P10S with an impact energy value of 2.26 J and an impact price of 0.02 J / mm2. In the D6110-04 specimen also showed the same characteristics as the ASTM D6110-10 specimen, the 30S30P variation or the composition of the most bamboo fibers had an impact energy value of 4.09 J while in the 10S10P variation it was only 1.47 J. Thus the more bamboo fibers will make the impact strength of the specimen higher.
ANALISIS PENGARUH PELAPISAN NIKEL PADA MATERIAL ALUMINIUM SERI 2024 TERHADAP KEKUATAN TARIK DAN KEKERASAN DENGAN METODE ELEKTROPLATING Fatir Slametriadi Fatir; Sehono; Ferry Setiawan
Teknika STTKD: : Jurnal Teknik, Elektronik, Engine Vol 9 No 1 (2023): TEKNIKA STTKD: JURNAL TEKNIK, ELEKTRONIK, ENGINE
Publisher : Sekolah Tinggi Teknologi Kedirgantaraan

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.56521/teknika.v9i1.611

Abstract

Aluminum alloy in the aerospace field has been widely used in the manufacture of skins from aircraft. The use of aluminum alloy has the advantages of relatively high mechanical strength and resistance to corrosion. In order to raise the strength of the material and the physical appearance of aluminum can use the electroplating method. Electroplating is a method used to coat metals with other types of metals, the coating process uses the help of electric current. The electric current used will trigger the release of metal ions at the anode to be further attached to the cathode. In this study, an electroplating process was carried out on 2024 aluminum alloy specimens with nickel coating. The variations in this study used differences in electric current voltages of 25 V, 35 V, and 45 V. Then to find out the differences from the variations that have been used, tensile tests and hardness tests were carried out. From the results of the tensile test, it shows that the higher the voltage of the electric current used, it will increase the tensile strength, but the yield strength will decrease. The highest tensile strength is found in the voltage variation of 45 V with a value of 452.53 MPa. Then on the hardness test shows that the higher the voltage of the electric current will reduce the hardness value. The highest hardness value is found at a voltage of 25 V with a value of 963.594.
PENGARUH VARIASI SUHU TERHADAP KEKUATAN MEKANIKA PADA ALUMUNIUM 7075-T6 DENGAN METODE ELEKTROPLATING Hardinus Apriantoni; Gaguk Marausna; Ferry Setiawan
Teknika STTKD: : Jurnal Teknik, Elektronik, Engine Vol 9 No 1 (2023): TEKNIKA STTKD: JURNAL TEKNIK, ELEKTRONIK, ENGINE
Publisher : Sekolah Tinggi Teknologi Kedirgantaraan

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.56521/teknika.v9i1.779

Abstract

Aluminum alloy 7075 series is one that is widely used in the aviation industry. More than 73% of aircraft components are aluminum alloy 7075 series because the properties of this aluminum can still be improved by giving it a treatment. The purpose of this study was to determine the effect of differences in nickel coating types on 7075-T6 aluminum plates on the level of hardness.aluminum plates with a length of 2 cm and a width of 2 cm as many as each variation of 4 specimens. temperature variations of 30 °C, 35 °C, 40 °C, 45 °C and time of 5, 10, 15, 20 minutes. The hardness value is obtained using a brinell test device, using a diamond pyramid indenter used for vickers hardness tests. The test object is pressed for 5 seconds with a load of 31.25 kgf and a magnification of 5 times. Hardness testing is carried out at 1 point of the surface of the specimen. Based on the results of research and calculations and discussions about the effect of temperature variations on the strength of mechanics by the electroplating method, it is known that the difference in time and temperature variations on the hardness of aluminum 7075-T6 shows an influence on the value of significant hardness. And the optimal variation value was obtained, namely the highest hardness value at a temperature of 45 ° C at a time of 5 minutes, namely 483.63 kgf / mm² and the lowest average hardness value at a temperature of 30 ° C at a 15-minute immersion time of 292.33 kgf / mm².
Testing the Bending Strength of Carbon Fiber Composites using the vacuum infusion and vacuum bagging method on the UAV Skywalker 1900 Fuselage Material Chandra Febriyanto; Ferry Setiawan; Ikbal Rizki Putra
Al-Fiziya: Journal of Materials Science, Geophysics, Instrumentation and Theoretical Physics AL-FIZIYA JOURNAL OF MATERIALS SCIENCE, GEOPHYSICS, INSTRUMENTATION AND THEORETICAL PHYSICS VOL.6, N
Publisher : Physics Study Programme, Faculty of Science and Technology UIN Syarif Hidayatullah Jakarta

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.15408/fiziya.v6iI.30562

Abstract

The purpose of this study was to determine the bending strength of carbon fiber composite materials with lycal epoxy resin on the Skywalker 1900 UAV. Composites will be made for test specimens with carbon fiber combined with lycal resin using vacuum infusion printing and vacuum bagging methods. From these two methods a sample of specimens will be made for testing using a bending test using the three point bending method to determine the bending strength value of the fuselage material. As for another test, namely microphotos, the process of observing this microstructure can find out how the shape, size, and distribution of second phase particles have an important role in knowing the properties of the material itself. The results of the test specimens were compared between vacuum infusion printing and vacuum bagging and then the best value was sought between the two methods. The results were obtained after testing where the two methods of printing and micro-photos obtained the best results in vacuum bagging. In the vacuum bagging process, the highest value was found in specimen b2 with a bending stress value of 1201.90Mpa and the lowest yield was found in specimen i1 with a bending stress value of 1017.74Mpa. Then the micro photo test can be seen in the vacuum bagging printing process, the penetration of the resin in bagging to the fiber is better.
Menghitung Besar Biaya (Cost) Dari Perancangan Perawatan Menggunakan Metode Reliability Centered Maintenance Pada Fuel Boost Pump Pesawat Boeing 737-400 Octaline Putri Efma; Reo Yudhono; Arfie Armelia Erissonia; Ferry Setiawan
Jurnal Mahasiswa Kreatif Vol. 1 No. 5 (2023): September : Jurnal Mahasiswa Kreatif
Publisher : Universitas Katolik Widya Karya Malang

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.59581/jmk-widyakarya.v1i5.1199

Abstract

This study aims to know the cost of designing maintenance using the Reliability Centered Maintenance method. Engine and fuel control, is a fuel engine system and fuel control system; in charge of distributing and measuring fuel from the fuel storage tank, to the combustion chamber. Gas turbine or component area (Combustor), functions as a distributor of fuel used in aircraft systems and plays a role in carrying out its operation (Boeing 737-400 Aircraft Maintenance Manual). Reliability is the possibility of a component or system to be able to operate and/or carry out its functions. The function has been assigned to certain operating conditions and in a certain environment for a predetermined period of time. Thus, reliability is the probability that it will not fail or be able to perform its function for a period of time (t) or more. In the analysis of preventive maintenance financing, which is carried out when the reliability value reaches 70%, 60% and 50%, respectively, it is obtained for each component.
Manufaktur Vacuum Resin Infusion Untuk Pembuatan Material Komposit Ilham Romdhani; Ferry Setiawan; Dimas Wicaksono
Journal of Education Transportation and Business Vol 1, No 2 (2024): Desember 2024
Publisher : CV. Rayyan Dwi Bharata

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.57235/jetbus.v1i2.3677

Abstract

Penggunaan material komposit dalam industri penerbangan semakin meningkat, menggantikan baja dan aluminium. Metode Vacuum Resin Infusion yang lebih efisien dibandingkan metode tradisional seperti Hand Lay-Up telah dikembangkan untuk meningkatkan kualitas dan menurunkan biaya produksi komposit yang digunakan pada struktur pesawat, UAV, dan drone. Penelitian ini menggunakan metode eksperimental dengan dua teknik pembuatan komposit: Vacuum Infusion dan Hand Lay-Up. Spesimen dibuat menggunakan variasi pipa spiral pada metode Vacuum Infusion. Pengujian meliputi evaluasi void menggunakan foto mikroskop dan pengukuran berat jenis material untuk membandingkan kualitas komposit yang dihasilkan oleh kedua metode tersebut. Mengetahui perbedaan kualitas material komposit yang dihasilkan oleh metode Vacuum Infusion dan Hand Lay-Up berdasarkan void dan berat jenisnya. Metode Vacuum Infusion dengan spiral out menunjukkan jumlah void paling sedikit dan nilai berat jenis tertinggi sebesar 0.00157 gram/mm³ dibandingkan dengan metode lain, menunjukkan bahwa metode ini menghasilkan komposit dengan kualitas dan kerapatan yang lebih baik, sehingga lebih unggul dalam hal kekuatan dan ketahanan material.
Co-Authors Aldo novando Aldo novando Arfie Armelia Erissonia Chandra Febriyanto Dendy Syaputra Pratama Dhimas Wicaksono Dimas Wicaksono Dwi Muridha C. Putra Edi Sofyan Edi Sofyan Edy Sofyan Faisal Romadhon Farid Jayadi Fatir Slametriadi Fatir Galang Anugrah Pratama Galang Hardinus Apriantoni Haris Ardianto Ilham Romdhani Marausna, Gaguk Mirhan Hadi Mohammed Taaqbier Mohammed Taaqbier Muh Anhar Muhammad Iqbal Aizi Iqbal Nicolaus Ardi Kurniawan Octaline Putri Efma Putra, Ikbal Rizki Rahmat Dwi Handoko Reo Yudhono Rio Saputra Lubis Sehono