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Analisis Uji Bending Pada Spesimen Serat Kulit Jagung Fiberglass Dengan Perpaduan Resin Lycal Menggunakan Variasi Metode Pembuatan Vacuum Bagging Dan Vacuum Infusion Setiawan, Ferry; Amri, Chairul; Suroso, Indreswari; Anhar, Muh
Journal of Applied Mechanical Engineering and Renewable Energy Vol 5 No 1: February 2025
Publisher : Indonesian Society of Applied Science

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.52158/jamere.v5i1.1062

Abstract

This research aims to analyze the bending strength of composite materials based on corn fiber and fiberglass with Lycal resin, which are produced using two methods, namely vacuum bagging and vacuum infusion.Composite materials are increasingly being used in various industries because of their light and strong haracteristics. In this research, corn fiber was chosen as a natural reinforcement material because of its abundant availability and economic potential, while fiberglass was used as additional reinforcement to increase the strength of the material.The composite manufacturing process is carried out using two different methods, namely vacuum bagging and vacuum infusion, which are then tested using the ASTM-D 790 standard to determine the mechanical characteristics of the material, especially in terms of its ability to withstand bending loads. Apart from the bending test, material density calculations were also carried out to compare the weight and density of the two manufacturing methods.The test results show that the vacuum infusion method producescomposites with higher flexural strength than vacuum bagging. This is caused by a more even distribution of resin and minimal air trapped in the material structure during the vacuum infusion process. The composite produced from this method also has a lower density, making it lighter but still mechanically strong.It is hoped that this research can contribute to the development of natural fiber-based composite materials that are environmentally friendly and efficient, and have the potential to be applied to the aerospace industry, especially in the manufacture of UAV structures
DESAIN DAN MANUFAKTUR BOX VACUUM FORMING DENGAN FINITE ELEMENT ANALYSIS Nurdiana, Yuda; Wicaksono, Dhimas; Setiawan, Ferry
Teknika STTKD: : Jurnal Teknik, Elektronik, Engine Vol 11 No 1 (2025): 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.v11i1.1129

Abstract

One of the manufacturing techniques often used in industry to produce various forms of plastic components. The research stage begins with designing a box using Solidworks software, Analysis carried out on the vacuum forming box structure using finite element analysis. The results obtained are in the form of maximum stress that occurs, displacement and safety factor. The vacuum forming box structure is also subjected to a load of 51.878 N or equivalent to 5.2901 kg. The location of the force given to the vacuum forming box structure with a vertical force direction downwards, the displacement that occurs in the vacuum forming box structure with a force of 51.878 N. The largest displacement occurs at the top center of the vacuum forming box surface with a displacement of 0.75 mm. This happens because in that section the area is free or does not have a support in the middle. the safety factor value that occurs in the vacuum forming box structure with a force of 51.878 N. The safety factor value used in this analysis is 1.5. The safety factor value obtained in the vacuum box structure is 1.8. The safety factor value requirement used, then based on the data obtained, the vacuum box structure using plywood material is safe in receiving a load of 51,878 N, because the FOS value obtained is greater than the FOS standard used. In testing the tool using PET plastic with a temperature of 100 ℃ and a time of 30 seconds, the testing process begins with the preparation of the appropriate PET plastic and is placed on the part or mold of the tool to be tested. The temperature of the tool is heated to 100 ℃.
Analisis Kekuatan Tarik Dan Foto Mikro Spesimen Serat Jagung Menggunakan Resin Lycal Dengan Variasi Metode Pembuatan Vacuum Infusion Dan Vacuum Bagging Setiawan, Ferry; Dina Prasetia, Gilang; Suroso, Indreswari; Anhar, Muh
Journal of Applied Mechanical Engineering and Renewable Energy Vol 5 No 1: February 2025
Publisher : Indonesian Society of Applied Science

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.52158/jamere.v5i1.1108

Abstract

Along with the development of drone technology, the development of technology in the field of materials also plays a role in advancing drone technology, where the use of materials for making drones must meet certain criteria. The natural fiber as a composite material used in this study is corn husk fiber. The type of matrix used in this study is lycal resin. And making it using the vacuum infusion and vacuum bagging methods. In addition, microstructure testing is carried out to determine the content of the content contained in the low-carbon steel specimen to be tested. By using a test specimen that has been refined so that the content in the test object can be seen. The method in this study was made of a specimen of corn fiber with lycal resin using the vacuum infusion and vacuum bagging methods, then it will be tested using tensile and microstructure tests. The results of the characteristics of the corn fiber composite material with the vacuum infusion manufacturing method, from the tensile test obtained an average value of 7.3 MPa, and in the microstructure test it can be seen that the fracture occurred due to air bubbles trapped in the specimen and the uneven weaving distance so that it affects the tensile strength. Characteristics of corn fiber composite material with vacuum bagging manufacturing method: from the tensile test results obtained an average value of 15.13 MPa, and in the microstructure test it can be seen that the fiber density level and the vacuum bagging method can produce higher specimen quality compared to vacuum infusion.
Pemanfaatan Aplikasi Google Form dalam Kegiatan Serbuan Vaksinasi COVID-19 Berbasis Online di Kabupaten Klaten Wicaksono, Dhimas; Setiawan, Ferry
JPP IPTEK (Jurnal Pengabdian dan Penerapan IPTEK) Vol 6, No 1 (2022)
Publisher : Institut Teknologi Adhi Tama Surabaya

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.31284/j.jpp-iptek.2022.v6i1.3017

Abstract

Pengabdian kepada masyarakat ini dilakukan dengan tujuan memberikan solusi kepada panitia vaksinasi COVID-19 di Kabupaten Klaten. Pada awal pelaksanaan vaksin yang dilakukan secara konvensional mempunyai banyak kendala terutama pada lamanya waktu pendaftaran, validasi, dan penumpukan antrian peserta vaksinasi. Solusi yang diterapkan adalah dengan pemanfaatan aplikasi berbasis Google Form sebagai platform dalam pelaksanaan pendaftaran kegiatan Serbuan Vaksinasi COVID-19 yang dilaksanakan di Gedung Saroga KONI Kabupaten Klaten. Google Form adalah sebuah fitur dari Google yang digunakan sebagai formulir pendaftaran, kuesioner online, atau merencanakan sebuah acara. Pelaksanaan pengabdian ini terdiri dari dua kegiatan utama, yang pertama adalah pelatihan pembuatan form pendaftaran online menggunakan Google Form. Peserta akan otomatis mendapatkan nomor antrian dan kartu vaksinasi secara online yang langsung terkirim saat selesai pendafataran serta yang kedua adalah pelaksanaan kegiatan Serbuan Vaksinasi COVID-19. Dari beberapa wawancara dengan peserta vaksinasi, hasil yang didapatkan dari implementasi sistem form registrasi yang dibuat adalah sangat mudah digunakan dan peserta tidak terjadi kerumunan dalam vaksinasi karna jadwal dan kartu vaksinasi bisa dipantau dan dicetak menggunakan genggaman tangan (handphone) tanpa bingung ke mana pengambilan kartu bisa dilakukan. Bagi panitai pelaksanan vaksinasi, dengan menggunakan aplikasi berbasis Google Form juga memberi kemudahan pada pendataan peserta, validasi, penyimpanan data, dan mempercepat pelaksanaan kegiatan Serbuan Vaksinasi COVID-19.
ANALISA UNJUK KERJA HEATER PIPA KONSENTRIK DENGAN PENAMBAHAN VORTEX GENERATOR GUNA MENGATASI ICING Aldo novando, Aldo novando; Edi Sofyan; Ferry Setiawan
Jurnal Ilmiah Teknik Mesin, Elektro dan Komputer Vol. 2 No. 2 (2022): Juli: Jurnal Ilmiah Teknik Mesin, Elektro dan Komputer
Publisher : Pusat Riset dan Inovasi Nasional

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.51903/juritek.v2i2.310

Abstract

Horizontal stabilizer merupakan salah satu komponen terpenting dari pesawat terbang dalam mengontrol sikap terbang dari suatu pesawat. Sehingga jika horizontal stabilizer terganggu dalam mengontrol sikap terbang maka dapat menyebabkan pesawat kehilangan kestabilan. Pada horizontal stabilizer terdapat anti icing system yang digunakan untuk menjaga leading edge wing agar tidak terjadi kontaminasi pada saat pesawat sedang terbang. Sistem anti icing yang sudah ada membutuhkan energi listrik yang dapat menambah beban kerja engine, sedangkan ada energi berupa kalor yang selama ini hanya digunakan sebagai tenaga dorong. Berdasarkan hasil penelitian, pengaruh variasi vortex generator insert pada heater didapatkan pressure drop twisted 16,70 Pa dan wire coil 14,38 Pa, sehingga pressure drop twisted lebih baik dari pressure drop wire coil. Perpindahan kalor dari twisted 70,32 Watt dan wire coil 70,11 Watt, sehingga perpindahan kalor twisted lebih baik. Hal ini disebabkan perpindahan kalor twisted mempunyai nilai friction factor yang besar, sehingga mengasilkan bilangan Reynolds yang kecil. Bilangan Reynolds kecil menyebabkan kecepatan aliran udara kecil, sehingga aliran udara semakin lama bersentuhan dengan luas bidang pemanas, dengan demikian menghasilkan perpindahan panas yang baik
Composite Material Impact Test With Resin Matrix And Kenaf Fiber Reinforcement Using The Hand Lay Up Method Setiawan, Ferry; Anhar, Muh; Akmal, Akmal; Wicaksono, Dhimas
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.v3i1.400

Abstract

The purpose of this study was to obtain the results of impact testing on composite material with the arrangement of kenaf fibers in woven with volume variations of 0%, 10%, 20%, 30%, 40%, and 50%. The value obtained from impact testing with 0% fiber variation has an average energy absorption yield of 1.730623009 J and an average impact price of 0.01273547 J/mm², 10% fiber has an average absorption energy yield of 1.468150063 J and an average yield of 1.468150063 J The average impact price is 0.01080396 J/mm², 20% fiber has an average energy absorption yield of 1.730623009 J and an average impact price is 0.01273547 J/mm², 30% fiber has an average energy absorption yield of 1.214516698 J and the average yield is 1.214516698 J The average impact price is 0.008937499 J/mm², 40% fiber has an average energy absorption yield of 1.993095955 J and an average impact price is 0.01466698 J/mm², 50% fiber has an average energy absorption yield of 2.264328531 J and an average yield of 2.264328531 J Average Impact Price 0.016662952 J/mm². This composite material is made with epoxy resin as a binder and kenaf fiber as a reinforcing material. The method used is hand lay-up and specimen testing using charpy impact. After testing, a micro photo will be taken to see the best specimen fracture results.
Aplikasi Pembelajaran Rc (Remote Control) Aeromodelling Untuk Santri Putri Pesantren Islamic Leadership School (Ils) Taruna Panatagama Setiawan, Ferry; Ardianto, Haris; Marausna, Gaguk; Sehono, Sehono; Jayadi, Arid
Literasi Jurnal Pengabdian Masyarakat dan Inovasi Vol 2 No 1 (2022)
Publisher : Pengelola Jurnal Politeknik Negeri Ketapang Jl. Rangga Sentap, Dalong Sukaharja, Ketapang 78813. Telp. (0534) 3030686 Kalimantan Barat

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.58466/literasi.v2i1.1782

Abstract

ILS Panatagama Islamic Boarding School does not yet have sufficient supporting facilities to facilitate learning activities, especially learning in the field of science. Learning facilities are needed to provide insight and prepare students before entering a higher level of education and getting involved with life in the midst of society.The service activity aims to help the application of science learning, especially Physics lessons on RC (Remote Control) Aeromodelling Airplanes at the Taruna Panatagama Putri ILS Islamic Boarding School. The approach method offered to solve partner problems is through observation and discussion with school management, followed by lectures, training workshops and assistance in the use of RC Aeromodelling, especially drones. Through this activity, Santri gain insight and operational strengthening of the use of drones for various activities
MAINTENANCE ACTIVITY PLANNING FOR FUEL SYSTEM COMPONENTS ON KT-1B AIRCRAFT USING RELIABILITY METHODS Adiksa, Ekklesia Christian; Setiawan, Ferry; Wicaksono, Dhimas; Anhar, Muh
Injection: Indonesian Journal of Vocational Mechanical Engineering Vol 3 No 2 (2023)
Publisher : Pengelola Jurnal Politeknik Negeri Ketapang

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.58466/injection.v3i2.1776

Abstract

This research aims to prevent unscheduled maintenance by determining the optimal maintenance time to plan preventive maintenance on the fuel system of the KT-1B aircraft. Fuel System components include Engine Driven Pump, Fuel Control Unit. The methods used are Fault Tree Analysis (FTA), Failure Mode and Effect Analysis (FMEA), and Weibull Distribution. This method is to determine the factors causing failure, calculate the failure rate, and system reliability. Factors causing fuel system failure are influenced by age, damaged seals, vibration. The level of reliability of the Fuel System decreases with the length of use. Where the system will experience a critical period when it reaches operational time, namely engine driven pump = 1010 hours with a reliability value of 70%, fuel control unit = 1637 hours with a reliability value of 70.1%. After knowing the critical mass limit of the components, Preventive Maintenance planning will be carried out on the parts and components that cause failure, namely by cleaning the engine driven pump components and the fuel control unit by periodically checking the parts on the KT-1B aircraft.
ANALISIS EFISIENSI THERMAL TERHADAP ENGINE TURBOFAN PESAWAT BOEING 737-500 Sofyan, Edi; Alexandro Grandy, Yoseph; Setiawan, Ferry; Anhar, Muh
Injection: Indonesian Journal of Vocational Mechanical Engineering Vol 4 No 1 (2024)
Publisher : Pengelola Jurnal Politeknik Negeri Ketapang

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.58466/injection.v4i1.1777

Abstract

Thermal efficiency is a dimensionless measure that shows the incoming heat is the energy obtained from the energy source. The cooled output may be either heat or work, or it may be both. The CFM56-3 engine is a turbofan jet engine with large bypass capacity, dual rotor used with advanced axial flow technology designed for use on BOEING737 aircraft and all its variants. The purpose of this study is to determine the thermal efficiency of a turbofan engine, the causes of decreased performance of a turbofan engine and efforts to overcome it. This research is a qualitative and quantitative research using primary data and secondary data. Data collection techniques used are field studies, literature studies, as well as discussion and problem analysis. The field study in this research is to make direct observations of the processes that occur in the field. The results of this study can be concluded that the thermal efficiency of the Boeing 737-500 aircraft occurs the higher the difference between the incoming energy and outgoing energy through the compressor is 49.11% and the turbine is 64.01% the system produces the ideal thermal efficiency value of the Brayton cycle of 70 ,51% produced will be higher while the actual thermal efficiency of the Brayton cycle of 44.0% has decreased compared to the ideal thermal efficiency. The comparison of the ideal thermal efficiency of the Brayton cycle and the actual thermal efficiency of the Brayton cycle is 26.51%, meaning that efficiency can still be increased by as much as possible returning the component dimensions to their proper condition. The cause of the decreased performance of the turbofan engine is a change in dimensions due to frictional materials; wear and tear caused by continuous operation; as well as incorrect operating steps on the turbine engine and efforts to overcome them are periodic inspections of each turbofan engine components and using accurate measuring instruments
Pelatihan Rukti Jenazah sebagai Strategi untuk Meningkatkan Kepedulian Sosial di Lingkungan Perkotaan Puspitasari, Evi; Murtiningsih, Sri Rejeki; Zulfa, Auliya Failaih; Setiawan, Ferry
BERDAYA: Jurnal Pendidikan dan Pengabdian Kepada Masyarakat Vol 7 No 2 (2025)
Publisher : LPMP Imperium

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.36407/berdaya.v7i2.1628

Abstract

The social phenomenon of urban communities that are prone to individualism influences low social awareness. Rukti Jenazah as an activity that captures the manifestation of social and cultural values in society is starting to be rarely found in urban communities. Generally, they rely on third party services for corpse care rather than doing it collectively. This shows that community activities that require a sense of social awareness face real challenges in an era where human relationships are starting to grow distant. This certainly needs to be a concern for all parties. By involving 26 members of the organization as participants, the activity was carried out in three stages, namely input session, discussions, and direct practice with media that had been prepared by the community service team. The series of activities went smoothly and proved successful in increasing participants' understanding of the attitude of social awareness and how it is manifested through this activity. This was shown through the average post-test score (49.69) which was higher than the average pre-test score (44.31). The average understanding of participants increased by 5.38 points. This is the basis for Branch Manager of Muhammadiyah Notoyudan to develop and expand the Rukti Jenazah training program as a sustainable strategy in increasing social awareness and solidarity between residents, as well as a model that can be applied in other areas with similar problems.
Co-Authors Adiksa, Ekklesia Christian Aditya Mahendra, Dimas agung nusantoro Ahmad Saefulloh Akmal Akmal Aldo novando, Aldo novando Alexandro Grandy, Yoseph Alkhalif, Farhan Amelia, Sonia Amri, Chairul Angger Bagus Prasetiyo Ani Yuningsih Arfie Armelia Erissonia assidiq, maulana hasbi Atie Rachmiatie Atmoko, Dwi Ayu, Katriani Puspita Azies, Ibnu Abdul B, Berkat Benny Aprianto Saputra Bhayu Rama Bhayu Rhama Chalik, Faturrahman Christina, Meilianna Devita Cris Aditya Pratama Dian Yulie Reindrawati Dina Prasetia, Gilang Dotrimensi . Edi Sofyan Edi Sofyan, Edi Edy Sofyan, Edy Emi Triani Endy Aditya, Virgiawan Eva Forwanti Evi Puspitasari Fajar Pradana Febriyanto, Chandra Fikri, Moh Afif Fikri Haris Ardianto, Haris Hazhari, Fadhlah Hermawan, Aldi Henda Hillal, Raden Fatchul Hotma P. Sibuea Ilhami, Zaqi Arya Zullfawas Jayadi, Arid Jiwangga Hadi Nata Ka'Issa, Adestima Kandriana, Kandeg Kasanah, Mauridhatul Lili Mulyani M. Zainuddin L. F Mahendra, Dimas Aditya Malik, Kurnia Marausna, Gaguk MARIA BINTANG Marvy Ferdian Agusta Sahay Muh Anhar Muhammad Ditya Satrianto Muhammad Luqman Bukhori Nazarullah, Ibny Noerachman, Edy Nur Hamzah, Muhammad Nurdiana, Yuda Nurul Hikmah NURUL HIKMAH Octaline Putri Efma Putra, Aldi Maha Putra, I Wayan Sumardana Eka Putra, Ikbal Rizki Putra, Ikbal Rizky Qayyum, A Reny Puspita Sari Nasution Reny Puspita Syari Nasution Reo Yudhono Retno Widyaningrum, Retno Rilah Fitria Utami Riswanto, Cipto Rizki, Ikbal Romadhon, Doni Sakti , Faras Bimo Saphira, Bella Saputro, Bayu Sapto Satria Maulana, Dede Satrya Buana, Allan Sehono Selvia, Fitriana Sintha, Melia Sitio, Elisabeth Fransisca Saragi Sofiyan, Edy Sofyan, Rifal Ma'rifatulloh Sontoe Sri Rejeki Murtiningsih Suja’i, Imam Sukwatus Suroso, Indreswari Syahirul Alam, Mochamad Doddy Syahirul Alam Taaqbier, Mohammed Tri Afirianto, Tri Tulis, Riamona Sadelman Ulfah, Sri Utami Irwan, Andi Ilmi Wahyuni Christiany Martono Wicaksono, Dhimas Wichaksono, Dhimas Widagdo, Djoko Widodo S Pranowo Widyananto, Eksi Wira Samudra, Elang Wiratama, Arif Prasetya Yolan Daniel Beni Yongki Candra Yorgen Kaharap Zulfa, Auliya Failaih Zulfikar Ramdhan, Muhammad