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ANALISA PREFERENSI KONSUMEN TERHADAP KERUPUK AMPLANG PRODUKSI TOKO OBIC DI KABUPATEN KETAPANG Anhar, Muh; Wardanu, Adha Panca
Jurnal Sistem Teknik Industri Vol. 18 No. 1 (2016): JSTI Volume 18 Number 1 January 2016
Publisher : TALENTA Publisher

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (53.988 KB) | DOI: 10.32734/jsti.v18i1.337

Abstract

Tujuan penelitian ini adalah Menganalisis karakteristik konsumen dan proses keputusan pembelianamplang merek OBIC, Menganalisis faktor-faktor yang mempengaruhi keputusan konsumen dalam pembelianamplang merek OBIC dan menganalisis sikap konsumen terhadap amplang merek OBIC. Jenis data yangdigunakan dalam penelitian ini adalah data primer dan data sekunder. Metode pengambilan sampel yangdigunakan adalah convenience sampling (pengambilan sampel secara kebetulan) yang termasuk ke dalam teknikpengambilan sampel non peluang. Karakteristik konsumen berdasarkan kelompok usia, jenis kelamin, jenispekerjaan, pengeluaran per bulan, ketertarikan konsumen mengkonsumsi Amplang, asal informasi mengenaiAmplang merek obic dan tempat konsumen biasa membeli Amplang merek obic dianalisis secara diskriptif.Penilaian sikap konsumen dianalisis dengan menggunakan Model Fishbein. Hasil Analisis diketahui bahwakarakteristik responden didominasi oleh perempuan. Usia terbanyak pada usia 21-30 tahun, tingkat pendidikandidomonasi oleh SLTA dan sebagian besar konsumen belum menikah. Pembelian Amplang OBIC olehresponden terjadi di tampat produksi. Setelah melakukan pembelian, konsumen mengevaluasi hasil pembeliandan hasilnya responden menyatakan puas terhadap Amplang OBIC. Reaksi konsumen apabila OBIC tidaktersedia di lokasi pembelian adalah membeli merek lain, dan apabila harga OBIC naik, maka konsumen akanmemilih merek lain. Atribut yang dinilai positif adalah atribut higienis, rasa, aroma, harga dan kemasan.Atribut yang dinilai netral adalah atribut volume, warna dan kemudahan dalam memperoleh produk. Atributproduk yang netral, agar dinilai positif maka perlu terus meningkatkan pelaksanaan atau kinerja dari atributtersebut. Secara keseluruhan atribut produk amplang OBIC dinilai positif oleh konsumen dengan nilai sikapsebesar 157,31. Hal ini menunjukkan bahwa atribut dari amplang OBIC diterima oleh konsumen.
PENERAPAN METODE SERVICE QUALITY & QUALITY FUNCTION DEPLOYMENT (QFD) DALAM UPAYA PENINGKATAN PELAYANAN KEPADA MAHASISWA POLITEKNIK KETAPANG Anhar, Muh; Kalsum, Syarifah Umi
Jurnal Sistem Teknik Industri Vol. 18 No. 2 (2016): JSTI Volume 18 Number 2 July 2016
Publisher : TALENTA Publisher

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (471.142 KB) | DOI: 10.32734/jsti.v18i2.352

Abstract

Penggunaan Servqual dan QFD untuk mengidentifikasi keinginan dan kebutuhan mahasiswa jurusan Perawatan Dan Perbaikan Mesin Politeknik Ketapang serta upaya peningkatan mutu layanan meliputi: penentuan atribut layanan, pembuatan kuesioner, pengumpulan dan pengolahan data, pembuatan HOQ, analisa dan Interprestasi dan identifikasi upaya perbaikan kualitas layanan. Dari hasil penelitian diperoleh servqual-gap secara berurutan adalah: Assurance (-1,491), Empathy (-1,462), Responsiveness (-1,459), Reliability (-1,457) dan Tangibles (-1,422). Hal ini berarti mahasiswa menaruh harapan sangat besar akan pelayanan yang baik dari lembaga. Namun demikian masih ada kesenjangan antara kualitas layanan yang diharapkan oleh mahasiswa dan tingkat kebaikan pelayanan yang diberikan sehingga belum sepenuhnya seperti yang diharapkan. Perbaikan dan peningkatan kualitas layanan sangat mungkin dilakukan mengingat improvement ratio nya sebesar 1,188 (Moderately Difficult Improvement) yang berarti sumber daya yang dimiliki oleh Jurusan perawatan dan perbaikan mesin Politeknik Ketapang mampu menunjangnya dengan baik.
PERENCANAAN PREVENTIVE MAINTENANCE MENGGUNAKAN METODE RELIABILITY PADA ELECTRICAL SISTEM AUXILIARY POWER UNIT BOEING 737-500 Taaqbier, Mohammed; Setiawan, Ferry; Anhar, Muh
Injection: Indonesian Journal of Vocational Mechanical Engineering Vol 2 No 1 (2022)
Publisher : Pengelola Jurnal Politeknik Negeri Ketapang

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.58466/injection.v2i1.1463

Abstract

The electrical system Auxiliary Power Unit on the Boeing 737-500 aircraft often experiences operational failure due to damage to the components in the system, this incident causes significant operational losses so that an appropriate maintenance method is needed to eliminate the factors that cause failure in the Electrical system Auxiliary Power Units. The purpose of this study is to plan preventive maintenance activities on the Electrical Auxiliary Power Unit system so that part damage that causes failure can be handled properly. The reliability method is calculated using the Weibull probability distribution so that the critical operating time limit is obtained on the Electrical Auxiliary Power Unit system. From the calculation results, the critical operational limit for the Electrical Auxiliary Power Unit system is 271 flight cycle with the main damage being the start relay component, with maintenance activities in the form of inspection, repair, testing and cleaning activities.
Low-Cost LoRaWAN Solution for Groundwater Monitoring in Peatlands Usman, Saifudin; Atimi, Rizqia Lestika; Anhar, Muh; Susanto, Anto
Journal of Information System and Informatics Vol 6 No 4 (2024): December
Publisher : Universitas Bina Darma

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.51519/journalisi.v6i4.923

Abstract

Some efforts made in restoring peatlands include moisture restoration, replanting, hydrological restoration, monitoring, and evaluation using technology to obtain periodic condition data. The implementation of the Water Level Logger (WLL) for monitoring groundwater levels in peatlands still faces issues because the sensor installation points are not served by cellular communication networks for data transmission. This research aims to implement a Low Power Wide Area Network (LPWAN) as a low-cost infrastructure used in applications for monitoring water levels in peatland. The method in this research is an approach to develop LoRaWAN gateway devices and servers using ChirpStack, equipped up to the application layer as supporting infrastructure for self-hosted groundwater level monitoring tools integrated with a time-series database and displaying measurement data on a dashboard periodically. Based on the tests, the average measurement of the Received Signal Strength Indicator (RSSI) obtained at the farthest distance of 3 km was -116 dBm, where the RSSI value also decreased with each additional distance, and the Line-of-Sight (LOS) condition significantly affected the RSSI value. This research shows that a real-time peat groundwater monitoring system has been successfully built at a low cost using self-hosted LoRaWAN gateways and servers, while maintaining reliability.
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
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.
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.
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
Effect Of Nano Reinforced Adhesive AL Powder And Cnt On Bending Strength Of Hybrid Laminate Structure AL - CFRP Anhar, Muh; Laksana, Lintang Bayu Adi; Wicaksono, Dhimas; Setiawan, Fery
Jurnal Riset Teknologi Pencegahan Pencemaran Industri Vol. 16 No. 1 (2025): May
Publisher : Balai Besar Standardisasi dan Pelayanan Jasa Pencegahan Pencemaran Industri

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.21771/jrtppi.2025.v16.no1.p51-60

Abstract

Amphibious aircraft are types of aircraft that can land on land and in water with floating components (floaters).  Amphibious aircraft are capable of landing both on land and water using float-equipped structures. In its operation, it is likely to have a bending force on the floater. When the floater is replaced with a hybrid composite, it is likely to have a light load and high beding value bending value. During operation, the floater is subjected to significant bending forces. Replacing the floater with a hybrid composite results in a lighter structure with improved bending strength. This study aims to analyze the bending test of hybrid composites reinforced with carbon fiber and aluminum faceplates. This study aims to evaluate the bending strength of hybrid composites reinforced with carbon fiber and aluminum faceplates. The method used in this study is vacuum bagging, where the sample is combined with epoxy resin and mixed with carbon nanotube (CNT) nanoparticles and aluminum powder (AL). The study was conducted with adhesive resin, surface treatment and the addition of nano particles to determine the effect of the bending strength of the composite. This study aims to analyze the effect of surface treatment and nanoparticle addition on the flexural strength of the hybrid composite.  The results showed that had a high bending value compared to the variation of specimens without surface treatment or nano particles. Specimens treated with surface modification and nanoparticles exhibited higher bending strength than those without either treatment. The highest bending stress value was obtained by the CNT variation of 133.89 MPa followed by the variation without nano particles of 98.59 MPa, then the variation without surface treatment of 91.76 MPa, and the one with the smallest value was the AL variation of 61.02 MPa. Macro photo analysis after bending test shows the presence of Mixed-mode defects in the specimen. This shows that specimens that have surface treatment and nano particles have better bonds and are able to fill the void in the empty area, so that the bending strength is good. This study provides an important contribution to understanding the variation of adhesives and nano particles on the bending strength of hybrid composites. This study offers preliminary insights into how variations in adhesives and nanoparticles influence the bending strength of a specific hybrid composite system.