Pub Date : 2023-01-18DOI: 10.28989/vortex.v4i1.1532
Berni Anisafitri, F. Rahmawati, Sri Mulyani
Analysis with the Weibull distribution method shows that the right treatment recommendations for treating air cycle machine (ACM) in the form of category preventive maintenancetime directed (TD), due to category preventive maintenanceTime Directed (TD) is a category of preventive maintenance that can be carried out if the time variable of a component or system is known and directly aims to prevent damage.
{"title":"REKOMENDASI PERAWATAN KOMPONEN AIR CYCLE MACHINE (ACM) PADA PESAWAT B737-900ER","authors":"Berni Anisafitri, F. Rahmawati, Sri Mulyani","doi":"10.28989/vortex.v4i1.1532","DOIUrl":"https://doi.org/10.28989/vortex.v4i1.1532","url":null,"abstract":"Analysis with the Weibull distribution method shows that the right treatment recommendations for treating air cycle machine (ACM) in the form of category preventive maintenancetime directed (TD), due to category preventive maintenanceTime Directed (TD) is a category of preventive maintenance that can be carried out if the time variable of a component or system is known and directly aims to prevent damage.","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"176 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-01-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"79611567","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2023-01-18DOI: 10.28989/vortex.v4i1.1533
Cristhina Cristhina, S. Mulyani, Istyawan Priyahapsara
Based on Boeing 737-900ER unscheduled removal data of pitot probe 0851HT-1 January, 2020 to November, 2021 found 14 removal for pitot probe with one of the defect is “pitot light on”. This indicate that there is a problem with the component and can disrupt the pilot and delay the aircraft. Knowing the result of failure identification and the type of failure be the aim of this research. Analysis using Failure Mode and Effect Analysis used to identify failure modes, causes and effects of failure, severity, occurrence, and detection ranking so that the risk priority number obtained. Based on the FMEA Worksheet, there are 8 failure modes that occur on the pitot probe with the highest Risk Priority Number is 126 on mode “IAS AND ALT DISAGREE”.
{"title":"IDENTIFIKASI KEGAGALAN PADA KOMPONEN PITOT PROBE BOEING 737-900ER","authors":"Cristhina Cristhina, S. Mulyani, Istyawan Priyahapsara","doi":"10.28989/vortex.v4i1.1533","DOIUrl":"https://doi.org/10.28989/vortex.v4i1.1533","url":null,"abstract":"Based on Boeing 737-900ER unscheduled removal data of pitot probe 0851HT-1 January, 2020 to November, 2021 found 14 removal for pitot probe with one of the defect is “pitot light on”. This indicate that there is a problem with the component and can disrupt the pilot and delay the aircraft. Knowing the result of failure identification and the type of failure be the aim of this research. Analysis using Failure Mode and Effect Analysis used to identify failure modes, causes and effects of failure, severity, occurrence, and detection ranking so that the risk priority number obtained. Based on the FMEA Worksheet, there are 8 failure modes that occur on the pitot probe with the highest Risk Priority Number is 126 on mode “IAS AND ALT DISAGREE”.","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"60 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-01-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"86424660","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2023-01-18DOI: 10.28989/vortex.v4i1.1528
Sarah Safira K Himran, Sri Mulyani, Fajar Khanif R
Bandar Udara Tanjung Api Ampana merupakan bandara yang cukup tingkat pelayanan terhadap arus penumpang dan barang yang digunakan untuk penerbangan ke berbagai wilayah di kota Ampana – Palu – Makasar. Dengan kebutuhan operasional penerbangan yang padat, kemampuan kapasitas muat pesawat yang diijinkan dan kekuatan runway dalam menerima pembebanan pesawat pada saat takeoff maupun landing. Maka penelitian ini dititik beratkan pada analisa berat operasional pesawat terbang terhadap kemampuan kekuatan runway di Bandar Udara Tanjung Api Ampana dengan menggunakan perhitungan ACN – PCN. Metode yang digunakan adalah metode ACN-PCN serta metode ARFL. Hasil menunjukkan hubungan antara berat take-off pesawat, PCN, serta panjang landasan. Pada analisa maksimum berat operasional yang dibatasi PCN didapatkan nilai maksimum yang diijinkan di Bandara tersebut dengan batasan kekuatan runway sesuai dengan jenis dan tipe pesawatnya. Hasil analisa runway strength didapatkan pada semua jenis dan tipe pesawat sesuai dengan operasional penerbangan di Bandar Udara Tanjung Api Ampana dapat menggunakan nilai maximum takeoff mass yang telah ditetapkan pada Tabel ACN Jeppesen. Dan berdasarkan analisis, panjang runway untuk pesawat ATR 500, CESSNA 208, dan HERCULES C-130 dapat dilayani oleh Bandara Tanjung Api Ampana dengan panjang runway nya. Agar pesawat jenis tersebut dapat take-off dan landing dengan aman.
{"title":"ANALISIS PERFORMA RUNWAY PADA BANDAR UDARA TANJUNG API AMPANA DENGAN METODE ACN-PCN","authors":"Sarah Safira K Himran, Sri Mulyani, Fajar Khanif R","doi":"10.28989/vortex.v4i1.1528","DOIUrl":"https://doi.org/10.28989/vortex.v4i1.1528","url":null,"abstract":"Bandar Udara Tanjung Api Ampana merupakan bandara yang cukup tingkat pelayanan terhadap arus penumpang dan barang yang digunakan untuk penerbangan ke berbagai wilayah di kota Ampana – Palu – Makasar. Dengan kebutuhan operasional penerbangan yang padat, kemampuan kapasitas muat pesawat yang diijinkan dan kekuatan runway dalam menerima pembebanan pesawat pada saat takeoff maupun landing. Maka penelitian ini dititik beratkan pada analisa berat operasional pesawat terbang terhadap kemampuan kekuatan runway di Bandar Udara Tanjung Api Ampana dengan menggunakan perhitungan ACN – PCN. Metode yang digunakan adalah metode ACN-PCN serta metode ARFL. Hasil menunjukkan hubungan antara berat take-off pesawat, PCN, serta panjang landasan. Pada analisa maksimum berat operasional yang dibatasi PCN didapatkan nilai maksimum yang diijinkan di Bandara tersebut dengan batasan kekuatan runway sesuai dengan jenis dan tipe pesawatnya. Hasil analisa runway strength didapatkan pada semua jenis dan tipe pesawat sesuai dengan operasional penerbangan di Bandar Udara Tanjung Api Ampana dapat menggunakan nilai maximum takeoff mass yang telah ditetapkan pada Tabel ACN Jeppesen. Dan berdasarkan analisis, panjang runway untuk pesawat ATR 500, CESSNA 208, dan HERCULES C-130 dapat dilayani oleh Bandara Tanjung Api Ampana dengan panjang runway nya. Agar pesawat jenis tersebut dapat take-off dan landing dengan aman.","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"26 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-01-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"81759684","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2022-07-01DOI: 10.28989/vortex.v3i2.1223
N. Retnowati, B. Junaidin, Dasrial Dasrial
The technology that can be developed from Unmanned Aerial Vehicle (UAV) in agriculture is the Unmanned Aerial Vehicle Eagle-X. This technology can help farmers in carrying out their daily activities to repel bird pests on agricultural land. However, people have difficulty understanding how to use UAVs. So, with this simulation, it is hoped that it can help farmers and producers understand the workings of the eagle-x aircraft. The simulation is made using 3Ds Max software which functions to create all 3D objects and also uses Unity software to create animations and simulations. This simulation can run well on a PC or laptop that has a Windows 10 operating system with 64bit and a minimum of core i-3 specifications. Trials using simulations were carried out on 30 farmers and the results showed that 86.67% of farmers stated that this simulation was effective in providing an overview of how the Unmanned Aerial Vehicle Eagle-X works in repelling sparrow pests.
{"title":"THE SIMULATION OF UNMANNED AERIAL VEHICLE EAGLE-X AS SPARROWS PESTS REPELLENT","authors":"N. Retnowati, B. Junaidin, Dasrial Dasrial","doi":"10.28989/vortex.v3i2.1223","DOIUrl":"https://doi.org/10.28989/vortex.v3i2.1223","url":null,"abstract":"The technology that can be developed from Unmanned Aerial Vehicle (UAV) in agriculture is the Unmanned Aerial Vehicle Eagle-X. This technology can help farmers in carrying out their daily activities to repel bird pests on agricultural land. However, people have difficulty understanding how to use UAVs. So, with this simulation, it is hoped that it can help farmers and producers understand the workings of the eagle-x aircraft. The simulation is made using 3Ds Max software which functions to create all 3D objects and also uses Unity software to create animations and simulations. This simulation can run well on a PC or laptop that has a Windows 10 operating system with 64bit and a minimum of core i-3 specifications. Trials using simulations were carried out on 30 farmers and the results showed that 86.67% of farmers stated that this simulation was effective in providing an overview of how the Unmanned Aerial Vehicle Eagle-X works in repelling sparrow pests.","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"50 2 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2022-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"84150991","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2022-07-01DOI: 10.28989/vortex.v3i2.1260
Ahmad Fikri Ramadhan, Lathifa Putri Afisna, A. Maharani, N. Ramadhanty, Rabin Isak, W. Ningsih
Destilasi merupakan salah satu proses pengolahan air keruh menjadi air bersih. Pada prinsipnya penyulingan merupakan cara sederhana untuk mendapatkan air bersih melalui proses penyulingan air kotor. Dalam proses distilasi, terdapat proses perpindahan panas, penguapan, dan kondensasi. Pada percobaan ini akan membuat alat destilasi air sederhana dengan menggunakan alat dan bahan yang terbuat dari stainless steel, styrofoam 2, aluminium foil, lakban hitam, lakban bening, kaca 28x34 cm. (tebal 3 mm), tipe ganda, gunting, pemotong, penggaris, dan air keruh. Hasil pengujian diperoleh dengan cara mengumpulkan data dengan cara mengkompromikan alat destilasi yang sudah berisi baskom stainless steel berisi air keruh di Desa Way Huwi.Kemudian udara ditempatkan di bawah sinar matahari. Pengambilan data suhu dan volume dilakukan mulai pukul 08.00 s/d 17.00 WIB. Dari data percobaan dapat diketahui bahwa efisiensi alat pada volume 1000 ml adalah 13,2%, pada volume 500 ml memiliki efisiensi 10,8%, dan pada volume 300 ml memiliki efisiensi. sebesar 10,3%. Kemudian ketebalan kaca yang digunakan sebagai penutup juga mempengaruhi efisiensi alat distilasi udara, dan ketebalan kaca yang efisien adalah 3 mm. Untuk mendapatkan data yang baik yang diperlukan sinar matahari yang terik. Semakin panas sinar matahari yang mengenai alat destilasi udara maka semakin cepat proses penguapan dan semakin banyak volume udara suling.Kemudian ketebalan kaca yang digunakan sebagai penutup juga mempengaruhi efisiensi alat distilasi udara, dan ketebalan kaca yang efisien adalah 3 mm. Untuk mendapatkan data yang baik yang diperlukan sinar matahari yang terik. Semakin panas sinar matahari yang mengenai alat destilasi udara maka semakin cepat proses penguapan dan semakin banyak volume udara suling. Kemudian ketebalan kaca yang digunakan sebagai penutup juga mempengaruhi efisiensi alat distilasi udara, dan ketebalan kaca yang efisien adalah 3 mm. Untuk mendapatkan data yang baik yang diperlukan sinar matahari yang terik. Semakin panas sinar matahari yang mengenai alat destilasi udara maka semakin cepat proses penguapan dan semakin banyak volume udara suling.
{"title":"STUDI EKSPERIMEN ALAT DESTILASI TENAGA SURYA DI KELURAHAN WAY HUWI","authors":"Ahmad Fikri Ramadhan, Lathifa Putri Afisna, A. Maharani, N. Ramadhanty, Rabin Isak, W. Ningsih","doi":"10.28989/vortex.v3i2.1260","DOIUrl":"https://doi.org/10.28989/vortex.v3i2.1260","url":null,"abstract":"Destilasi merupakan salah satu proses pengolahan air keruh menjadi air bersih. Pada prinsipnya penyulingan merupakan cara sederhana untuk mendapatkan air bersih melalui proses penyulingan air kotor. Dalam proses distilasi, terdapat proses perpindahan panas, penguapan, dan kondensasi. Pada percobaan ini akan membuat alat destilasi air sederhana dengan menggunakan alat dan bahan yang terbuat dari stainless steel, styrofoam 2, aluminium foil, lakban hitam, lakban bening, kaca 28x34 cm. (tebal 3 mm), tipe ganda, gunting, pemotong, penggaris, dan air keruh. Hasil pengujian diperoleh dengan cara mengumpulkan data dengan cara mengkompromikan alat destilasi yang sudah berisi baskom stainless steel berisi air keruh di Desa Way Huwi.Kemudian udara ditempatkan di bawah sinar matahari. Pengambilan data suhu dan volume dilakukan mulai pukul 08.00 s/d 17.00 WIB. Dari data percobaan dapat diketahui bahwa efisiensi alat pada volume 1000 ml adalah 13,2%, pada volume 500 ml memiliki efisiensi 10,8%, dan pada volume 300 ml memiliki efisiensi. sebesar 10,3%. Kemudian ketebalan kaca yang digunakan sebagai penutup juga mempengaruhi efisiensi alat distilasi udara, dan ketebalan kaca yang efisien adalah 3 mm. Untuk mendapatkan data yang baik yang diperlukan sinar matahari yang terik. Semakin panas sinar matahari yang mengenai alat destilasi udara maka semakin cepat proses penguapan dan semakin banyak volume udara suling.Kemudian ketebalan kaca yang digunakan sebagai penutup juga mempengaruhi efisiensi alat distilasi udara, dan ketebalan kaca yang efisien adalah 3 mm. Untuk mendapatkan data yang baik yang diperlukan sinar matahari yang terik. Semakin panas sinar matahari yang mengenai alat destilasi udara maka semakin cepat proses penguapan dan semakin banyak volume udara suling. Kemudian ketebalan kaca yang digunakan sebagai penutup juga mempengaruhi efisiensi alat distilasi udara, dan ketebalan kaca yang efisien adalah 3 mm. Untuk mendapatkan data yang baik yang diperlukan sinar matahari yang terik. Semakin panas sinar matahari yang mengenai alat destilasi udara maka semakin cepat proses penguapan dan semakin banyak volume udara suling. ","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"24 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2022-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"90692331","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2022-07-01DOI: 10.28989/vortex.v3i2.1237
Istyawan Priyahapsara
Delaminasi adalah sebuah ukuran dari area rusak sekitar lubang (Abdullah, 2019). Delaminasi tinggi bisa mengakibatkan kekuatan struktur yang berkurang. Dalam penelitian ini, akan dilakukan drilling dengan parameter permesinan yang sesuai dalam kaedah permesinan, selanjutnya dilakukan observasi citra makro terhadap lubang yang dihasilkan. Pengujian dilakukan pada material serat gelas 5 layer, dengan pahat drilling diameter 6.3 mm. Parameter drilling menggunakan variasi putaran mesin 1860 rpm, 2920 rpm, 4540 rpm, dan kecepatan pemakanan vertikal (plunging) 0.038 m/menit, 0.067m/menit. Didapatkan hasil nilai terendah delaminasi didapat pada spindle speed 1860 RPM dan plunging rate 0.038 rev/min sebesar 1.24. Nilai tertinggi delaminasi didapat pada spindle speed 4540 RPM dan plunging speed 0.076 rev/min
{"title":"ANALISIS FAKTOR DELAMINASI PADA MATERIAL SERAT GELAS TERHADAP PARAMETER DRILLING","authors":"Istyawan Priyahapsara","doi":"10.28989/vortex.v3i2.1237","DOIUrl":"https://doi.org/10.28989/vortex.v3i2.1237","url":null,"abstract":"Delaminasi adalah sebuah ukuran dari area rusak sekitar lubang (Abdullah, 2019). Delaminasi tinggi bisa mengakibatkan kekuatan struktur yang berkurang. Dalam penelitian ini, akan dilakukan drilling dengan parameter permesinan yang sesuai dalam kaedah permesinan, selanjutnya dilakukan observasi citra makro terhadap lubang yang dihasilkan. Pengujian dilakukan pada material serat gelas 5 layer, dengan pahat drilling diameter 6.3 mm. Parameter drilling menggunakan variasi putaran mesin 1860 rpm, 2920 rpm, 4540 rpm, dan kecepatan pemakanan vertikal (plunging) 0.038 m/menit, 0.067m/menit. Didapatkan hasil nilai terendah delaminasi didapat pada spindle speed 1860 RPM dan plunging rate 0.038 rev/min sebesar 1.24. Nilai tertinggi delaminasi didapat pada spindle speed 4540 RPM dan plunging speed 0.076 rev/min","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"158 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2022-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"74181948","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2022-07-01DOI: 10.28989/vortex.v3i2.1242
D. Hartini, Lazuardy Rahendra Pinandita, Pramuda Naufal Mubarak
The use of sea pandan leaves (pandanus tectorius) as a composite material is intended to reduce the use of synthetic fibers and increase the use of sea pandan leaves which are still wasted. This study aims to determine the tensile strength of the fiber composite of sea pandan leaves based on the manufacturing method and the direction of the fiber used. Composite manufacture using Hand Lay Up and Vacuum Bag methods. The direction of the fiber used is 00 and 900. Tensile test is based on ASTM D3039. The results showed that the composites made using the Vacuum Bag method had a higher tensile strength than the composites made using the Hand Lay Up method, which was 16.54 MPa for the 00 fiber direction and 13.60 MPa for the 900 fiber direction. The tensile strength of the composite using the 00 fiber direction is higher than the composite using the 900 fiber direction, which is 6.48 MPa for the Hand Lay Up method and 16.54 MPa for the Vacuum Bag method.
{"title":"TENSILE STRENGTH ANALYSIS OF SEA PANDAN LEAVES (PANDANUS TECTORIUS) FIBER REINFORCED EPOXY COMPOSITE","authors":"D. Hartini, Lazuardy Rahendra Pinandita, Pramuda Naufal Mubarak","doi":"10.28989/vortex.v3i2.1242","DOIUrl":"https://doi.org/10.28989/vortex.v3i2.1242","url":null,"abstract":"The use of sea pandan leaves (pandanus tectorius) as a composite material is intended to reduce the use of synthetic fibers and increase the use of sea pandan leaves which are still wasted. This study aims to determine the tensile strength of the fiber composite of sea pandan leaves based on the manufacturing method and the direction of the fiber used. Composite manufacture using Hand Lay Up and Vacuum Bag methods. The direction of the fiber used is 00 and 900. Tensile test is based on ASTM D3039. The results showed that the composites made using the Vacuum Bag method had a higher tensile strength than the composites made using the Hand Lay Up method, which was 16.54 MPa for the 00 fiber direction and 13.60 MPa for the 900 fiber direction. The tensile strength of the composite using the 00 fiber direction is higher than the composite using the 900 fiber direction, which is 6.48 MPa for the Hand Lay Up method and 16.54 MPa for the Vacuum Bag method.","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"28 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2022-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"77302969","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2022-07-01DOI: 10.28989/vortex.v3i2.1236
D. Santoso, K. Hariyanto
UAV aircraft with a fixed wing configuration with multi-rotor are aircraft capable of vertical take-off and landing (VTOL). In designing the wing structure of aircraft, the weight factor and the strength of the wing structure are factors that need to be considered. The use of sandwich composite materials on UAV wings is expected to be able to meet the requirements of UAV aircraft, namely having a light weight, having high rigidity and strength. In this study, a comparative analysis the strength of the sandwich composite wing structure with the balsa wood wing of the UAV VTOL VX-2 aircraft was carried out. The steps taken are to model the composite wing structure of sandwiches and balsa wood using CATIA. Performing the process of structural analysis using ANSYS software. Both half-span models are subjected to lift and vertical take-off loads. From the analysis results, the sandwich composite wing (glass fiber skin with styrofoam core) is stronger than the balsa wood wing structure under vertical take off loads. While the VTOL rods, upper and lower spars of the balsa wood wing model are stronger than the sandwich structure under lift loads, but overall the sandwich wing structure is stronger than the balsa wood wing
{"title":"COMPARISON OF SANDWICH COMPOSITE WING STRUCTURE WITH BALSA WOOD (CASE STUDY OF UAV AIRCRAFT FIXED WING VTOL VX-2)","authors":"D. Santoso, K. Hariyanto","doi":"10.28989/vortex.v3i2.1236","DOIUrl":"https://doi.org/10.28989/vortex.v3i2.1236","url":null,"abstract":"UAV aircraft with a fixed wing configuration with multi-rotor are aircraft capable of vertical take-off and landing (VTOL). In designing the wing structure of aircraft, the weight factor and the strength of the wing structure are factors that need to be considered. The use of sandwich composite materials on UAV wings is expected to be able to meet the requirements of UAV aircraft, namely having a light weight, having high rigidity and strength. In this study, a comparative analysis the strength of the sandwich composite wing structure with the balsa wood wing of the UAV VTOL VX-2 aircraft was carried out. The steps taken are to model the composite wing structure of sandwiches and balsa wood using CATIA. Performing the process of structural analysis using ANSYS software. Both half-span models are subjected to lift and vertical take-off loads. From the analysis results, the sandwich composite wing (glass fiber skin with styrofoam core) is stronger than the balsa wood wing structure under vertical take off loads. While the VTOL rods, upper and lower spars of the balsa wood wing model are stronger than the sandwich structure under lift loads, but overall the sandwich wing structure is stronger than the balsa wood wing","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"1 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2022-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"79973525","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2022-07-01DOI: 10.28989/vortex.v3i2.1265
Fajar Nugroho, Nurfi Ahmadi, Sarif Hidayat
Friction stir welding (FSW) adalah suatu teknologi pengelasan yang merupakan proses solid-state joining yang bisa digunakan untuk menyambungkan material aluminium dengan mampu las yang rendah. Proses FSW memanfaatkan putaran dari tool yang menggesek dua buah lempengan logam yang akan disambung. Aluminium 2024 T3 dengan ketebalan 4 mm disambung menggunakan proses FSW dengan variasi feedrate yang digunakan 13 mm/menit, 15 mm/menit, dan 25 mm/menit, kecepatan putaran spindle 910 rpm dan kedalaman pin 3 mm. Pengujian yang dilakukan adalah pengujian tarik, kekerasan dan uji struktur mikro pada masing-masing variasi pengelasan.Hasil penelitian menunjukkan bahwa kekuatan tarik dan regangan tarik tertinggi terjadi pada pengelasan dengan feedrate 25 mm/menit sebesar 221,51 MPa dan 3,60. Kemudian kekuatan tarik dan regangan tarik terendah terjadi pada pengelasan dengan feedrate 13 mm/menit sebesar 198,63 MPa dan 2,26. Nilai kekerasan tertinggi di area nugget zone dihasilkan pada pengelasan dengan feedrate 25 mm/menit yaitu sebesar 137 VHN dan nilai kekerasan terendah dihasilkan pada pengelasan dengan feedrate 13 mm/menit yaitu sebesar 105 VHN. Hasil foto struktur mikro pada area nugget zone dan TMAZ (Thermomecanically Affected Zone) mengalami perubahan seiring dengan berubahnya feedrate.
{"title":"PENGARUH KECEPATAN FEEDRATE FRICTION STIR WELDING (FSW) TERHADAP SIFAT MEKANIK DAN STRUKTUR MIKRO PADA ALUMINIUM PADUAN AA 2024-T3","authors":"Fajar Nugroho, Nurfi Ahmadi, Sarif Hidayat","doi":"10.28989/vortex.v3i2.1265","DOIUrl":"https://doi.org/10.28989/vortex.v3i2.1265","url":null,"abstract":"Friction stir welding (FSW) adalah suatu teknologi pengelasan yang merupakan proses solid-state joining yang bisa digunakan untuk menyambungkan material aluminium dengan mampu las yang rendah. Proses FSW memanfaatkan putaran dari tool yang menggesek dua buah lempengan logam yang akan disambung. Aluminium 2024 T3 dengan ketebalan 4 mm disambung menggunakan proses FSW dengan variasi feedrate yang digunakan 13 mm/menit, 15 mm/menit, dan 25 mm/menit, kecepatan putaran spindle 910 rpm dan kedalaman pin 3 mm. Pengujian yang dilakukan adalah pengujian tarik, kekerasan dan uji struktur mikro pada masing-masing variasi pengelasan.Hasil penelitian menunjukkan bahwa kekuatan tarik dan regangan tarik tertinggi terjadi pada pengelasan dengan feedrate 25 mm/menit sebesar 221,51 MPa dan 3,60. Kemudian kekuatan tarik dan regangan tarik terendah terjadi pada pengelasan dengan feedrate 13 mm/menit sebesar 198,63 MPa dan 2,26. Nilai kekerasan tertinggi di area nugget zone dihasilkan pada pengelasan dengan feedrate 25 mm/menit yaitu sebesar 137 VHN dan nilai kekerasan terendah dihasilkan pada pengelasan dengan feedrate 13 mm/menit yaitu sebesar 105 VHN. Hasil foto struktur mikro pada area nugget zone dan TMAZ (Thermomecanically Affected Zone) mengalami perubahan seiring dengan berubahnya feedrate.","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"22 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2022-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"81741233","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2022-07-01DOI: 10.28989/vortex.v3i2.1241
Gladis Tiara Andan Dewi, Muhammad Ridlo Erdata Nasution, Gunawan Gunawan
Pengembangan algoritma suatu program analisis performa landasan pacu terhadap berat take-off pesawat dilakukan untuk memfasilitasi analisis pada bandar udara secara umum. Dalam hal ini, metode ACN-PCN dan ARFL digunakan pada algoritma yang dibuat. Algoritma kemudian diimplementasikan pada kode program yang ditulis dengan GNU Octave dan dicoba untuk dijalankan dengan menggunakan data bandar udara Depati Amir serta tiga jenis pesawat berbeda, yaitu ATR 72, Boeing 737-800, dan Boeing 777-300ER. Berdasarkan hasil yang diperoleh, program berhasil melakukan analisis kemampuan pengoperasian take-off pesawat termasuk mengindikasikan ada tidaknya batasan operasional ketiga jenis pesawat terhadap kondisi landasan pada bandar udara acuan.
{"title":"PENGEMBANGAN AWAL ALGORITMA PROGRAM ANALISIS PERFORMA LANDASAN PACU TERHADAP BERAT TAKE-OFF PESAWAT","authors":"Gladis Tiara Andan Dewi, Muhammad Ridlo Erdata Nasution, Gunawan Gunawan","doi":"10.28989/vortex.v3i2.1241","DOIUrl":"https://doi.org/10.28989/vortex.v3i2.1241","url":null,"abstract":"Pengembangan algoritma suatu program analisis performa landasan pacu terhadap berat take-off pesawat dilakukan untuk memfasilitasi analisis pada bandar udara secara umum. Dalam hal ini, metode ACN-PCN dan ARFL digunakan pada algoritma yang dibuat. Algoritma kemudian diimplementasikan pada kode program yang ditulis dengan GNU Octave dan dicoba untuk dijalankan dengan menggunakan data bandar udara Depati Amir serta tiga jenis pesawat berbeda, yaitu ATR 72, Boeing 737-800, dan Boeing 777-300ER. Berdasarkan hasil yang diperoleh, program berhasil melakukan analisis kemampuan pengoperasian take-off pesawat termasuk mengindikasikan ada tidaknya batasan operasional ketiga jenis pesawat terhadap kondisi landasan pada bandar udara acuan.","PeriodicalId":40576,"journal":{"name":"Revista Vortex-Vortex Music Journal","volume":"10 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2022-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"86001275","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
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