Analisis Geometris Sistem Kendali Elevator Pesawat Udara N219
<em>Flight control of elevator are used to control the attitude of the aircraft in pitching configuration. The system of this flight control are controlled by the force given by a pilot so that the aircraft will move to the desired pitch condition. In this research the force that should be inp...
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| Format: | Article |
| Language: | English |
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Department of Mechanical Engineering, Faculty of Engineering, Universitas Andalas
2021-10-01
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| Series: | Metal: Jurnal Sistem Mekanik dan Termal |
| Subjects: | |
| Online Access: | https://metal.ft.unand.ac.id/index.php/metal/article/view/136 |
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| _version_ | 1832574958888288256 |
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| author | Lenny Iryani Arie S Ramadhan |
| author_facet | Lenny Iryani Arie S Ramadhan |
| author_sort | Lenny Iryani |
| collection | DOAJ |
| description | <em>Flight control of elevator are used to control the attitude of the aircraft in pitching configuration. The system of this flight control are controlled by the force given by a pilot so that the aircraft will move to the desired pitch condition. In this research the force that should be inputted by a pilot easily and smooth are analyze. The study of this analysis was using N219 airplane designed by PT. Dirgantara Indonesia. The preliminary design of the force that should be inputted by a pilot are in 495 kN.mm. The result of the study are shown that the length of the arm in the elevator system give Margin of Safety in a range of 3 – 4.</em> |
| format | Article |
| id | doaj-art-6f0015a641be4633a641bb748816545f |
| institution | Kabale University |
| issn | 2598-1137 2597-4483 |
| language | English |
| publishDate | 2021-10-01 |
| publisher | Department of Mechanical Engineering, Faculty of Engineering, Universitas Andalas |
| record_format | Article |
| series | Metal: Jurnal Sistem Mekanik dan Termal |
| spelling | doaj-art-6f0015a641be4633a641bb748816545f2025-02-01T10:20:39ZengDepartment of Mechanical Engineering, Faculty of Engineering, Universitas AndalasMetal: Jurnal Sistem Mekanik dan Termal2598-11372597-44832021-10-0152939710.25077/metal.5.2.93-97.202198Analisis Geometris Sistem Kendali Elevator Pesawat Udara N219Lenny Iryani0Arie S Ramadhan1Politeknik Negeri BandungUniversitas Nurtanio<em>Flight control of elevator are used to control the attitude of the aircraft in pitching configuration. The system of this flight control are controlled by the force given by a pilot so that the aircraft will move to the desired pitch condition. In this research the force that should be inputted by a pilot easily and smooth are analyze. The study of this analysis was using N219 airplane designed by PT. Dirgantara Indonesia. The preliminary design of the force that should be inputted by a pilot are in 495 kN.mm. The result of the study are shown that the length of the arm in the elevator system give Margin of Safety in a range of 3 – 4.</em>https://metal.ft.unand.ac.id/index.php/metal/article/view/136flight controlelevatorgeometrismargin of safety |
| spellingShingle | Lenny Iryani Arie S Ramadhan Analisis Geometris Sistem Kendali Elevator Pesawat Udara N219 Metal: Jurnal Sistem Mekanik dan Termal flight control elevator geometris margin of safety |
| title | Analisis Geometris Sistem Kendali Elevator Pesawat Udara N219 |
| title_full | Analisis Geometris Sistem Kendali Elevator Pesawat Udara N219 |
| title_fullStr | Analisis Geometris Sistem Kendali Elevator Pesawat Udara N219 |
| title_full_unstemmed | Analisis Geometris Sistem Kendali Elevator Pesawat Udara N219 |
| title_short | Analisis Geometris Sistem Kendali Elevator Pesawat Udara N219 |
| title_sort | analisis geometris sistem kendali elevator pesawat udara n219 |
| topic | flight control elevator geometris margin of safety |
| url | https://metal.ft.unand.ac.id/index.php/metal/article/view/136 |
| work_keys_str_mv | AT lennyiryani analisisgeometrissistemkendalielevatorpesawatudaran219 AT ariesramadhan analisisgeometrissistemkendalielevatorpesawatudaran219 |