Analisis Geometris Sistem Kendali Elevator Pesawat Udara N219



DOI: https://doi.org/10.25077/metal.5.2.93-97.2021

Author(s)

Lenny Iryani (Politeknik Negeri Bandung)
Arie S Ramadhan (Universitas Nurtanio)

Abstract


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.

Keywords


flight control; elevator; geometris; margin of safety

Full Text:

PDF

References


Federal Aviation Administration, “Flight Control”, FAA Publisher, 2018, Chapter 6.

Federal Aviation Regulation, “Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes”, PART 23, FAA Publisher, 2017.

R.C. Hibbeler, “Mechanics of Materials”, Eight Edition. New York: Pearson Prentice Hall, 2011.

D.L. Logan, “A First Course in The Finite Element Method”. United States: Cengage Learning, 2012.

J.L. Meriam and L.G. Kraige, “Engineering Mechanics Statics” (sixth edition). New York: John Wiley & Sons Inc, 2008.

I. Moir and A. Seabridge, “Aircraft Systems: Mechanical, Electrical, and Avionics Subsystems Integration” (third edition). England, John Wiley & Sons Ltd, 2008.

M.C. Niu, “Airframe Stress Analysis and Sizing (second edition)”. Hongkong Conmilit Press Ltd., 1999.

M.D. Pinem, “Analisis Struktur Dengan Metode Elemen Hingga”. Bandung: Rekayasa Sains, 2010.

R.C. Rice et al., “Metallic Materials Properties Development and Standarization (MMPDS)”. Washington: Federal Aviation Administration, 2003.

D.I. Sadeli, “Analisis Kekuatan Struktur Sayap Pesawat Tanpa Awak AI-X1 Menggunakan Software PATRAN/NASTRAN”. Tugas Sarjana, 2017

M.H. Sadraey, “Aircraft Design a Systems Engineering Approach (first edition)”. United States: John Wiley & Sons, 2017.

H.B.H. Siahaan, “Analisis Buckling Struktur Grid Pada Skin Panel Sayap Pesawat Terbang Menggunakan Software MSC PATRAN/NASTRAN”, 2017, Tugas Sarjana.

https://www.indonesian-aerospace.com/aircraft/detail/11_n219+nurtanio (diakses pada tanggal 30 Januari 2019)

https://id.wikipedia.org/wiki/N-219 (diakses pada tanggal 10 Oktober 2019)


StatisticsArticle Metrics

This article has been read : 406 times
PDF file viewed/downloaded : 122 times

Copyright (c) 2021 Lenny Iryani

 


View METAL's Stats

 

Creative Commons License

This work is licensed under a Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International License.