RELIABILITY ANALYSIS OF MAIN ROTOR EC 155B1 ON PIN BLADE AND ATTACH BEAMS COMPONENTS USING MARKOV ANALYSIS

IF 0.1 0 MUSIC
Irvan Aditiya, L. R. Pinandhita, Bangga Dirgantara Adiputra
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Abstract

Reliability is used to estimate the conditions of systems or components in the future based on previous conditions. The objects of this research are EC 155B1 aircrafts owned by Indonesia Air Transport & Infrastrucure (IAT), and the method used for analysis is markov analysis. Markov analysis is widely used as an analyzing technique the states of the system that has limited information (memoryless). From this research, ATA chapter 62 Main Rotor that meets the requirements of reliability analysis. The constituent components of main rotor states are Pin Blade, Lower Attach Beam, and Upper Attach Beam. The results of the markov analysis of main rotor system, the states that worked properly are state 1, state 3, and state 4. The probability of the state 1 showed that state has decreased from initial condition, while the state 3 and state 4 have increased from initial condition and subsequently have decreased. The reliability of main rotor system has decreased along with increasing of flight hours with the Mean Time To Failure (MTTF) is 2340.22 flight hours.
用马尔可夫分析方法对主转子ec155b1销叶和附梁构件进行可靠性分析
可靠性是指在现有条件的基础上对系统或部件的未来状态进行估计。本研究的对象是印度尼西亚航空运输和基础设施公司(IAT)拥有的EC 155B1飞机,使用马尔可夫分析方法进行分析。马尔可夫分析作为一种分析有限信息(无记忆)系统状态的技术被广泛应用。从本研究出发,对ATA第62章主转子进行了满足要求的可靠性分析。主转子状态的组成部分是销叶、下附梁和上附梁。主转子系统的马尔可夫分析结果表明,正常工作的状态为状态1、状态3和状态4。状态1的概率从初始条件开始减小,而状态3和状态4的概率从初始条件开始增大后减小。随着飞行时数的增加,主旋翼系统的可靠性逐渐降低,平均故障时间(MTTF)为2340.22飞行时数。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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