ANALISIS KEANDALAN DALAM PERANCANGAN TEKNIK, STUDI KASUS SISTEM KENDALI ELEVATOR PESAWAT CN235-220

Penulis

  • I Wayan Suweca
  • Rosyidin Sufyani

Abstrak

This paper presents a reliability analysis of elevator control system for CN235-220 aircraft. The analysis is carried out using Bayes theorem. Reliability analysis is performed for several system configurations, existing system and two modified systems. Reliability calculation shows that one of the modified systems has reliability relatively higher than the existing system. To insure all requirement needed, the other analysis i.e. strength, stability, etc. must be conducted for the modified system.

Referensi

Dhilon B.S, 1988, Mechanical Reliability, Theory, Model and Applications, American Institute of Aeronautics and Astronautics, Inc.370 L'Enfant Promanade, SW, Washington.

Dimitri,K, 1991, Reliability Hand Book, Vol II, Departemen Aero Space and Mechanical Engineering, University Arizona, Cliss, New Jersey.

Rao SS, 1992, Reliability Based Design, McGraw Hill, Inc, New York.

Benjamin S. Blanchard, Dinesh Verma, Elmer L. Peterson, 1995, Maintainability: A Key to Effective Serviceability and Maintenance Management, John Wiley & Sons.

Noneleectronic Parts Reliability Data, 1995, Reliability Analysis Center, Rome, NY.

Respati B, 1994, Flight Control System Description for CN235-220, IPTN, Bandung.

Diterbitkan

2017-05-15

Cara Mengutip

Suweca, I. W., & Sufyani, R. (2017). ANALISIS KEANDALAN DALAM PERANCANGAN TEKNIK, STUDI KASUS SISTEM KENDALI ELEVATOR PESAWAT CN235-220. Mesin, 17(3), 93-97. Diambil dari https://journals.itb.ac.id/index.php/jtms/article/view/4895

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