Optimalisasi Proses Perakitan Pesawat Tanpa Awak dengan Metoda Critical Path Methods (CPM)

Adi Saputra M, Dendi and Satria, Eka and Arif Pandy, Gusman (2016) Optimalisasi Proses Perakitan Pesawat Tanpa Awak dengan Metoda Critical Path Methods (CPM). Jurnal Optimasi Sistem Industri, 15 (1). pp. 87-92. ISSN 2088-4842

PDF (Jurnal Nasional Tidak Terakreditasi (bisa ditelusuri online)) - Published Version Restricted to Repository staff only until 2 January 2017. Available under License Creative Commons Public Domain Dedication. Download (318Kb) | Request a copy

Abstract

The manufacturing of Unmanned Aerial Vehicles (UAV) requires a design process that involves the design of aircraft’s components such as fuselage, wing, horizontal stabilizer, vertical stabilizer, ailerons, elevators, tail, and wing. The process takes a long time. Therefore, the distribution of structural works based on their characteristics and classifications by considering their design attributes and manufacturing processes is required. This research aims to find the optimal time and critical path of the assembly process of an UAV based on product work breakdown structure (PWBS) and critical path method (CPM). The result reveals that the optimal assembly time is 139 minutes. Finally, the application of product-oriented structural work distribution and the optimization of the assembly activities involved in the critical path successfully minimize the duration of the assembly process.

Item Type:	Article
Subjects:	T Technology > TS Manufactures
Unit atau Lembaga:	Fakultas Teknik > Teknik Mesin
Depositing User:	Mrs. Dendi Adi Saputra
Date Deposited:	15 Oct 2016 01:19
Last Modified:	15 Oct 2016 01:19
URI:	http://repository.unand.ac.id/id/eprint/23827

Actions (login required)

View Item