An optimise drilling process for an aircraft composite structure using design of experiments

The present work is focusing on an optimisation of the drilling cutting process for the composite sandwich panel. The study provided machinist with a simple procedure in order to minimise the damage events occurring during drilling process for composite material. A statistical approach is used to an...

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Main Authors:	Mohd Ariffin, Mohd Khairol Anuar, Mohd Ali, M. I., Salit, Mohd Sapuan, Ismail, Napsiah
Format:	Article
Language:	English
Published:	Academic Journals 2009
Online Access:	http://psasir.upm.edu.my/id/eprint/13053/ http://psasir.upm.edu.my/id/eprint/13053/ http://psasir.upm.edu.my/id/eprint/13053/1/13053.pdf

id	upm-13053
recordtype	eprints
spelling	upm-130532016-01-26T01:53:12Z http://psasir.upm.edu.my/id/eprint/13053/ An optimise drilling process for an aircraft composite structure using design of experiments Mohd Ariffin, Mohd Khairol Anuar Mohd Ali, M. I. Salit, Mohd Sapuan Ismail, Napsiah The present work is focusing on an optimisation of the drilling cutting process for the composite sandwich panel. The study provided machinist with a simple procedure in order to minimise the damage events occurring during drilling process for composite material. A statistical approach is used to analyse the experiment data and it is called as design of experiment (DOE). The technique minimise the number of test required and maximizes the amount of reliable information. A glass fiber reinforced plastic (GFRP) sandwich part number of BMS 4 - 17 form boeing corporation is used for testing. There are 2 type of drill bit material were selected and 4 variable such as drill bit material, cutting velocity, feed rate and hole diameter. The results from this study shows that the minimum damage length is 0.05 mm and the maximum is 0.44 mm which are done at 3000 rpm, feed rate of 80.2 mm/rev for HSS and spindle speed at 500 rpm, feed rate of 246.8 mm/rev using carbide tool respectively. Academic Journals 2009-10 Article PeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/13053/1/13053.pdf Mohd Ariffin, Mohd Khairol Anuar and Mohd Ali, M. I. and Salit, Mohd Sapuan and Ismail, Napsiah (2009) An optimise drilling process for an aircraft composite structure using design of experiments. Scientific Research and Essays, 4 (10). pp. 1109-1116. ISSN 1992-2248 http://www.academicjournals.org/journal/SRE/article-abstract/E509DE018608
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Putra Malaysia
building	UPM Institutional Repository
collection	Online Access
language	English
description	The present work is focusing on an optimisation of the drilling cutting process for the composite sandwich panel. The study provided machinist with a simple procedure in order to minimise the damage events occurring during drilling process for composite material. A statistical approach is used to analyse the experiment data and it is called as design of experiment (DOE). The technique minimise the number of test required and maximizes the amount of reliable information. A glass fiber reinforced plastic (GFRP) sandwich part number of BMS 4 - 17 form boeing corporation is used for testing. There are 2 type of drill bit material were selected and 4 variable such as drill bit material, cutting velocity, feed rate and hole diameter. The results from this study shows that the minimum damage length is 0.05 mm and the maximum is 0.44 mm which are done at 3000 rpm, feed rate of 80.2 mm/rev for HSS and spindle speed at 500 rpm, feed rate of 246.8 mm/rev using carbide tool respectively.
format	Article
author	Mohd Ariffin, Mohd Khairol Anuar Mohd Ali, M. I. Salit, Mohd Sapuan Ismail, Napsiah
spellingShingle	Mohd Ariffin, Mohd Khairol Anuar Mohd Ali, M. I. Salit, Mohd Sapuan Ismail, Napsiah An optimise drilling process for an aircraft composite structure using design of experiments
author_facet	Mohd Ariffin, Mohd Khairol Anuar Mohd Ali, M. I. Salit, Mohd Sapuan Ismail, Napsiah
author_sort	Mohd Ariffin, Mohd Khairol Anuar
title	An optimise drilling process for an aircraft composite structure using design of experiments
title_short	An optimise drilling process for an aircraft composite structure using design of experiments
title_full	An optimise drilling process for an aircraft composite structure using design of experiments
title_fullStr	An optimise drilling process for an aircraft composite structure using design of experiments
title_full_unstemmed	An optimise drilling process for an aircraft composite structure using design of experiments
title_sort	optimise drilling process for an aircraft composite structure using design of experiments
publisher	Academic Journals
publishDate	2009
url	http://psasir.upm.edu.my/id/eprint/13053/ http://psasir.upm.edu.my/id/eprint/13053/ http://psasir.upm.edu.my/id/eprint/13053/1/13053.pdf
first_indexed	2018-09-07T13:19:46Z
last_indexed	2018-09-07T13:19:46Z
_version_	1610954977221541888

An optimise drilling process for an aircraft composite structure using design of experiments

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