NASA-LLIS-1860

Lessons Learned - Inherent Difficulty in Manufacturing Small Fillet Welds in 6000 Series Aluminum

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:28:36Z
date available	2017-09-04T15:28:36Z
date copyright	06/25/2008
date issued	2008
identifier other	NUXCQCAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/29697
description abstract	Abstract: The lesson learned is that when producing small size fillet welds in 6000 series aluminum there is an inherent risk that the welded part can be produced in accordance with approved manufacturing standards and inspection techniques, and yet result in a weld that has subsurface cracks. These cracks can result in a part with less than the required design strength and fail under load. The recommendation is that designers should be trained to understand the risk inherent in designing load carrying parts that incorporate critical welds in 6000 series aluminum.
language	English
title	NASA-LLIS-1860	num
title	Lessons Learned - Inherent Difficulty in Manufacturing Small Fillet Welds in 6000 Series Aluminum	en
type	standard
page	3
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2008
contenttype	fulltext
subject keywords	Additional Categories.
subject keywords	Additional Categories.Ground Equipment
subject keywords	Manufacturing and Assembly
subject keywords	Mission Operations and Ground Support Systems.
subject keywords	Mission Operations and Ground Support Systems.Ground support systems