Aircraft component with closed box structure
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United States of America Patent
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Nov 6, 2018
Grant Date -
Nov 17, 2016
app pub date -
May 12, 2016
filing date -
May 15, 2015
priority date (Note) -
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Abstract
A method of manufacturing an aircraft component, the component comprising a pair of covers joined by a pair of spars. The covers and spars form a closed box structure with four corners, each corner providing a transition between one of the covers and one of the spars. The method comprises: laying up a laminated sheet of fiber plies; and after the sheet has been laid up, folding the sheet to form the four corners and then joining the sheet to itself to provide the closed box structure.
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