Folding wing for aircraft
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United States of America Patent
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-
Nov 4, 2014
Issued Date -
N/A
app pub date -
May 2, 2012
filing date -
May 3, 2011
priority date (Note) -
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Abstract
A folding wing for an aircraft comprises first and second inboard wing sections, and first and second outboard wing sections. The first and second inboard wing sections rotate about a centerline hinge, and a centerline spring applies force to the first and second inboard wing sections to rotate the first and second inboard wing sections from a stowed position to a deployed position. At least one of the first and second inboard wing sections translates along the axis of rotation of the first and second inboard wing sections as they move from the stowed to the deployed positions. The first and second outboard wing sections rotate between the stowed and the deployed positions about first and second outboard hinges.
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