Stiffening Element, Method For Coupling The Same, And Shell Component For An Aircraft Or Spacecraft
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United States of America Patent
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Aug 13, 2015
app pub date -
Feb 10, 2015
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Feb 13, 2014
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Abstract
A method for coupling a first and a second stiffening element for a skin of an aircraft or spacecraft, wherein the first stiffening element has a cross-sectional profile with first and second web portions extending from a flange portion of a predefined width toward the skin includes forming a coupling zone of the first stiffening element wherein the second web portion is at least partially removed to expose an inner surface of the first web portion, and a step of fastening a coupling element, for coupling the stiffening elements, to the coupling zone of the first stiffening element.
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