CRACK AND DELAMINATION STOPPERS FOR AIRCRAFT PROPULSION SYSTEM COMPONENTS
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United States of America Patent
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Issued Date -
May 23, 2013
app pub date -
Dec 20, 2012
filing date -
May 20, 2011
priority date (Note) -
Abandoned
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Abstract
An inner fixed structure of a thrust reverser includes an inner skin, an outer skin, a cellular core disposed between the inner skin and the outer skin, and at least one crack and delamination stopper extending radially between the inner skin and the outer skin.
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