Method of fabricating a bonded cascade assembly for an aircraft thrust reverser
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United States of America Patent
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Oct 31, 2017
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N/A
app pub date -
Nov 2, 2016
filing date -
Jun 19, 2013
priority date (Note) -
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Abstract
A method of fabricating a bonded cascade assembly of a thrust reverser for an aircraft nacelle. The method may include inserting individual turning vanes between spaced apart elongated stiffeners at an aft end thereof and sliding the turning vanes toward a front frame piece attached to or integrally formed with forward ends of the elongated stiffeners. The elongated stiffeners may have inner and outer flanges for trapping and limiting radial movement of the turning vanes. The method may further include bonding the turning vanes to the structural frame with a structural adhesive and attaching a closeout cap to the aft ends of each of the elongated stiffeners.
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