AIRCRAFT NOZZLE
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United States of America Patent
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Issued Date -
Jul 25, 2019
app pub date -
Jan 15, 2019
filing date -
Jan 15, 2019
priority date (Note) -
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Abstract
A flap for a variable area exhaust nozzle of a gas turbine engine. The flap includes a support structure and a gas shield retained thereto. The support structure and the gas shield include a pair of grooves extending in a longitudinal direction of the flap and a pair of corresponding tongues that engage the pair of grooves so as to retain the gas shield to the support structure and to allow movement of the gas shield by thermal expansion along the support structure in the longitudinal direction.
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