RETRACTABLE LEADING EDGE WING SLATS HAVING AUTONOMOUSLY CURVABLE AIRFLOW SHIELD FOR NOISE-ABATEMENT

Noise-abatement for a leading edge wing slat is provided by a noise-abatement airflow shield integral with the lower trailing edge of the slat, wherein the shield is reciprocally autonomously curveable from a substantially planar configuration when the slat is in a retracted position thereof and int...

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Main Authors CAPUCHO COELHO, Eduardo Lobão, DE MOURA LIMA, Leandro Souza, HORI OCHI, Marcus Felipe, CRENITE SIMOES, Leandro Guilherme, MARTINI CATALANO, Fernando, WAGNER SKALESKI, Cecil, DOS REIS, Danillo Cafaldo, KELLER KLUG, Francisco, DA SILVA, Paulo Anchieta, DO CARMO, Micael Gianini Valle, DA SILVA, Fábio Santos
Format Patent
LanguageEnglish
French
German
Published 11.01.2023
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:Noise-abatement for a leading edge wing slat is provided by a noise-abatement airflow shield integral with the lower trailing edge of the slat, wherein the shield is reciprocally autonomously curveable from a substantially planar configuration when the slat is in a retracted position thereof and into a convexly curved configuration when the slat is in a deployed position thereof.
Bibliography:Application Number: EP20170779993