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.
RETRACTABLE LEADING EDGE WING SLATS HAVING AUTONOMOUSLY CURVABLE AIRFLOW SHIELD FOR NOISE-ABATEMENT
EINZIEHBARE VORFLÜGEL MIT EINEM AUTONOM KRÜMMBAREN LUFTSTROMSCHIRM ZUR LÄRMMINDERUNG
BECS DE BORD D'ATTAQUE RÉTRACTABLES AYANT UN DISPOSITIF D'ARRÊT DE L'ÉCOULEMENT D'AIR POUVANT ÊTRE INCURVÉ DE MANIÈRE AUTONOME POUR RÉDUIRE LE BRUIT
2023-01-11
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Retractable leading edge wing slats having autonomously curvable airflow shield for noise-abatement
European Patent Office | 2022
|RETRACTABLE LEADING EDGE WING SLATS HAVING AUTONOMOUSLY CURVABLE AIRFLOW SHIELD FOR NOISE-ABATEMENT
European Patent Office | 2019
|RETRACTABLE LEADING EDGE WING SLATS HAVING AUTONOMOUSLY CURVABLE AIRFLOW SHIELD FOR NOISE-ABATEMENT
European Patent Office | 2020
|NOISE ABATEMENT SYSTEMS FOR RETRACTABLE LEADING EDGE WING SLATS OF AN AIRCRAFT WING ASSEMBLY
European Patent Office | 2019
|NOISE ABATEMENT SYSTEMS FOR RETRACTABLE LEADING EDGE WING SLATS OF AN AIRCRAFT WING ASSEMBLY
European Patent Office | 2021
|