The present disclosure relates generally to an aerodynamic track fairing assembly (200) used on an engine nacelle (66), the track fairing assembly (200) positionable on the aft section (67) of the engine nacelle, the aerodynamic track fairing assembly (200) including an upper section (202) extending toward an aft end (69) of the aft section (67) of the engine nacelle (66), a bottom section (206) extending toward the aft end (69) of the aft section (67) of the engine nacelle (66), the bottom section (206) affixed to the upper section (202) to form a track cavity (212) therebetween, and a fairing fitting (214) disposed within the track cavity (212) and affixed to the bottom section (206).
TRACK FAIRING ASSEMBLY FOR A TURBINE ENGINE NACELLE
GONDELVERKLEIDUNGSANORDNUNG FÜR EINE TURBINENMOTOR
ENSEMBLE DE CARÉNAGE POUR UNE NACELLE DE TURBORÉACTEUR
06.05.2020
Patent
Elektronische Ressource
Englisch
Aerodynamic track fairing for a gas turbine engine fan nacelle
Europäisches Patentamt | 2019
|AERODYNAMIC TRACK FAIRING FOR A GAS TURBINE ENGINE FAN NACELLE
Europäisches Patentamt | 2020
|