A nacelle assembly includes a fixed inlet segment (56) and a translating inlet segment (58). The translating inlet segment (58) includes a slider beam (86) laterally between a pair of tracks (68;70) of the fixed inlet segment (56). The slider beam (86) is mated with and slidable longitudinally along the pair of tracks (68;70). The translating inlet segment (58) is configured to translate longitudinally between a retracted position and an extended position. An aft end (78) of the translating inlet segment (58) is abutted against a forward end (60) of the fixed inlet segment (56) when the translating inlet segment (58) is in the retracted position. An airflow inlet (46) into an inlet passage of the nacelle assembly is opened longitudinally between the aft end (78) and the forward end (60) when the translating inlet segment (58) is in the extended position.
NACELLE WITH A TRANSLATABLE INLET FOR AN AIRCRAFT PROPULSION SYSTEM
GONDEL MIT EINEM VERSCHIEBBAREN EINLASS FÜR EIN FLUGZEUGANTRIEBSSYSTEM
NACELLE AYANT UNE ENTRÉE DÉPLAÇABLE POUR SYSTÈME DE PROPULSION D'AÉRONEF
2022-10-26
Patent
Elektronische Ressource
Englisch
NACELLE WITH A TRANSLATABLE INLET FOR AN AIRCRAFT PROPULSION SYSTEM
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