A nacelle (20) for a gas turbine engine (10) includes at least one hinge axis (30) extending along the nacelle (20). At least one cowl (28) is mounted to the nacelle (20), along the at least one hinge axis (30), by a plurality of hinges (34). The plurality of hinges (34) includes at least one latch (36). The at least one latch (36) includes a clevis (40) and a tang (38). The clevis (40) and the tang (38) of the at least one latch (36) are configured to receive a hinge pin (50), through a pin aperture (42), when the at least one cowl (28) is in a closed condition.
NACELLE COWL HINGE
GONDELVERKLEIDUNGSSCHARNIER
CHARNIÈRE DE CAPOT DE NACELLE
2020-05-06
Patent
Elektronische Ressource
Englisch