A nacelle for a gas turbine engine includes at least one hinge axis extending along the nacelle. At least one cowl is mounted to the nacelle, along the at least one hinge axis, by a plurality of hinges. The plurality of hinges includes at least one latch. The at least one latch includes a clevis and a tang. The clevis and the tang of the at least one latch are configured to receive a hinge pin, through a pin aperture, when the at least one cowl is in a closed condition.
Nacelle cowl hinge
2021-02-02
Patent
Electronic Resource
English