A nacelle for a gas turbine engine includes a upper and lower bifurcations, an inner diameter cowl and a first latch system. The inner diameter cowl extends between the upper and lower bifurcations and the first latch system is mounted on the inner diameter cowl. The first latch system is spaced along the inner diameter cowl between the upper and lower bifurcations.
NACELLE MOUNTED LATCHING SYSTEM
AN EINER GONDEL MONTIERTES VERRIEGELUNGSSYSTEM
SYSTÈME DE VERROUILLAGE MONTÉ SUR UNE NACELLE
01.05.2019
Patent
Elektronische Ressource
Englisch
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