A spinner (80) for a gas turbine engine (20) comprises an outer shell (82) for defining an airflow path when mounted in a gas turbine engine (20). An inner surface (84) is provided with a plurality of webs (86). A gas turbine engine (20) and a fan section (22) for a gas turbine engine (20) are also disclosed.
GAS TURBINE ENGINE WITH REINFORCED SPINNER
Gasturbinenmotor mit verstärkter Nasenhaube
Moteur à turbine à gaz avec cône renforcé
2019-08-28
Patent
Elektronische Ressource
Englisch