A fan nacelle includes a metallic fan containment case. A nacelle inlet is secured to the metallic fan containment case by permanent fastening elements. A gas turbine engine includes a metallic fan containment case. A core engine has a static engine structure housing a compressor section, a combustor section and a turbine section. The core engine is configured to receive core airflow. A fan is arranged within the metallic fan containment case. The fan is coupled to the core engine and is arranged in a bypass flowpath provided between the core engine and the metallic fan containment case. A nacelle inlet is secured to the metallic fan containment case by permanent fastening elements.
INTEGRATED NACELLE INLET AND METALLIC FAN CONTAINMENT CASE
INTEGRIERTE GONDELEINLASSÖFFNUNG UND METALLISCHES LÜFTERGEHÄUSE
ADMISSION DE NACELLE ET CARTER MÉTALLIQUE DE SOUFFLANTE INTÉGRÉS
2020-02-12
Patent
Electronic Resource
English
Integrated nacelle inlet and metallic fan containment case
European Patent Office | 2017
|