A supplemental power generation arrangement for an aircraft includes a duct defined in the aircraft, a ram air turbine located in the duct and driven to rotate about a turbine axis by a ram airflow through the duct. One or more accessory components are operably connected to the ram air turbine. The ram air turbine is configured to provide rotational energy to power the one or more accessory components.
DUCTED SUPPLEMENTAL POWER UNIT OF AIRCRAFT
MIT KANÄLEN VERSEHENE ZUSÄTZLICHE ANTRIEBSEINHEIT FÜR EIN FLUGZEUG
UNITÉ D'ALIMENTATION SUPPLÉMENTAIRE À CONDUIT D'AÉRONEF
11.12.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |