A turbofan engine includes a core engine section including a compressor section feeding air to a combustor to generate high speed exhaust gases that drive a turbine section all disposed about an engine axis, a geartrain driven by the core engine section, a fan section driven by the geartrain about a fan axis spaced apart from the engine axis, and an accessory gearbox driven by the geartrain and mounted apart from the core engine section and the fan section.
De-couple geared turbo-fan engine and aircraft
10.01.2017
Patent
Elektronische Ressource
Englisch
Geared diesel-engine performance
Engineering Index Backfile | 1933
GEARED TURBOFAN ENGINE WITH LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM FOR AIRCRAFT
Europäisches Patentamt | 2017
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