L'invention concerne un ensemble propulsif (151) pour un aéronef qui comporte un châssis (180), un système de motorisation (150) comportant un noyau (152) enfermé dans un carter (154) et comportant une chambre de combustion (158) et une turbine (160), ...

A mounting assembly for attaching a ducted fan gas turbine engine to an aircraft is provided. The engine has an intake (111), a propulsive fan, a fan case (125) surrounding the fan, and a core engine (126). The air intake (111) is attached to the front of ...

The present invention relates to a system for taxiing an aircraft without starting one or more main aircraft propulsion engines. In one embodiment, a low pressure spool of a gas turbine engine is driven by a mechanical coupling with an auxiliary power unit...