PROPULSION SYSTEM FOR AN AIRCRAFT

A propulsion system 50 for an aircraft 10 includes a turbomachine 102 having a first turbine, a primary fan 104 mechanically driven by the first turbine of the turbomachine 102, and an electric generator 56 mechanically driven by the first turbine of the turbomachine 102. The propulsion system 50 al...

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Bibliographische Detailangaben
Hauptverfasser:	VONDRELL, Randy M, CRABTREE, Glenn David
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A propulsion system 50 for an aircraft 10 includes a turbomachine 102 having a first turbine, a primary fan 104 mechanically driven by the first turbine of the turbomachine 102, and an electric generator 56 mechanically driven by the first turbine of the turbomachine 102. The propulsion system 50 also includes an electric fan assembly, the electric generator 56 electrically connected to the electric fan assembly for powering the electric fan assembly.