Propulsion system for an aircraft

CN122166314APending Publication Date: 2026-06-09GENERAL ELECTRIC CO
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
GENERAL ELECTRIC CO
Filing Date
2018-02-09
Publication Date
2026-06-09

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Abstract

A propulsion system for an aircraft includes a turbomachine having a first turbine, a main fan mechanically driven by the first turbine of the turbomachine, and an electric generator mechanically driven by the first turbine of the turbomachine. The propulsion system further includes an electric fan assembly, the electric generator being electrically connected to the electric fan assembly to provide power thereto.
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