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US Patent 10247108 Turbojet engine with offset fans with a differential system

Patent 10247108 was granted and assigned to Safran on April, 2019 by the United States Patent and Trademark Office.

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Patent abstract

A propulsion unit of an aircraft including a turbine (15), at least one fan (10) with an axis offset relative to the axis of the turbine and a power transmission mechanism between the turbine and the fan. The power transmission mechanism includes a speed reducing gear (20) with an input and a movement output, the input being in the extension of the axis (16) of the turbine and the output connected to the fan.

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