GEARED TURBOFAN ENGINE GEARBOX ARRANGEMENT
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United States of America Patent
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Issued Date -
Dec 24, 2020
app pub date -
Aug 31, 2020
filing date -
Nov 22, 2013
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Abstract
A gas turbine engine according to the present disclosure includes, among other things, a fan section having a plurality of fan blades, the plurality of fan blades having a peak tip radius Rt and an inboard leading edge radius Rh at a first inboard boundary of a first flowpath, and a core engine including a first turbine configured to drive a first compressor, and a fan drive turbine configured to drive the fan section.
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