GAS TURBINE ENGINE WITH FRONT SUPPORT ARRANGEMENT
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United States of America
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Issued Date -
Feb 13, 2025
app pub date -
Oct 29, 2024
filing date -
Oct 29, 2024
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Abstract
A gas turbine engine includes a propulsor section including a propulsor having blades extending from a propulsor hub, and a propulsor shaft that drives the propulsor hub. A compressor section includes a first compressor having a rotatable compressor hub. A speed reduction device drives the compressor hub and the propulsor through a connection established axially forward of the epicyclic gear system relative to an engine longitudinal axis. The epicyclic gear system is straddled by forward and aft bearings that engage a carrier of the speed reduction device.
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