Gas turbine engine architecture

Power plants – Combustion products used as motive fluid – With lubricators

Reexamination Certificate

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Details

C060S802000, C184S006110

Reexamination Certificate

active

07055303

ABSTRACT:
A gas turbine engine having an oil cavity architecture and bearing placement which reduce heat rejection and oil system complexity by enclosing the reduction gearbox bearings and at least the shaft bearings supporting the high pressure shaft in the same oil cavity.

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