Modular gas turbine engine

Power plants – Reaction motor – Interrelated reaction motors

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Details

60 39161, 60 3931, 244 54, F02K 304

Patent

active

049341405

ABSTRACT:
A gas turbine fan engine with improved maintainability features is disclosed. Forward and rearward sections of the core of the engine are joined one to the other, and each are independently separable from the pylon on which the engine is mounted without the necessity of removing the other from the airplane.

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