Methods and apparatus for assembling gas turbine engines

Power plants – Reaction motor – Method of operation

Reexamination Certificate

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Details

C060S226100, C060S226300, C060S791000

Reexamination Certificate

active

10845032

ABSTRACT:
A method facilitates assembling a gas turbine engine including a compressor and a rotor assembly coupled in axial flow communication downstream from the compressor. The method comprises coupling a bypass system in flow communication with the compressor to channel a portion of flow discharged from the compressor towards the rotor assembly is channeled through the bypass system, and coupling a downstream end of the bypass system within the gas turbine engine such that the flow entering the bypass system flows past the rotor assembly and is discharged downstream from the rotor assembly.

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