Vortex reducer in the high-pressure compressor of a gas turbine

Power plants – Combustion products used as motive fluid – For nominal other than power plant output feature

Reexamination Certificate

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Details

C415S115000, C415S116000

Reexamination Certificate

active

10309233

ABSTRACT:
A tube-type vortex reducer for the conduction of cooling air in a compressor1of a gas turbine with at least one radial secondary air tube2arranged in a disk interspace3, includes a deflector arranged in a discharge area of the secondary air tube for the deflection of the secondary air flow into an axial direction or away from an axial direction.

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