Gas turbine engine systems and related methods involving...

Power plants – Reaction motor – Including counter rotating rotors

Reexamination Certificate

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C415S199500

Reexamination Certificate

active

07984607

ABSTRACT:
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity are provided. In this regard, a representative turbine stage for a gas turbine engine includes a first set of rotatable blades operative to be positioned downstream of and adjacent to a first set of vanes, a number of blades of the first set of blades being less than a number of vanes of the first set of vanes.

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