Combustion turbine system with integrated ion transport membrane.

摘要

Integrated gas turbine combustion engine and ion transport membrane system (221) comprising a gas turbine combustion engine including a compressor (203) with a compressed oxygen-containing gas outlet (205); a combustor (235) comprising an outer shell, a combustion zone in flow communication with the compressed oxygen-containing gas outlet, and a dilution zone (239) in flow communication with the combustion zone and having one or more dilution gas inlets; and a gas expander. The system includes an ion transport membrane oxygen recovery system (221) with an ion transport membrane module that includes a feed zone, a permeate zone, a feed inlet to the feed zone in flow communication with the compressed oxygen-containing gas outlet of the compressor, a feed zone outlet (233), and a permeate withdrawal outlet from the permeate zone (231). The feed zone outlet of the membrane module is in flow communication with any of the one or more dilution gas inlets of the combustor dilution zone (239).