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Gas turbine inlet gas phase contaminant removal

  • US 9,492,780 B2
  • Filed: 01/16/2014
  • Issued: 11/15/2016
  • Est. Priority Date: 01/16/2014
  • Status: Active Grant
First Claim
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1. A sorption arrangement for a gas turbine, the sorption arrangement including:

  • an inlet system for the gas turbine, the inlet system including a substantially hollow chamber;

    a support structure positioned within the substantially hollow chamber, the support structure including an exterior surface configured to contact inlet air passing through the substantially hollow chamber of the inlet system; and

    a sorbent-laden media positioned on the support structure, the sorbent-laden media including one or more sorbents, wherein the support structure defines a substantially hollow interior with one or more openings extending through the support structure between the hollow interior of the support structure and the sorbent-laden media,wherein the sorbent-laden media is configured to contact inlet air passing through the substantially hollow chamber of the inlet system for the gas turbine such that gas phase contaminants are removed from the inlet air by the sorbent-laden media.

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