{
  "$type": "site.standard.document",
  "description": "The present application provides a compressor (100) for a gas turbine. The compressor may include a number of rotor wheels (120) positioned about a compressor aft section (170) having a low alloy material, a number of inlet guide vanes (180) positioned about a compressor inlet section (160), and a…",
  "path": "/patents/1013050",
  "publishedAt": "2011-05-11T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/1435",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "The present application provides a compressor (100) for a gas turbine. The compressor may include a number of rotor wheels (120) positioned about a compressor aft section (170) having a low alloy material, a number of inlet guide vanes (180) positioned about a compressor inlet section (160), and a wet compression system (190) positioned about the compressor inlet section.",
  "title": "Gas turbine compressor and method of operation"
}