{
  "$type": "site.standard.document",
  "description": "The method involves providing a compressor (4), a combustor (10), a turbine (12), and a flow channel (16) in gas turbine (1). The thermal energy is acquired from outlet of turbine by heat exchanger (22) in the flow channel. The thermal energy is transferred over thermal conduction before thermal…",
  "path": "/patents/987428",
  "publishedAt": "2013-08-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/305",
    "SIEMENS AG [DE]"
  ],
  "textContent": "The method involves providing a compressor (4), a combustor (10), a turbine (12), and a flow channel (16) in gas turbine (1). The thermal energy is acquired from outlet of turbine by heat exchanger (22) in the flow channel. The thermal energy is transferred over thermal conduction before thermal energy is entered into compressor by heat exchanger (26) in the flow channel. Independent claims are included for the following: (1) gas turbine; (2) heat exchanger system; and (3) power plant.",
  "title": "Method for operating a gas turbine"
}