{
  "$type": "site.standard.document",
  "description": "A supercharging system (11) for a gas turbine system (13) is provided the supercharging system having a fan (41) mechanically coupled to the turbine shaft (27) of the turbine system. A bypass subsystem (59) is provided or optionally conveying a portion of the airstream output to other uses. The…",
  "path": "/patents/981272",
  "publishedAt": "2013-12-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C6/12",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A supercharging system (11) for a gas turbine system (13) is provided the supercharging system having a fan (41) mechanically coupled to the turbine shaft (27) of the turbine system. A bypass subsystem (59) is provided or optionally conveying a portion of the airstream output to other uses. The supercharging system may also be used in conjunction with a combined cycle power system and a bypass subsystem optionally conveys a portion of the airstream output to a heat recovery steam generator (15).",
  "title": "Gas turbine compressor inlet pressurization and flow control system"
}