{
  "$type": "site.standard.document",
  "description": "A system 10 for heating fuel in a combined cycle gas turbine 12 includes a fuel heat exchanger 50 downstream from a turbine outlet 36, and the fuel heat exchanger 50 has an exhaust gas inlet 52, an exhaust gas outlet 54, a fuel inlet 56, and a fuel outlet 58. A first exhaust gas plenum 70 has a…",
  "path": "/patents/976040",
  "publishedAt": "2014-04-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C6/06",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A system 10 for heating fuel in a combined cycle gas turbine 12 includes a fuel heat exchanger 50 downstream from a turbine outlet 36, and the fuel heat exchanger 50 has an exhaust gas inlet 52, an exhaust gas outlet 54, a fuel inlet 56, and a fuel outlet 58. A first exhaust gas plenum 70 has a first exhaust gas inlet connection 72 between the turbine outlet 36 and a heat exchanger 50 and a first exhaust gas outlet connection 74 upstream from the exhaust gas inlet 52. A second exhaust gas plenum 80 has a second exhaust gas inlet connection 82 downstream from at least a portion of the heat exchanger 50 and a second exhaust gas outlet connection 84 upstream from the exhaust gas inlet 52.",
  "title": "System for heating fuel in a combined cycle gas turbine"
}