{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "A gas turbine exhaust frame includes an inner barrel (38) and an outer barrel (40) establishing an annular exhaust gas flow path therebetween. A plurality of airfoils (36) extend radially between the inner barrel (38) and the radially, outer barrel (40), the plurality of airfoils (36) arranged in…",
  "path": "/patents/973230",
  "publishedAt": "2014-06-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/30",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A gas turbine exhaust frame includes an inner barrel (38) and an outer barrel (40) establishing an annular exhaust gas flow path therebetween. A plurality of airfoils (36) extend radially between the inner barrel (38) and the radially, outer barrel (40), the plurality of airfoils (36) arranged in first and second axially-spaced and circumferentially-staggered rows (42,44).",
  "title": "Staggered double row, slotted airfoil design for gas turbine exhaust frame"
}