{
  "$type": "site.standard.document",
  "description": "A turbine nozzle (100) having a non-linear cooling conduit (108) is disclosed. In one embodiment, a turbine nozzle (100) includes: an airfoil (102), at least one endwall (104) adjacent the airfoil (102), and a fillet region (106) connecting the airfoil (102) and the at least one endwall (104), the…",
  "path": "/patents/974905",
  "publishedAt": "2014-05-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/12",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A turbine nozzle (100) having a non-linear cooling conduit (108) is disclosed. In one embodiment, a turbine nozzle (100) includes: an airfoil (102), at least one endwall (104) adjacent the airfoil (102), and a fillet region (106) connecting the airfoil (102) and the at least one endwall (104), the fillet region (106) including an outer surface (110). The turbine nozzle (100) also includes a non-linear cooling conduit (108) located within the fillet region (106) and adjacent the outer surface (110) of the fillet region (106), the non-linear cooling conduit (108) allows fluid flow through the fillet region (106). The non-linear cooling conduit (108) spans substantially along an axial length of the airfoil between a leading edge (113) of the airfoil (102) and a trailing edge (114) of the airfoil (102). Additionally, the non-linear cooling conduit (108) includes an arc profile substantially similar to an arc profile of the airfoil (102).",
  "title": "Turbine nozzle having non-linear cooling conduit"
}