{
  "$type": "site.standard.document",
  "description": "A vane arc segment (60) includes an airfoil piece (62) that defines first and second platforms (64, 66) and an airfoil section (68) that extends between the first and second platforms (64, 66). The airfoil section (68) has a trailing edge (68b), a leading edge (68a), a pressure side (68c), and a…",
  "path": "/patents/1409854",
  "publishedAt": "2023-07-26T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D5/282",
    "RAYTHEON TECH CORP [US]"
  ],
  "textContent": "A vane arc segment (60) includes an airfoil piece (62) that defines first and second platforms (64, 66) and an airfoil section (68) that extends between the first and second platforms (64, 66). The airfoil section (68) has a trailing edge (68b), a leading edge (68a), a pressure side (68c), and a suction side (68d). The platforms each define first and second circumferential mate faces (64c, 64d, 66c, 66d), forward and aft sides (64a, 64b, 66a, 66b), a gaspath side (64e, 66e), a non-gaspath side (64f, 66f), and a radial flange (70) that projects from the non-gaspath side (64f, 66f). Each radial flange (70) extends continuously and includes a first leg portion (70c) that extends adjacent the trailing edge (68b), a second leg portion (70d) that extends from the first leg portion (70c) and curves around the suction side (68d), and a third leg portion (70e) that extends from the second leg portion (70d) toward the forward side (64a, 66a).",
  "title": "VANE ARC SEGMENT WITH CURVED RADIAL FLANGE"
}