{
  "$type": "site.standard.document",
  "description": "A turbine blade (102) includes an airfoil (106) including a pressure side (107) and a suction side (109). A platform (108) includes a pressure side wall (92) and a suction side wall (94), and has a leading edge end wall (88) and a trailing edge end wall (90). A pocket (108) is positioned under the…",
  "path": "/patents/1416506",
  "publishedAt": "2023-12-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/04",
    "RTX CORP [US]"
  ],
  "textContent": "A turbine blade (102) includes an airfoil (106) including a pressure side (107) and a suction side (109). A platform (108) includes a pressure side wall (92) and a suction side wall (94), and has a leading edge end wall (88) and a trailing edge end wall (90). A pocket (108) is positioned under the platform (108) on the pressure side (107). A hole (128) has a first end (130) communicating with the pocket (108) and having a second end (132) communicating with the pressure side wall (92). A gas turbine engine (20) is also disclosed.",
  "title": "TURBINE BLADE COOLING HOLE FOR SIDE WALL"
}