{
  "$type": "site.standard.document",
  "description": "A fan blade platform (82; 182; 282) assembly includes a pressure side platform half (84; 184; 284) that includes a first attachment wall (84-2; 184-2), a first gas path wall (84-1; 184-1), and a first connecting wall (84-3; 184-3) attached to both the first attachment wall (84-2; 184-2) and the…",
  "path": "/patents/1416493",
  "publishedAt": "2023-11-08T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/005",
    "RTX CORP [US]"
  ],
  "textContent": "A fan blade platform (82; 182; 282) assembly includes a pressure side platform half (84; 184; 284) that includes a first attachment wall (84-2; 184-2), a first gas path wall (84-1; 184-1), and a first connecting wall (84-3; 184-3) attached to both the first attachment wall (84-2; 184-2) and the first gas path wall (84-1; 184-1). A suction side platform half (86; 186; 286) includes a second attachment wall (86-2; 186-2), a second gas path wall (86-1; 186-1), and a second connecting wall (86-3; 186-3) attached to both the second attachment wall (86-2; 186-2) and the second gas path wall (86-1; 186-1). A seal (88; 188; 288) engages the pressure side platform half (84; 184; 284) and the suction side platform half (86; 186; 286).",
  "title": "FAN BLADE PLATFORM FOR GAS TURBINE ENGINE"
}