{
  "$type": "site.standard.document",
  "description": "A liner panel (72A;74A) for use in a combustor of a gas turbine engine, the liner panel (72A;74A) including a cold side (110); and a rail (124a;122b) that extends from the cold side (110), the rail (124a;122b) includes a first diffusion interface passage surface (156;160) and a second diffusion…",
  "path": "/patents/1405494",
  "publishedAt": "2024-04-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/18",
    "RTX CORP [US]"
  ],
  "textContent": "A liner panel (72A;74A) for use in a combustor of a gas turbine engine, the liner panel (72A;74A) including a cold side (110); and a rail (124a;122b) that extends from the cold side (110), the rail (124a;122b) includes a first diffusion interface passage surface (156;160) and a second diffusion interface passage surface (158;162), the first diffusion interface passage surface (156;160) angled with respect to the second diffusion interface passage surface (158;162).",
  "title": "GAS TURBINE COMBUSTOR WITH LINER PANEL END RAILS"
}