{
  "$type": "site.standard.document",
  "description": "A turbine exhaust case (70) for a gas turbine engine (20) includes a multiple of ceramic matrix composite (CMC) turbine exhaust case struts (72) between a CMC core nacelle aft portion (76) and a CMC tail cone (74). A corresponding gas turbine engine (20) is also provided.",
  "path": "/patents/985556",
  "publishedAt": "2013-03-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/30",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A turbine exhaust case (70) for a gas turbine engine (20) includes a multiple of ceramic matrix composite (CMC) turbine exhaust case struts (72) between a CMC core nacelle aft portion (76) and a CMC tail cone (74). A corresponding gas turbine engine (20) is also provided.",
  "title": "Ceramic matrix composite turbine exhaust case for a gas turbine engine and corresponding gas turbine engine"
}