{
  "$type": "site.standard.document",
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  "description": "A turbine engine fan case assembly includes a structural case (100) and a liner assembly (140). A radially accommodating attachment system connects the liner assembly (140) to the structural case (100). The attachment system comprises a circumferentially-distributed plurality of longitudinally…",
  "path": "/patents/987717",
  "publishedAt": "2013-08-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/122",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A turbine engine fan case assembly includes a structural case (100) and a liner assembly (140). A radially accommodating attachment system connects the liner assembly (140) to the structural case (100). The attachment system comprises a circumferentially-distributed plurality of longitudinally elongate radially outwardly open channels (192) mounted to the liner assembly (140). The attachment system further comprises an associated plurality of inwardly-projecting tongues (194) mounted to the structural case (100). Each tongue (194) is accommodated in an associated said channel (192).",
  "title": "FAN CASE ASSEMBLY"
}