{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "An assembly (200) for mounting an auxiliary component (120) to an engine case (210) of a gas turbine engine (100) includes a support bracket (222), the support bracket (222) having a first end (230) configured for attachment to a first flange (232) of the engine case (210), a second end (236)…",
  "path": "/patents/1400815",
  "publishedAt": "2024-07-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D21/045",
    "RTX CORP [US]"
  ],
  "textContent": "An assembly (200) for mounting an auxiliary component (120) to an engine case (210) of a gas turbine engine (100) includes a support bracket (222), the support bracket (222) having a first end (230) configured for attachment to a first flange (232) of the engine case (210), a second end (236) configured for attachment to a second flange (238) of the engine case (210), and an intermediate portion (246) located intermediate the first end (230) and the second end (236); a bearing member (248) disposed within the intermediate portion (246); a locator (224) disposed within the bearing member (248); a first plurality of bolts (234) configured to attach the first end (230) of the support bracket (222) to the first flange (232); a second plurality of bolts (240) configured to attach the second end (238) of the support bracket (222) to the second flange (238); and a mechanical fuse (264).",
  "title": "AUXILIARY COMPONENT MOUNTING SYSTEM FOR GAS TURBINE ENGINES"
}