{
  "$type": "site.standard.document",
  "description": "A system (200) includes one or more debris sensors or particulate sensors (71, 72, 73) are used to sense engine inlet debris (6) or particulate matter which are drawn into the engine (100) during flight, in real-time. The system (200) employs that information, in conjunction with other engine…",
  "path": "/patents/1397891",
  "publishedAt": "2025-10-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/04",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A system (200) includes one or more debris sensors or particulate sensors (71, 72, 73) are used to sense engine inlet debris (6) or particulate matter which are drawn into the engine (100) during flight, in real-time. The system (200) employs that information, in conjunction with other engine health and module health techniques, to identify which gas-path modules of the aircraft engine (100) may require maintenance or repair. In one embodiment, existing engine health technique may be based on various engine (100) operational parameters for a new engine (100) or an average engine (100).",
  "title": "USE OF PARTICULATE SENSOR IN ENGINE POWER ASSURANCE"
}