{
  "$type": "site.standard.document",
  "description": "A measurement system (13) for a gas turbine engine (11) is provided. The measurement system (13) comprises a sensor assembly (48). The measurement system (13) also includes multiple sensors (64) coupled to the sensor assembly (48). The sensor assembly (48) is configured to be removably inserted…",
  "path": "/patents/1422337",
  "publishedAt": "2024-11-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/02",
    "GENERAL ELECTRIC TECHNOLOGY GMBH [CH]"
  ],
  "textContent": "A measurement system (13) for a gas turbine engine (11) is provided. The measurement system (13) comprises a sensor assembly (48). The measurement system (13) also includes multiple sensors (64) coupled to the sensor assembly (48). The sensor assembly (48) is configured to be removably inserted within a space defined by a circumferential track (44, 52, 54) embedded within an inner diameter of a compressor casing (42) of the gas turbine engine (11) without having to disassemble the compressor casing (42).",
  "title": "SYSTEM AND METHOD FOR REMOVABLY INSERTING A SENSOR ASSEMBLY INTO A COMPRESSOR CASING"
}