{
  "$type": "site.standard.document",
  "description": "A stator assembly (22) for a compressor of a gas turbine assembly wherein air flows along a direction (D); the stator assembly comprising a stator ring (24), which extends about a longitudinal axis (A) and comprises a leading wall (30) and a trailing wall (31); the leading wall (30) being arranged…",
  "path": "/patents/1398703",
  "publishedAt": "2024-11-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/001",
    "ANSALDO ENERGIA SPA [IT]"
  ],
  "textContent": "A stator assembly (22) for a compressor of a gas turbine assembly wherein air flows along a direction (D); the stator assembly comprising a stator ring (24), which extends about a longitudinal axis (A) and comprises a leading wall (30) and a trailing wall (31); the leading wall (30) being arranged upstream the trailing wall (31) along the air flow direction (D); the trailing wall (31) being is shaped so as to define an open cavity (40).",
  "title": "STATOR ASSEMBLY FOR A COMPRESSOR OF A GAS TURBINE ASSEMBLY AND COMPRESSOR FOR A GAS TURBINE ASSEMBLY"
}