{
  "$type": "site.standard.document",
  "description": "A thermal management system (230) for a component of a gas turbine engine (20) is disclosed. In various embodiments, the thermal management system (230) includes a manifold (238) extending circumferentially about a longitudinal axis (A) and defining a plenum (240); a cooling fluid transfer tube…",
  "path": "/patents/1416433",
  "publishedAt": "2024-07-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/12",
    "RTX CORP [US]"
  ],
  "textContent": "A thermal management system (230) for a component of a gas turbine engine (20) is disclosed. In various embodiments, the thermal management system (230) includes a manifold (238) extending circumferentially about a longitudinal axis (A) and defining a plenum (240); a cooling fluid transfer tube (236) disposed within the plenum (240) and configured to transfer a component cooling fluid from a component cooling fluid source to the component; and a cooling fluid passageway (244) connected to the manifold (238) and configured to transfer a plenum cooling fluid from a plenum cooling fluid source to the plenum (240).",
  "title": "THERMAL MANAGEMENT SYSTEM FOR A COMPONENT OF A GAS TURBINE ENGINE"
}