{
  "$type": "site.standard.document",
  "description": "Disclosed is a structural frame (38) for a gas turbine (10) engine comprising an integral fluid reservoir (60) and air/fluid heat exchanger (68;168;268). A central hub (56) includes a reservoir (60) for storing a fluid and an outer rim (62) circumscribes the hub (56). A heat exchanger (68;168;268)…",
  "path": "/patents/1069584",
  "publishedAt": "2006-03-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/162",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "Disclosed is a structural frame (38) for a gas turbine (10) engine comprising an integral fluid reservoir (60) and air/fluid heat exchanger (68;168;268). A central hub (56) includes a reservoir (60) for storing a fluid and an outer rim (62) circumscribes the hub (56). A heat exchanger (68;168;268) is fluidly coupled to the reservoir (60) and is in simultaneous communication with the fluid and an air stream.",
  "title": "A gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger"
}