{
  "$type": "site.standard.document",
  "description": "An air cycle system (100) for a gas turbine engine includes a compressor (62), a turbine (64) and a heat exchanger (66) fluidly connected between the compressor (62) and the turbine (64). A fluid source (92) communicates a fluid through the heat exchanger (66). The heat exchanger (66) exchanges…",
  "path": "/patents/985820",
  "publishedAt": "2013-03-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/12",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "An air cycle system (100) for a gas turbine engine includes a compressor (62), a turbine (64) and a heat exchanger (66) fluidly connected between the compressor (62) and the turbine (64). A fluid source (92) communicates a fluid through the heat exchanger (66). The heat exchanger (66) exchanges heat between the fluid and an airflow communicated through the heat exchanger (66) from the compressor (62) to provide a conditioned airflow.",
  "title": "Gas turbine engine air cycle system"
}