{
  "$type": "site.standard.document",
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  "description": "A method for recovering air in an aircraft includes bleeding bypass air (122;196) from an engine bypass (76;152), bleeding core air (120;194) from an engine core (74;150), and placing the bypass air and the core air in a heat exchange relationship to produce heated bypass air (126;200) and cooled…",
  "path": "/patents/988658",
  "publishedAt": "2013-07-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C6/08",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "A method for recovering air in an aircraft includes bleeding bypass air (122;196) from an engine bypass (76;152), bleeding core air (120;194) from an engine core (74;150), and placing the bypass air and the core air in a heat exchange relationship to produce heated bypass air (126;200) and cooled core air (124;198). The method further includes directing the heated bypass air to one or more of: the engine bypass (76), a cowl (149) de-icing system, and a wing (206) anti-ice system.",
  "title": "AIR RECOVERY SYSTEM FOR PRECOOLER HEAT-EXCHANGER AND CORRESPONDING METHOD"
}