{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (20) includes a compressor section (106), a combustor (108), and a turbine section (110). A bleed tap (116) taps air from the compressor section (106) through a bleed valve (112). The bleed valve (112) is selectively opened by a control to dump air from the compressor section…",
  "path": "/patents/1424743",
  "publishedAt": "2025-03-26T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C6/08",
    "RTX CORP [US]"
  ],
  "textContent": "A gas turbine engine (20) includes a compressor section (106), a combustor (108), and a turbine section (110). A bleed tap (116) taps air from the compressor section (106) through a bleed valve (112). The bleed valve (112) is selectively opened by a control to dump air from the compressor section (106) to a dump outlet (118). A heat exchanger duct (119) includes a duct air inlet (104) to cool a fluid in a heat exchanger (124) and a duct air outlet (122). The dump outlet (118) is within the heat exchanger duct (119).",
  "title": "ENGINE BLEED AIR DUCTING INTO HEAT EXCHANGER DUCT"
}