{
  "$type": "site.standard.document",
  "description": "A CO2 bottoming cycle (40) system includes a first compressor (46) operatively connected to a first turbine (48) through a first shaft (50). A first generator is operatively connected to the first shaft. A second compressor (66) is fluidically connected to the first compressor (46). The second…",
  "path": "/patents/1396529",
  "publishedAt": "2025-12-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D15/10",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "A CO2 bottoming cycle (40) system includes a first compressor (46) operatively connected to a first turbine (48) through a first shaft (50). A first generator is operatively connected to the first shaft. A second compressor (66) is fluidically connected to the first compressor (46). The second compressor (66) is operatively connected to a second turbine (68) through a second shaft (70). A second generator is operatively connected to the second shaft. The first turbine (48) is fluidically connected to the second turbine (68).",
  "title": "MULTI-SPOOL CO2 AIRCRAFT POWER SYSTEM FOR OPERATING MULTIPLE GENERATORS"
}