{
  "$type": "site.standard.document",
  "description": "A fluid cooling system of an aircraft includes a compressor (42), a condenser (44), an expansion device (56), a turbine (46), and an evaporator (48) fluidly coupled to form a closed loop through which a cooling medium circulates. The expansion device is positioned such that an inlet of the…",
  "path": "/patents/1395459",
  "publishedAt": "2025-10-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D13/06",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "A fluid cooling system of an aircraft includes a compressor (42), a condenser (44), an expansion device (56), a turbine (46), and an evaporator (48) fluidly coupled to form a closed loop through which a cooling medium circulates. The expansion device is positioned such that an inlet of the expansion device receives a flow of the cooling medium from the condenser and an outlet of the expansion device delivers the flow of cooling medium to the turbine. Within the evaporator, the cooling medium is arranged in thermal communication with a medium of an environmental control system of the aircraft.",
  "title": "VAPOR COMPRESSION SYSTEM FOR AEROSPACE APPLICATIONS"
}