{
  "$type": "site.standard.document",
  "description": "A propulsion system for an aircraft includes a gas generating core engine that generates an exhaust gas flow that is expanded through a turbine section. A power turbine is forward of the core engine and is coupled to drive a propulsor. A hydrogen fuel system supplies hydrogen fuel to the combustor…",
  "path": "/patents/1395568",
  "publishedAt": "2025-12-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B01D45/16",
    "RTX CORP [US]"
  ],
  "textContent": "A propulsion system for an aircraft includes a gas generating core engine that generates an exhaust gas flow that is expanded through a turbine section. A power turbine is forward of the core engine and is coupled to drive a propulsor. A hydrogen fuel system supplies hydrogen fuel to the combustor through a fuel flow path. A condenser (62) extracts water from the exhaust gas flow. A water separator (108) is in communication with the condenser (62) and directs the extracted water (54) to a water storage tank (90). An evaporator receives a portion of the water that is extracted by the condenser (62) and generates a steam flow. The steam flow is injected into the core flow path upstream of the turbine section.",
  "title": "HYDROGEN FUELED TURBINE ENGINE PINCH POINT WATER SEPARATOR"
}