{
  "$type": "site.standard.document",
  "description": "A compression pump (128) for an engine (100) is provided. The pump (128) may include a first impeller (136) operatively coupled to a main shaft (108) of the engine (100), a first inlet (144) configured to at least partially receive bypass airflow and a first outlet (148) configured to direct…",
  "path": "/patents/991794",
  "publishedAt": "2013-04-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/14",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A compression pump (128) for an engine (100) is provided. The pump (128) may include a first impeller (136) operatively coupled to a main shaft (108) of the engine (100), a first inlet (144) configured to at least partially receive bypass airflow and a first outlet (148) configured to direct compressed air to a thermal management system (130).",
  "title": "Combined Pump system for size reduction of thermal management heat exchangers and optimized ventilation to the aircraft cabin"
}