{
  "$type": "site.standard.document",
  "description": "Methods and apparatus for power generation and/or thermal management on a high speed flight vehicle (102) include circulating a power generation loop working fluid (122) through a power generation loop (120), which absorbs heat associated with the flight vehicle (102). A generator (170) operably…",
  "path": "/patents/1410090",
  "publishedAt": "2024-06-19T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01K25/103",
    "BOEING CO [US]"
  ],
  "textContent": "Methods and apparatus for power generation and/or thermal management on a high speed flight vehicle (102) include circulating a power generation loop working fluid (122) through a power generation loop (120), which absorbs heat associated with the flight vehicle (102). A generator (170) operably coupled to the power generation loop (120) generates electrical power. Additionally, a heat transport loop working fluid (252) may circulate through a heat transport loop (250) to provide thermal management through heat transfer.",
  "title": "METHODS AND SYSTEMS FOR GENERATING POWER AND THERMAL MANAGEMENT HAVING DUAL LOOP ARCHITECTURE"
}