{
  "$type": "site.standard.document",
  "description": "A pulse detonation system (202) for a turbofan engine (200) including a fan assembly (212) and a turbine sub-system (230), which includes at least one turbine (232), is configured to create a temperature rise and a pressure rise within the turbofan engine and to generate thrust for the turbofan…",
  "path": "/patents/1085975",
  "publishedAt": "2004-06-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K3/075",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A pulse detonation system (202) for a turbofan engine (200) including a fan assembly (212) and a turbine sub-system (230), which includes at least one turbine (232), is configured to create a temperature rise and a pressure rise within the turbofan engine and to generate thrust for the turbofan engine. The pulse detonation system includes a pulse detonation core replacement assembly (242) comprising at least one detonation chamber configured to detonate a fuel mixture. The pulse detonation core replacement assembly is positioned between the fan assembly and the turbine sub-system.",
  "title": "Combined cycle pulse detonation turbine engine"
}