{
  "$type": "site.standard.document",
  "description": "An engine (100) contains at least one pulse detonation combustor (103) having a combustion chamber (106) and an exit nozzle (107) coupled to and downstream of the combustion chamber (107). During operation of the at least one pulse detonation combustor (103) a detonation occurs within the…",
  "path": "/patents/1009527",
  "publishedAt": "2011-09-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C5/00",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "An engine (100) contains at least one pulse detonation combustor (103) having a combustion chamber (106) and an exit nozzle (107) coupled to and downstream of the combustion chamber (107). During operation of the at least one pulse detonation combustor (103) a detonation occurs within the combustion chamber (107) and at least one of a fuel fill fraction and purge fraction of the at least one pulse detonation combustor (103) are utilized to offset a temperature peak of said detonation from a pressure peak of said detonation. The fuel fill fraction is defined as 1 - purge fraction, and the purge fraction is the ratio of the purge time of the at least one pulse detonation combustor (103) to a sum of the purge time of the at least one pulse detonation combustor (103) and a fuel fill time of the at least one pulse detonation combustor.",
  "title": "Partial filling of a pulse detonation combustor in a pulse detonation combustor based hybrid engine"
}