{
  "$type": "site.standard.document",
  "description": "A technique for operating a pulse detonation combustor (PDC) is provided. A flow of fuel/air mixture is provided to the combustion tube (120) via an inlet (110) and an initiation system (150) is activated at a selected location along the length of the combustion tube to ignite the fuel/air mixture…",
  "path": "/patents/984880",
  "publishedAt": "2013-06-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C5/00",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A technique for operating a pulse detonation combustor (PDC) is provided. A flow of fuel/air mixture is provided to the combustion tube (120) via an inlet (110) and an initiation system (150) is activated at a selected location along the length of the combustion tube to ignite the fuel/air mixture within the combustion tube at the selected location. This allows selection of an expected detonation region at which the combustion of the fuel/air mixture is expected to transition to a detonation.",
  "title": "Method for positioning deflagration-detonation transition during operation of a pulse detonation combustor"
}