{
  "$type": "site.standard.document",
  "description": "An aircraft power plant (1), has: a combustion engine (2) having an outlet outputting combustion gases; a turbine (5) downstream of the combustion engine; a detonation combustion tube (8) fluidly connecting the combustion engine (2) to the turbine (5); a member having an open position in which the…",
  "path": "/patents/1391796",
  "publishedAt": "2025-09-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01C1/22",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "An aircraft power plant (1), has: a combustion engine (2) having an outlet outputting combustion gases; a turbine (5) downstream of the combustion engine; a detonation combustion tube (8) fluidly connecting the combustion engine (2) to the turbine (5); a member having an open position in which the outlet of the combustion engine (2) is fluidly connected to the turbine (5) and a closed position in which the combustion engine (2) is fluidly disconnected from the turbine (5); a fuel injector fluidly connected to the detonation combustion tube (8); an igniter operatively connected to the detonation combustion tube (8); and a controller operatively connected to the fuel injector and to the igniter, the controller configured to, in response to receiving of a command: inject fuel into the detonation combustion tube (8) via the fuel injector, and once the member is in the closed position, power the igniter to ignite a mixture of the combustion gases and the fuel into the detonation combustion tube (8).",
  "title": "AIRCRAFT POWER PLANT WITH DETONATION COMBUSTION TUBE"
}