{
  "$type": "site.standard.document",
  "description": "In one embodiment, a pulse detonation system (10) includes a pulse detonation tube (36) including a base tube (78) and a thermally protective layer (82) disposed adjacent to an inner surface (83) of the base tube (78). The thermally protective layer (82) is configured to limit temperature…",
  "path": "/patents/1009637",
  "publishedAt": "2011-09-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D5/28",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "In one embodiment, a pulse detonation system (10) includes a pulse detonation tube (36) including a base tube (78) and a thermally protective layer (82) disposed adjacent to an inner surface (83) of the base tube (78). The thermally protective layer (82) is configured to limit temperature fluctuations at the inner surface (83) of the base tube (78) to less than approximately 20 degrees Celsius during operation of the pulse detonation system (10), and the thermally protective layer (82) does not comprise a ceramic coating.",
  "title": "Pulse detonation system for a gas turbine"
}