{
  "$type": "site.standard.document",
  "description": "A turbine containing system (10) is disclosed. The system includes an intake section (14), a compressor section (16) downstream from the intake section (14), a combustor section (20) having a primary combustion system (22) downstream from the intake section (14), a secondary combustion system (24)…",
  "path": "/patents/1086129",
  "publishedAt": "2004-06-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/14",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A turbine containing system (10) is disclosed. The system includes an intake section (14), a compressor section (16) downstream from the intake section (14), a combustor section (20) having a primary combustion system (22) downstream from the intake section (14), a secondary combustion system (24) downstream from the primary combustion system (22), a turbine section (18), an exhaust section (26) and a load (28). The secondary combustion system (24) includes an injector for transversely injecting a secondary fuel into a stream of combustion products of the primary combustion system (22). The injector includes a coupling (30), a wall (34) defining an airfoil shape circumscribing a fuel mixture passage (36), and at least one exit (34) for communication between said fuel mixture passage (36) and said stream of primary combustion products.",
  "title": "Injector"
}