{
  "$type": "site.standard.document",
  "description": "A cooling system (100) and assembly method for a gas turbine engine assembly (10) that includes mounting a gas turbine engine including an inlet and an exhaust within a module (60) that includes an inlet area (62), an exhaust area (64), and an engine area (66) extending therebetween, such that the…",
  "path": "/patents/1067980",
  "publishedAt": "2006-04-26T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/12",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A cooling system (100) and assembly method for a gas turbine engine assembly (10) that includes mounting a gas turbine engine including an inlet and an exhaust within a module (60) that includes an inlet area (62), an exhaust area (64), and an engine area (66) extending therebetween, such that the gas turbine engine is housed within the module, coupling a first deflector (110) within the module engine area such that when cooling air (160) is channeled past the deflector, the deflector induces a substantially helically-shaped cooling air flowpath around a periphery of the gas turbine engine, and coupling an exhaust duct (82) to an outlet of the module exhaust area.",
  "title": "Method and apparatus for cooling gas turbine engines"
}