{
  "$type": "site.standard.document",
  "description": "A method for operating an aircraft engine facilitates preventing ice accumulation on the aircraft engine. The method comprises coupling a semi-permeable membrane (66) to the engine adjacent an outer surface (68) of the engine, coupling a fluid reservoir (62) to the aircraft engine in flow…",
  "path": "/patents/1090580",
  "publishedAt": "2004-01-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/02",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method for operating an aircraft engine facilitates preventing ice accumulation on the aircraft engine. The method comprises coupling a semi-permeable membrane (66) to the engine adjacent an outer surface (68) of the engine, coupling a fluid reservoir (62) to the aircraft engine in flow communication with the semi-permeable membrane, and supplying fluid from the fluid reservoir to the semi-permeable membrane to facilitate preventing ice accumulation on the aircraft engine outer surface.",
  "title": "Methods and apparatus for operating gas turbine engines"
}