{
  "$type": "site.standard.document",
  "description": "The cooling system (30) includes at least one channel (32) that draws off cold air (300) in a secondary air flow (200). At least one heat exchanger (34) is located in the channel for circulation of hot air (420) from a primary air flow (100) before reaching the hot parts (22) of an aircraft engine…",
  "path": "/patents/1075793",
  "publishedAt": "2005-07-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/141",
    "SNECMA MOTEURS [FR]"
  ],
  "textContent": "The cooling system (30) includes at least one channel (32) that draws off cold air (300) in a secondary air flow (200). At least one heat exchanger (34) is located in the channel for circulation of hot air (420) from a primary air flow (100) before reaching the hot parts (22) of an aircraft engine (10). The channel is provided with a supply pipe (322), an evacuation pipe (326) and an intermediate box (324). An independent claim is also included for an aircraft engine.",
  "title": "Nacelle and aircraft engine with a cooling system for its hot elements"
}