{
  "$type": "site.standard.document",
  "description": "The variable cycle engine has a main propulsor (1) generating supersonic flight thrust, and an auxiliary engine (16) generating thrust for take off and landing and subsonic flight. The auxiliary unit has a gas generator and a mechanism (20) transmitting part of the mechanical power from the main…",
  "path": "/patents/1099677",
  "publishedAt": "2002-12-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/36",
    "SNECMA MOTEURS [FR]"
  ],
  "textContent": "The variable cycle engine has a main propulsor (1) generating supersonic flight thrust, and an auxiliary engine (16) generating thrust for take off and landing and subsonic flight. The auxiliary unit has a gas generator and a mechanism (20) transmitting part of the mechanical power from the main propulsor towards the auxiliary unit.",
  "title": "Variable cycle propulsion device using mechanical transmission for supersonic airplanes"
}