{
  "$type": "site.standard.document",
  "description": "The device (1) has a set of strut-like support elements (17) connected at one end to an inner wall (3) and at another end to an outer wall (4). Each support element has a thickness distribution defined along a central longitudinal plane (21). Each plane forms a positive acute angle (17G) with an…",
  "path": "/patents/998577",
  "publishedAt": "2012-09-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/162",
    "ROLLS ROYCE DEUTSCHLAND [DE]"
  ],
  "textContent": "The device (1) has a set of strut-like support elements (17) connected at one end to an inner wall (3) and at another end to an outer wall (4). Each support element has a thickness distribution defined along a central longitudinal plane (21). Each plane forms a positive acute angle (17G) with an engine axis (6) in an area (B) of the support element adjacent the inner wall, and a negative acute angle (17H) with the engine axis in an area (A) of the support element adjacent the outer wall to enlarge flow cross-sections in acute angle areas (17A, 17B) adjacent the inner and outer walls.",
  "title": "Jet engine device with a bypass flow channel"
}