{
  "$type": "site.standard.document",
  "description": "The system (6) has multiple nozzles (8), which are arranged in a side wall (2) that limits stream (4) and area oriented diagonally in flow direction (x). The nozzles have a rectangular flat cross-section. An injecting channel (10) is arranged with constriction (32) upstream the nozzles, where the…",
  "path": "/patents/993798",
  "publishedAt": "2013-01-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/22",
    "MTU AERO ENGINES GMBH [DE]"
  ],
  "textContent": "The system (6) has multiple nozzles (8), which are arranged in a side wall (2) that limits stream (4) and area oriented diagonally in flow direction (x). The nozzles have a rectangular flat cross-section. An injecting channel (10) is arranged with constriction (32) upstream the nozzles, where the constriction forms a boundary surface (34). The boundary surface defines the nozzle cross-section. The injecting channel is extended upstream of the constriction. An independent claim is included for a compressor provided with a rear edge area.",
  "title": "System for injecting a fluid, compressor and turbomachine comprising the same"
}