{
  "$type": "site.standard.document",
  "description": "The present invention proposes an air-conducting structure (100) for an aircraft. The air-conducting structure (100) has a first duct portion (110), which is configured to conduct a first air stream (111), a second duct portion (120), which opens into the first duct portion (110) and is configured…",
  "path": "/patents/1388810",
  "publishedAt": "2026-02-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D13/06",
    "AIRBUS DEFENCE & SPACE GMBH [DE]"
  ],
  "textContent": "The present invention proposes an air-conducting structure (100) for an aircraft. The air-conducting structure (100) has a first duct portion (110), which is configured to conduct a first air stream (111), a second duct portion (120), which opens into the first duct portion (110) and is configured to conduct a second air stream (121), and a vaned rotor (130), which is arranged in the first duct portion (110) such that it can be driven by means of the second air stream (121). The air-conducting structure (100) can be used as or in an air ejector or ejector pump.",
  "title": "AIR-CONDUCTING STRUCTURE FOR AN AIRCRAFT, AIR EJECTOR OR EJECTOR PUMP, AND AIRCRAFT"
}