公开(公告)号：EP4431396A1

公开(公告)日：2024-09-18

申请号：EP24161290.2

申请日：2024-03-04

申请人： Airbus Defence and Space GmbH

发明人： KOPP, Sven ,  ABERLE-KERN, Svenja ,  BREHM, Sebastian

IPC分类号： B64D13/06 ,  B64D13/08 ,  F02C7/00

CPC分类号： B64D13/06 ,  B64D2013/061820130101 ,  B64D13/08 ,  F02C6/08 ,  F02C9/18

摘要： 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.