发明公开
- 专利标题： AIR-CONDUCTING STRUCTURE FOR AN AIRCRAFT, AIR EJECTOR OR EJECTOR PUMP, AND AIRCRAFT
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申请号： US18603890申请日： 2024-03-13
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公开(公告)号： US20240308671A1公开(公告)日： 2024-09-19
- 发明人: Sven KOPP , Svenja ABERLE-KERN , Sebastian BREHM
- 申请人： Airbus Defence and Space GmbH
- 申请人地址： DE Taufkirchen
- 专利权人： Airbus Defence and Space GmbH
- 当前专利权人： Airbus Defence and Space GmbH
- 当前专利权人地址： DE Taufkirchen
- 优先权： DE 2023106153.4 2023.03.13
- 主分类号： B64D13/08
- IPC分类号： B64D13/08 ; B64D13/06
摘要：
An air-conducting structure (100) for an aircraft including a first duct portion (110) 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) in the first duct portion (110) and driven by the second air stream (121). The air-conducting structure (100) may be used as or in an air ejector or ejector pump.
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