- 专利标题: Air direction arrangement for an aircraft with integrated heat exchanger
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申请号: US17497080申请日: 2021-10-08
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公开(公告)号: US11702219B2公开(公告)日: 2023-07-18
- 发明人: Martin Pfefferkorn , Robert Ehrmayr
- 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
- 代理机构: KDW Firm PLLC
- 优先权: DE 2020006235.0 2020.10.09
- 主分类号: B64D33/02
- IPC分类号: B64D33/02 ; B64D13/06
摘要:
An air direction arrangement for an aircraft. The air direction arrangement contains an inlet opening and an inlet channel connected thereto and which is at least partially surrounded by an outer wall. The inlet channel is configured to guide air to an engine of the aircraft. The outer wall contains at least one outlet channel and at least one outlet element. The outlet element is configured to selectively release or close the outlet channel for an air flow from the inlet channel into the environment of the aircraft. The air direction arrangement contains a heat exchanger in the outlet channel to discharge thermal energy to the air flow which is flowing from the inlet channel into the environment of the aircraft.
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