- 专利标题： DRAG RECOVERY SCHEME USING BOUNDARY LAYER INGESTION
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申请号： US17850674申请日： 2022-06-27
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公开(公告)号： US20220348315A1公开(公告)日： 2022-11-03
- 发明人: Mark Allan Page
- 申请人： Blended Wing Aircraft, Inc.
- 申请人地址： US CA Orange
- 专利权人： Blended Wing Aircraft, Inc.
- 当前专利权人： Blended Wing Aircraft, Inc.
- 当前专利权人地址： US CA Orange
- 主分类号： B64C21/02
- IPC分类号： B64C21/02 ; B64C39/10 ; B64D29/04 ; B64D33/02 ; B64D33/04
摘要：
Technologies are described herein for a drag recovery scheme using a boundary layer bypass duct system. In some examples, boundary layer air is routed around the intake of one or more of the engines and reintroduced aft of the engine fan in the nozzle duct in a mixer-ejector scheme. Mixer-ejectors mix the boundary layer flow to increase mass flow.
公开/授权文献
- US11975819B2 Drag recovery scheme using boundary layer ingestion 公开/授权日：2024-05-07
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