DEDICATED FANS FOR BOUNDARY LAYER INGESTION |
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| 申请号 | US15606051 | 申请日 | 2017-05-26 | 公开(公告)号 | US20180339765A1 | 公开(公告)日 | 2018-11-29 |
| 申请人 | UNITED TECHNOLOGIES CORPORATION; | 发明人 | Alan H. Epstein; Gabriel L. Suciu; Jesse M. Chandler; | ||||
| 摘要 | A propulsion system for an aircraft comprises at least two main gas turbine engines and a plurality of dedicated boundary layer ingestion fans. An aircraft is also disclosed. | ||||||
| 权利要求 | |||||||
| 说明书全文 | |||||||
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