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公开(公告)号：US10246197B2
公开(公告)日：2019-04-02
申请号：US15280170
申请日：2016-09-29
Applicant: ROLLS-ROYCE plc
Inventor： Rory D Stieger , Matthew Moxon , Mikko Mattila
Abstract: An aircraft (10) comprising a fuselage (12), the fuselage (10) comprising at least first and second inwardly tapering portions (20, 22) extending in a generally rearward direction from an aft end of the fuselage (12), each inwardly tapering portion (20, 22) comprising a boundary layer ingesting propulsor (36) mounted thereon.
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