公开(公告)号：US20170121031A1

公开(公告)日：2017-05-04

申请号：US15280170

申请日：2016-09-29

Applicant: ROLLS-ROYCE plc

Inventor： Rory D. STIEGER ,  Matthew MOXON ,  Mikko MATTILA

IPC: B64D33/02 ,  B64D27/14 ,  B64C21/06 ,  B64D27/02

CPC classification number: B64D33/02 ,  B64C1/0009 ,  B64C21/06 ,  B64C2230/04 ,  B64D27/02 ,  B64D27/14 ,  B64D2033/0226 ,  Y02T50/12 ,  Y02T50/166

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.