公开(公告)号：US20180201362A1

公开(公告)日：2018-07-19

申请号：US15849250

申请日：2017-12-20

Applicant: Airbus Operations, S.L.

Inventor： Alberto Arana Hidalgo ,  Raúl Carlos Llamas Sandín ,  Jesús Javier Vázquez Castro

IPC: B64C21/10 ,  B64C21/06 ,  B64D29/04

CPC classification number: B64C21/10 ,  B64C1/0009 ,  B64C21/00 ,  B64C21/06 ,  B64D27/14 ,  B64D27/20 ,  B64D29/04 ,  B64D33/02 ,  B64D2033/0226 ,  B64D2033/0273 ,  B64D2033/0286 ,  Y02T50/12 ,  Y02T50/166

Abstract: An aircraft including a propulsion system formed by engines arranged to ingest boundary layer air. These engines are placed inside of nacelles partially embedded in the aircraft fuselage and, thus, their intake conduits are delimited by specific fuselage areas and the nacelles. For the specific fuselage areas skins are disclosed with a flexible portion and actuation systems over them for changing their surfaces to adapt them to the needs of the propulsion system.