公开(公告)号：US20180009521A1

公开(公告)日：2018-01-11

申请号：US15327118

申请日：2015-07-17

Applicant: STELIA AEROSPACE

Inventor： Hervé DUCOURNAU ,  Alain PRUDENT ,  Florian GAUCHET

IPC: B64C1/06 ,  B64C1/14

CPC classification number: B64C1/068 ,  B64C1/08 ,  B64C1/1461 ,  B64C1/1492

Abstract: An aircraft fuselage includes a structure, considered in respect of all or part of the fuselage, with fuselage upper sub-structure constituting an upper part of the fuselage and a fuselage bottom sub-structure constituting a lower part of the fuselage. Openings in the structure of the fuselage are intended for the installation of windows or doors for exiting the fuselage. Furthermore, the fuselage upper sub-structure are the fuselage bottom sub-structure form fuselage sub-structures that are assembled with one another via at least one lintel in which all or some of the openings intended for installing the exit doors or windows are formed.