公开(公告)号：US20200269982A1

公开(公告)日：2020-08-27

申请号：US16792488

申请日：2020-02-17

Applicant: DASSAULT AVIATION

Inventor： Christophe HARROIS ,  Jean-Rémi BILLON ,  Séverine ASFAUX

IPC: B64D11/00 ,  B64D11/04 ,  B64C1/14

Abstract: An aircraft (10) includes a fuselage (12) delimiting a cockpit (14), a passenger entry area (18) and a passenger cabin (16) configured to accommodate passengers during a flight phase. The entry area (18) is interposed longitudinally between the cockpit (14) and the cabin. The cockpit and the entry area are delimited by a front separating element (24) and the entry area and the cabin are delimited by a rear separating element (26). The fuselage delimits a side boarding door (20). A transverse median plane (66) of the boarding door is placed at a distance from the front separating element, considered along the longitudinal axis, greater than 39% of the length between the front separating element and the rear separating element, considered along the longitudinal axis.