公开(公告)号：US10717513B2

公开(公告)日：2020-07-21

申请号：US15814455

申请日：2017-11-16

Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH ,  AIRBUS HELICOPTERS

Inventor： Aurelien Vayssiere ,  Pierre Fruitet ,  Fabrice Joussellin ,  Robert Sienicki ,  Bartlomiej Tazbir ,  Michal Mroz ,  Bernhard Rein

IPC: B64C1/14 ,  E05D15/10 ,  B64C27/04 ,  E05F5/00

Abstract: A rotary wing aircraft with a fuselage that is equipped with at least one rail, comprising at least one sliding element, in particular a sliding door or a sliding window, that is slidably supported by the at least one rail, wherein the at least one sliding element is at least slidable along the at least one rail by means of an opening sliding movement into an opening movement direction from a fully closed position into a fully opened position, wherein a dampening unit is provided that dampens the opening sliding movement of the at least one sliding element upon reaching of the fully opened position.