Aircraft fuselage with door stoppers attached to a door frame bulkhead
AssigneeAirbus Operations GmbH
InventorCarsten Paul
Life of this patent
Estimating the term…
Abstract
An aircraft fuselage includes at least one opening that can be closed by a flap or door, which comes to abut against at least one door stopper that is arranged on a fuselage-side door frame bulkhead and transfers the impact forces into an intermediate costal for diversion into an aircraft structure that encompasses bulkheads, wherein the door frame bulkhead exhibits an opening, through which an impact section of the door stopper extends, wherein a fastening plate section adjoining the latter comes to abut the rear side of the door frame bulkhead, which interacts with means for directly introducing the impact forces from the door stopper into the intermediate costal.
Claims10
An aircraft fuselage comprising:
- at least one opening configured to be closed by a flap or a door,
- wherein the flap or the door is configured to abut against at least one door stopper arranged on a fuselage-side door frame bulkhead and to transfer the impact forces into an intermediate costal for diversion into an aircraft structure encompassing bulkheads,
- wherein the door frame bulkhead exhibits an opening, through which an impact section of the door stopper extends,
- wherein a fastening plate section adjoining the door stopper comes to abut the rear side of the door frame bulkhead interacting with means for directly introducing the impact forces from the door stopper into the intermediate costal.
Dependencies are inferred from the claim text.