A pressure seal coupling device for coupling first and second seal body end regions of an elongate and at least partially resiliently deformable pressure seal to seal an opening providing access to a pressurizable interior space of an aircraft or spacecraft, when the opening is closed by a closure component. The coupling device includes a first coupling device portion at the first seal body end region and a second coupling device portion at the second seal body end region. The first and second coupling device portions are configured to engage with each other for coupling the first and second seal body end regions. A pressure seal includes such a coupling device, to a door of an aircraft including such a seal arranged on the door, and a method is disclosed for installing a pressure seal.
PRESSURE SEAL COUPLING DEVICE, PRESSURE SEAL, DOOR OF AN AIRCRAFT, AND METHOD FOR INSTALLING A PRESSURE SEAL
15.08.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2024
|Europäisches Patentamt | 2024
|NTIS | 1969
|MOUNTING SYSTEM FOR A PRESSURE SEAL OF AN AIRCRAFT DOOR
Europäisches Patentamt | 2020
|Mounting system for a pressure seal of an aircraft door
Europäisches Patentamt | 2021
|