The invention relates to a pressure seal coupling device (20) for coupling first and second seal body end regions (30, 50) of an elongate and at least partially resiliently deformable pressure seal (10; 10'; 10"), the pressure seal being adapted to seal an opening (90) providing access to a pressurizable space, in particular a pressurizable interior space of an aircraft or spacecraft (100), when the opening is closed by a closure component (107; 107a, 107b). The coupling device comprises a first coupling device portion (40) at the first seal body end region (30) and a second coupling device portion (60) at the second seal body end region (50). The first and second coupling device portions are configured to engage with each other for coupling the first and second seal body end regions. The invention further relates to a pressure seal comprising such a coupling device, to a door of an aircraft comprising such a seal arranged on the door, and to a method for installing a pressure seal.
PRESSURE SEAL COUPLING DEVICE, PRESSURE SEAL, DOOR OF AN AIRCRAFT, AND METHOD FOR INSTALLING A PRESSURE SEAL
DRUCKDICHTUNGSKOPPLUNGSVORRICHTUNG, DRUCKDICHTUNG, TÜR EINES FLUGZEUGS UND VERFAHREN ZUR INSTALLATION EINER DRUCKDICHTUNG
DISPOSITIF D'ACCOUPLEMENT DE JOINT D'ÉTANCHÉITÉ À PRESSION, JOINT D'ÉTANCHÉITÉ À PRESSION, PORTE D'AÉRONEF ET PROCÉDÉ DE MONTAGE D'UN JOINT D'ÉTANCHÉITÉ À PRESSION
2024-08-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2024
|European Patent Office | 2024
|NTIS | 1969
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