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PRESSURE SEAL COUPLING DEVICE, PRESSURE SEAL, DOOR OF AN AIRCRAFT, AND METHOD FOR MOUNTING A PRESSURE SEAL
The invention relates to a pressure seal coupling device (20) for coupling an elongated and at least partially elastically deformable pressure seal (10; 10 '; 10 ''), the pressure seal being adapted to be coupled at an opening (90) by a closure member (107; 107a, 107b), the opening providing access to a pressurizable space, in particular a pressurizable interior space of an aircraft or spacecraft (100). The coupling device comprises a first coupling device portion (40) at a first seal body end region (30) and a second coupling device portion (60) at a second seal body end region (50). The first and second coupling device portions are configured to engage each other to couple the first and second seal body end regions. The invention also relates to a pressure seal comprising such a coupling device, a door of an aircraft provided with such a seal, and a method for mounting a pressure seal.
本发明涉及一种压力密封件联接装置(20),其用于将长形且可至少部分地弹性变形的压力密封件(10;10’;10”)的第一和第二密封件本体端部区域(30、50)联接,压力密封件适于在开口(90)由闭合部件(107;107a、107b)封闭时密封该开口,开口提供通向可加压空间的通路,可加压空间特别地是飞行器或航天器(100)的可加压内部空间。联接装置包括第一密封件本体端部区域(30)处的第一联接装置部分(40)和第二密封件本体端部区域(50)处的第二联接装置部分(60)。第一和第二联接装置部分构造成彼此接合以将第一和第二密封件本体端部区域联接。本发明还涉及包括这种联接装置的压力密封件、布置有这种密封件的飞行器的门以及用于安装压力密封件的方法。
PRESSURE SEAL COUPLING DEVICE, PRESSURE SEAL, DOOR OF AN AIRCRAFT, AND METHOD FOR MOUNTING A PRESSURE SEAL
The invention relates to a pressure seal coupling device (20) for coupling an elongated and at least partially elastically deformable pressure seal (10; 10 '; 10 ''), the pressure seal being adapted to be coupled at an opening (90) by a closure member (107; 107a, 107b), the opening providing access to a pressurizable space, in particular a pressurizable interior space of an aircraft or spacecraft (100). The coupling device comprises a first coupling device portion (40) at a first seal body end region (30) and a second coupling device portion (60) at a second seal body end region (50). The first and second coupling device portions are configured to engage each other to couple the first and second seal body end regions. The invention also relates to a pressure seal comprising such a coupling device, a door of an aircraft provided with such a seal, and a method for mounting a pressure seal.
本发明涉及一种压力密封件联接装置(20),其用于将长形且可至少部分地弹性变形的压力密封件(10;10’;10”)的第一和第二密封件本体端部区域(30、50)联接,压力密封件适于在开口(90)由闭合部件(107;107a、107b)封闭时密封该开口,开口提供通向可加压空间的通路,可加压空间特别地是飞行器或航天器(100)的可加压内部空间。联接装置包括第一密封件本体端部区域(30)处的第一联接装置部分(40)和第二密封件本体端部区域(50)处的第二联接装置部分(60)。第一和第二联接装置部分构造成彼此接合以将第一和第二密封件本体端部区域联接。本发明还涉及包括这种联接装置的压力密封件、布置有这种密封件的飞行器的门以及用于安装压力密封件的方法。
PRESSURE SEAL COUPLING DEVICE, PRESSURE SEAL, DOOR OF AN AIRCRAFT, AND METHOD FOR MOUNTING A PRESSURE SEAL
压力密封件联接装置、压力密封件、飞行器的门以及用于安装压力密封件的方法
HOLTLAUF ENNO (Autor:in)
16.08.2024
Patent
Elektronische Ressource
Chinesisch
IPC:
E06B
Feste oder bewegliche Abschlüsse für Öffnungen in Bauwerken, Fahrzeugen, Zäunen oder ähnlichen Einfriedungen allgemein, z.B. Türen, Fenster, Läden, Tore
,
FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES, OR LIKE ENCLOSURES, IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
/
B64C
AEROPLANES
,
Flugzeuge
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
|