There is described an aircraft cabin section (5) comprising: a door frame (7) forming a door opening (8); a passenger door (10) arranged on the door frame (7) and configured for closing the door opening (8); and a door insulation (100) larger than the door opening (8) in at least one direction. The door insulation (100) is made of a textile that insulates heat and/or air flow. Furthermore, a door insulation for a passenger door (10) in an aircraft (1) and an aircraft having such an aircraft cabin section or such a door insulation are disclosed.
描述了一种飞行器舱室区段(5),飞行器舱室区段包括:构成门开口(8)的门框(7);乘客门(10),该乘客门布置在门框(7)上并且被配置成用于封闭门开口(8);以及门隔热件(100),该门隔热件在至少一个方向上大于门开口(8)。门隔热件(100)由隔热和/或隔绝气流的纺织品制成。此外,公开了一种用于飞行器(1)中的乘客门(10)的门隔热件以及一种具有这样的飞行器舱室区段或这样的门隔热件的飞行器。
Aircraft cabin section, door insulation and aircraft
飞行器舱室区段、门隔热件和飞行器
2022-10-28
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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