A door (100) for an aircraft configured to move from a closed position of a cabin shell to an open position to allow inspection of an interior compartment of a cabin, comprising: a first multilayer portion (40) comprising an inner layer (10), an outer layer (30) and an intermediate layer (20), where the intermediate layer (20) is made of a composite material having an inorganic matrix and a carbon-based filler, the first portion is shaped in such a way as to have at least one substantially rectangular reinforcing projection (14, 14 '); -a second layered portion (50) having an aerodynamic profile and shaped to be coupled with the first multilayer portion (40), the integral configuration of the door (100) being such that, in the assembled configuration and in the coupled connection between the first multilayer portion (40) and the second portion (50), the substantially rectangular reinforcing protrusions (14, 14 ') face the interior compartment of the nacelle.
一种用于航空器的门(100),其被配置成从机舱外壳的关闭位置移动到打开位置以允许检查机舱的内部隔室,包括:第一多层部分(40),包括内层(10)、外层(30)和中间层(20),其中中间层(20)由具有无机基质和碳基填料的复合材料制成,第一部分以具有至少一个实质上长方形的加强突起(14、14')的方式成形;‑第二层状部分(50),具有空气动力学轮廓并且成形为与第一多层部分(40)耦合连接,门(100)的整体构造使得在组装构造中,并且在第一多层部分(40)和第二部分(50)之间的耦合连接中,实质上长方形的加强突起(14、14')面向机舱的内部隔室。
Aircraft door and method of manufacture
航空器门及制作方法
2023-09-12
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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