The invention provides an aircraft conical cabin integrated equipment installation covering cap and an installation method, the aircraft conical cabin integrated equipment installation covering cap comprises a conical cabin and a covering cap cover plate, the inner side of the conical cabin is provided with a covering cap countersunk head used for installing equipment such as an electrical connector, and the covering cap cover plate is detachably and fixedly installed on the outer side of the covering cap countersunk head. And a sealing part is arranged between the covering cap countersunk head and the covering cap cover plate. Through highly integrated assembly of the covering cap cover plate, the covering cap countersunk head and the conical cabin body, the covering cap cover plate, the covering cap countersunk head and the conical cabin body are good in installation matching performance on the conical cabin body, sufficient in equipment installation space and simple and convenient in production process, and through the mode that the heat-proof layer and the metal layer are combined, the structure and heat-proof requirements are considered, the aerodynamic shape of an aircraft can be kept, and the service life of the aircraft is prolonged. Through the covering cap sealing gasket, the sealant and the heat-proof putty, effective sealing can be achieved, and disassembly and assembly are convenient.
本发明提供了一种飞行器锥形舱体一体化设备安装口盖及安装方法,包括锥形舱体和口盖盖板,所述锥形舱体的内侧安装有用于安装电气接插件等设备的口盖埋头,所述口盖盖板可拆卸固定安装在口盖埋头的外侧,且所述口盖埋头和口盖盖板之间设置有密封件。通过口盖盖板、口盖埋头以及锥形舱体的高度集成化装配,在锥形舱体上的安装匹配性良好,设备安装空间充足,生产工艺简便,且通过防热层和金属层结合的形式,兼顾结构和防热需求,有助于保持飞行器的气动外形,且通过口盖密封垫、密封胶和防热腻子,有助于实现有效密封,且拆装方便。
Aircraft conical cabin integrated equipment installation covering cap and installation method
飞行器锥形舱体一体化设备安装口盖及安装方法
2021-06-15
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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