Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
舱门止动结构和飞行器舱门
本发明涉及一种舱门止动结构，该舱门止动结构设置在飞行器舱门与飞行器机身之间，舱门止动结构包括：机身止动块，机身止动块固定到飞行器机身；止动钉，止动钉固定到飞行器舱门，并且在飞行器舱门闭合到飞行器机身并且在飞行器舱内增压期间，止动钉被机身止动块止挡并且与机身止动块电连通；以及电搭接结构，电搭接结构在飞行器舱门闭合到飞行器机身并且在飞行器舱内未增压期间，使飞行器舱门与飞行器机身电连通。这种舱门止动结构能够在增压前止动钉与止动块脱离时，为舱门增加导电通路，从而降低舱门与门框结构在增压前的电阻值，从而有效增加舱门的电磁防护能力。另外，本发明还涉及一种飞行器舱门。
The invention relates to a cabin door stop structure, the cabin door stop structure is arranged between an aircraft cabin door and an aircraft fuselage, and the cabin door stop structure comprises a fuselage stop block fixed to the aircraft fuselage; a stop stud secured to the aircraft cabin door and stopped by and in electrical communication with the fuselage stop block during closing of the aircraft cabin door to the aircraft fuselage and pressurization within the aircraft cabin; and an electrical lap structure that electrically communicates the aircraft cabin door with the aircraft fuselage during closing of the aircraft cabin door to the aircraft fuselage and non-pressurization within the aircraft cabin. According to the cabin door locking structure, when the locking nail is separated from the locking block before pressurization, a conductive path is added for the cabin door, so that the resistance value of the cabin door and the door frame structure before pressurization is reduced, and the electromagnetic protection capability of the cabin door is effectively improved. In addition, the invention also relates to an aircraft cabin door.
舱门止动结构和飞行器舱门
本发明涉及一种舱门止动结构，该舱门止动结构设置在飞行器舱门与飞行器机身之间，舱门止动结构包括：机身止动块，机身止动块固定到飞行器机身；止动钉，止动钉固定到飞行器舱门，并且在飞行器舱门闭合到飞行器机身并且在飞行器舱内增压期间，止动钉被机身止动块止挡并且与机身止动块电连通；以及电搭接结构，电搭接结构在飞行器舱门闭合到飞行器机身并且在飞行器舱内未增压期间，使飞行器舱门与飞行器机身电连通。这种舱门止动结构能够在增压前止动钉与止动块脱离时，为舱门增加导电通路，从而降低舱门与门框结构在增压前的电阻值，从而有效增加舱门的电磁防护能力。另外，本发明还涉及一种飞行器舱门。
The invention relates to a cabin door stop structure, the cabin door stop structure is arranged between an aircraft cabin door and an aircraft fuselage, and the cabin door stop structure comprises a fuselage stop block fixed to the aircraft fuselage; a stop stud secured to the aircraft cabin door and stopped by and in electrical communication with the fuselage stop block during closing of the aircraft cabin door to the aircraft fuselage and pressurization within the aircraft cabin; and an electrical lap structure that electrically communicates the aircraft cabin door with the aircraft fuselage during closing of the aircraft cabin door to the aircraft fuselage and non-pressurization within the aircraft cabin. According to the cabin door locking structure, when the locking nail is separated from the locking block before pressurization, a conductive path is added for the cabin door, so that the resistance value of the cabin door and the door frame structure before pressurization is reduced, and the electromagnetic protection capability of the cabin door is effectively improved. In addition, the invention also relates to an aircraft cabin door.
舱门止动结构和飞行器舱门
28.02.2025
Patent
Elektronische Ressource
Chinesisch