It is proposed a structural system for installation in a fuselage structure of an aircraft interior, the system comprising: at least one first carrier element; at least one second carrier element; at least one elongated frame element, the at least one elongated frame element having a first end and a second end; at least one first attachment means for attaching the first carrier element to the fuselage structure or to an element coupled to the fuselage structure; at least one first coupling means mounted to the first end for coupling the first carrier element with the at least one frame element; and at least one second coupling device mounted to the second end for coupling the second carrier element with the at least one frame element, where the at least one frame element is adapted to hold at least one component to be mounted inside, where the at least one frame element is adapted to hold at least one component to be mounted inside. The at least one first carrier element is designed to be coupled to the at least one first coupling device, and wherein the at least one second carrier element is designed to be coupled to the at least one second coupling device, and wherein the at least one second carrier element is designed to be coupled to the at least one second coupling device. One of the at least one first coupling device and the at least one second coupling device is adapted to be snapped into a respective carrier element, to move relative to a respective end of the frame element, and to be snapped in a desired position relative to the respective end of the frame element.
提出了一种安装到飞行器内部的机身结构中的结构系统,该系统包括:至少一个第一载体元件;至少一个第二载体元件;至少一个长形的框架元件,该至少一个长形的框架元件具有第一端部和第二端部;至少一个第一附接装置,该至少一个第一附接装置用于将第一载体元件附接至机身结构或附接至与机身结构联接的元件;至少一个第一联接装置,该至少一个第一联接装置安装到第一端部,用于将第一载体元件与至少一个框架元件联接;以及至少一个第二联接转置,该至少一个第二联接装置安装到第二端部,用于将第二载体元件与至少一个框架元件联接,其中,至少一个框架元件适于固持要安装到内部的至少一个部件,其中,至少一个第一载体元件设计用于与至少一个第一联接装置联接,其中,至少一个第二载体元件设计用于与至少一个第二联接装置联接,并且其中,至少一个第一联接装置和至少一个第二联接装置中的一个适于卡入相应的载体元件中、相对于框架元件的相应端部移动、以及相对于框架元件的该相应端部卡制在期望位置。
Structural system for installation in fuselage structure
安装到机身结构中的结构系统
2024-06-21
Patent
Electronic Resource
Chinese
STRUCTURE SYSTEM FOR INSTALLATION INTO A FUSELAGE STRUCTURE
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