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发明公开
CN105584617A 具有结构支柱和非结构支柱的机身 有权

具有结构支柱和非结构支柱的机身
摘要：
本发明涉及具有结构支柱和非结构支柱的机身。公开了一种交通工具(例如，飞机)的机身部。机身部包括：框架；底梁，附接至框架并且包括端部；结构支柱，包括第一端和第二端；第一结构耦接，接合底梁和结构支柱的第一端；第二结构耦接，接合框架和结构支柱的第二端；非结构支柱，包括第三端和第四端；第一非结构耦接，接合底梁和非结构支柱的第三端；以及第二非结构耦接，接合框架和非结构支柱的第四端。
摘要（英）：

The invention relates to a fuselage with structural and non-Structural stanchions. The fuselage portion of a vehicle (e.g., an aircraft) is disclosed. The fuselage portion comprises a frame; a floor beam attached to the frame and comprising ends; a structural stanchion comprising a first end and a second end; a first structural coupling joining the first end of the structural stanchion and the floor beam; a second structural coupling joining the second end of the structural stanchion and the frame; a non-structural stanchion comprising a third end and a fourth end; a first non-structural coupling joining the third end of the non-structural stanchion and the floor beam; and a second non-structural coupling (209B) joining the fourth end of the non-structural stanchion and the frame.

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