The invention relates to a monolithic composite structure. A monolithic composite structure and method of formation are presented. A method of laying a monolithic composite structure includes laying a plurality of circular top sheets on a circular end of a mandrel using a plurality of guide sheets; laying a plurality of cylindrical plies on the cylindrical surface of the mandrel using a laminated guide vane independent of the plurality of guide vanes; and forming a transition region by varying the length of the plurality of round top plies and the length of the plurality of cylindrical plies, the transition region including a joint between the plurality of round top plies and the plurality of cylindrical plies.
本申请涉及整体式复合结构。提出了一种整体式复合结构和形成方法。一种铺设整体式复合结构的方法,包括:使用多个导片将多个圆顶层片铺设在心轴的圆形端部上;使用独立于多个导片的叠层导片将多个圆柱形层片铺设在心轴的圆柱形表面上;以及通过改变多个圆顶层片的长度和多个圆柱形层片的长度来形成过渡区域,该过渡区域包括多个圆顶层片和多个圆柱形层片之间的接头。
Integral composite structure
整体式复合结构
2025-03-25
Patent
Electronic Resource
Chinese
IPC: | B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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